Reading prompt from stdin... OpenAI Codex v0.161.0 -------- workdir: /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 model: gpt-6-astra provider: openai approval: never sandbox: danger-full-access reasoning effort: xhigh reasoning summaries: none session id: 01a14603-7093-7592-8377-63f2aca047f5 -------- user Build realistic near-future military space interceptor (hard science fiction, real spaceflight engineering): a slim armoured fuselage with a two-seat tandem cockpit under a small faceted armoured canopy, one big fusion main engine with a bell nozzle at the rear, four RCS thruster quads, folding heat-radiator panels along the sides, a nose railgun barrel, sensor blisters, cylindrical propellant tanks; no wings (there is no air in space) (the one on sheet.jpg) as a production, REALISTIC 3D game asset in Blender, for Forge's asset library. Look at the reference images in this directory with your image tool first: sheet.jpg. It must look like a real object from a modern third-person game up close: never blocky, never toy-like, never flat colours. Blender 5.2 is headless on another machine. Write bpy scripts here and run them with: ssh gex44 /root/blender-spike/blender-5.2.0-linux-x64/blender -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/ HTML cat > /tmp/interceptor-runtime/capture.mjs <<'JS' import {chromium} from 'playwright';import fs from 'fs'; const browser=await chromium.launch({headless:true,executablePath:'/home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux64/chrome',args:['--no-sandbox','--use-angle=swiftshader','--enable-unsafe-swiftshader']});const page=await browser.newPage({viewport:{width:1600,height:900}});let errors=[];page.on('pageerror',e=>errors.push(String(e)));await page.goto('http://127.0.0.1:8347/');await page.waitForFunction(()=>window.done,{timeout:60000});await page.screenshot({path:'/tmp/interceptor-runtime/runtime.png'});fs.writeFileSync('/tmp/interceptor-runtime/runtime.json',JSON.stringify({...await page.evaluate(()=>window.result),errors},null,2));await browser.close(); JS python3 -m http.server 8347 --directory /tmp/interceptor-runtime > /tmp/interceptor-runtime/server.log 2>&1" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'node /tmp/interceptor-runtime/capture.mjs > /tmp/interceptor-runtime/capture.log 2>&1 cat /tmp/interceptor-runtime/capture.log cat /tmp/interceptor-runtime/runtime.json' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 exited 1 in 577ms: node:internal/modules/run_main:123 triggerUncaughtException( ^ browserType.launch: Failed to launch chromium because executable doesn't exist at /home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux64/chrome at /tmp/interceptor-runtime/capture.mjs:2:30 { log: [], name: 'Error' } Node.js v20.20.2 cat: /tmp/interceptor-runtime/runtime.json: No such file or directory hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'tail -8 /tmp/interceptor-critic-r1.txt tail -3 /tmp/interceptor-build.log date -u +%FT%TZ' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: 2. **Open cavity in front of the windscreen and boxy, unintegrated canopy** - **What is visible**: In [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) and [interceptor-clay-r1.png](file:///tmp/interceptor-clay-r1.png), the canopy sits inside an open rectangular trough that leaves a gaping hole at the front of the nose and open gaps along the side sills. The canopy itself is a tall, flat-roofed greenhouse box instead of a low teardrop flush with the dorsal spine. - **Correction**: Close the forward nose deck so it meets the front windscreen frame seamlessly. Lower the canopy roof by ~35%, angle the side glazing inward, and fairs the rear canopy frame smoothly into the dorsal spine without a vertical step. - **Acceptance condition**: Zero visible gaps or open interior troughs around the canopy perimeter in 3/4 and clay views; canopy roofline flows continuously into the nose and spine. 3. **Missing recessed forward flank intakes (replaced by flat surface grilles)** - **What is visible**: In [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/BUILD_COMPLETE 100.8 87994 7113348 Blender quit 2026-10-16T18:48:49Z hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'cat /tmp/interceptor-critic-r1.txt rg --files /home/claude-agent/.cache/ms-playwright/chromium-1223 | head -8' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: **Verdict: REVISE** ### Top 5 Visible Findings (Ordered by Impact) 1. **Foreshortened hull proportions, blunt nose, and oversized engine bell flare** - **What is visible**: In [interceptor-side-r1.png](file:///tmp/interceptor-side-r1.png), the fuselage is stubby and tall (roughly 2.3:1 length-to-height vs the reference's sleek 3.8:1 ratio in [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg)). The forward nose terminates abruptly right in front of the windscreen in a flat vertical face, and the fusion nozzle flares out as a wide cone that is taller than the hull. - **Correction**: Extend and taper the forward nose section ahead of the canopy to match the 16.0m x 4.2m reference silhouette. Reduce the fusion nozzle expansion angle to a tight parabolic bell whose outer rim stays within the dorsal-to-ventral tank height envelope. - **Acceptance condition**: Side orthographic view matches the reference length-to-height ratio (3.8:1), with a long tapered nose cone and a nozzle diameter no taller than the outer tank profile. 2. **Open cavity in front of the windscreen and boxy, unintegrated canopy** - **What is visible**: In [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) and [interceptor-clay-r1.png](file:///tmp/interceptor-clay-r1.png), the canopy sits inside an open rectangular trough that leaves a gaping hole at the front of the nose and open gaps along the side sills. The canopy itself is a tall, flat-roofed greenhouse box instead of a low teardrop flush with the dorsal spine. - **Correction**: Close the forward nose deck so it meets the front windscreen frame seamlessly. Lower the canopy roof by ~35%, angle the side glazing inward, and fairs the rear canopy frame smoothly into the dorsal spine without a vertical step. - **Acceptance condition**: Zero visible gaps or open interior troughs around the canopy perimeter in 3/4 and clay views; canopy roofline flows continuously into the nose and spine. 3. **Missing recessed forward flank intakes (replaced by flat surface grilles)** - **What is visible**: In [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg), deep trapezoidal intakes are carved into the forward cheeks below the front cockpit, creating the main width step between the mid-hull and the nose. In [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) and [interceptor-side-r1.png](file:///tmp/interceptor-side-r1.png), the hull flanks are flat slabs with two surface-mounted louvered grilles, plus an exposed dark cutout behind the deployed radiator panel. - **Correction**: Remove the two pasted-on side grilles. Model the recessed forward cheek intakes into the hull geometry ahead of the radiator bay, and recess a clean housing pocket behind the deployed radiator so the hull wall does not look torn open. - **Acceptance condition**: 3/4 and side views show deep structural cheek intakes below the forward cockpit and a finished mechanical recess behind the deployed radiator. 4. **Bright silver hull shader, shading artifact on flank, and missing heat-scorched metal** - **What is visible**: In [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) and [interceptor-side-r1.png](file:///tmp/interceptor-side-r1.png), the hull reads as bright, glossy silver-wh/home/claude-agent/.cache/ms-playwright/chromium-1223/DEPENDENCIES_VALIDATED /home/claude-agent/.cache/ms-playwright/chromium-1223/INSTALLATION_COMPLETE /home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux/resources.pak /home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux/chrome_crashpad_handler /home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux/libvk_swiftshader.so /home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux/libGLESv2.so /home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux/vk_swiftshader_icd.json /home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux/PrivacySandboxAttestationsPreloaded/privacy-sandbox-attestations.dat succeeded in 53061ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "cp build_interceptor-hardsf.py /tmp/interceptor-build-r1.py python3 - <<'PY' p='build_interceptor-hardsf.py' s=open(p).read().replace(\"m.segments=3\",\"m.segments=2\") s=s.replace(\"r,'Alloy',6,group,.003)\",\"r,'Alloy',6,group,0)\") s=s.replace(\"('Paint',(1,1,1),.63,.37\", \"('Paint',(1,1,1),.42,.46\") s=s.replace(\"low=.69 if neutral else .62;high=.97 if neutral else 1.15\", \"low=.58 if neutral else .62;high=.94 if neutral else 1.15\") s=s.replace(\"mix.inputs[0].default_value=.23\", \"mix.inputs[0].default_value=.40\") s=s.replace(\"(-5.85,.46,-.48,.40)\",\"(-6.10,.40,-.44,.24)\") s=s.replace(\"mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.065)\",\"hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045)\") s=s.replace(\"for k,(ya,yb) in enumerate([(-2.5,-1.0),(-.95,.65),(.70,2.1),(2.15,3.65),(3.70,4.35)]):\", \"for k,(ya,yb) in enumerate([(-.05,.65),(.70,2.1),(2.15,3.65),(3.70,4.35)]):\") s=s.replace(\"ff=[(0,1,2,3,4,5),(6,11,10,9,8,7)]+\", \"ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+\") s=s.replace(\"mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.045)\", \"\"\"cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) tube('Cheek aperture vertical rim',(x,y,.10),(x,y,.64),.032,'Alloy',10) \"\"\") s=s.replace(\" sphere('Domed propellant vessel',(x,2.40,z),(.49,2.03,.49),'Alloy',segs=48,rings=24)\\n # A lathed capsule gives a substantial straight cylinder, not an ellipsoid tank.\\n # Overlaid central jacket is flush with domed vessel.\\n lathe('Tank cylinder',[(1.13,.46),(1.28,.49),(3.52,.49),(3.68,.46)],(x,0,z),'Alloy',segments=48)\",\"\"\" cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) \"\"\") s=s.replace(\"box('Cockpit floor',(0,-1.85,.73),(1.46,4.4,.14),'Cockpit',.06)\\nfor y in [-2.70,-.92]:\", \"cockpit_start=len(GROUPS['Hull'])\\nbox('Cockpit floor',(0,-1.55,.73),(1.46,3.9,.14),'Cockpit',.06)\\nfor y in [-2.25,-.65]:\") s=s.replace(\"# Canopy mesh: faceted windscreen\", \"for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24\\n# Canopy mesh: faceted windscreen\") s=s.replace(\"CAN=[(-4.55,.39,1.03,1.18),(-3.55,.66,1.09,1.88),(-2.25,.77,1.14,2.31),(-.72,.79,1.17,2.58),(.72,.77,1.20,2.56)]\", \"\"\"CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] if y>=rows[-1][0]:return rows[-1][1:] for a,b in zip(rows,rows[1:]): if a[0]<=y<=b[0]: t=(y-a[0])/(b[0]-a[0]);return tuple(a[j]*(1-t)+b[j]*t for j in range(1,len(a))) yys=sorted(set([-5.35,-4.25,-2.9,-1.1,.70]+[r[0] for r in CAN])) for sign in [-1,1]: for ya,yb in zip(yys,yys[1:]): vv=[] for y in [ya,yb]: w,bot,top=interp(y,SECTIONS);cw,cb,ct=interp(y,CAN) if y-.7: tube('Recessed armour panel join',(x,y,bot+.30),(x,y,top-.30),.010,'Radiator',6,bevel=0) for z in [bot+.35,top-.35]:bolt((x+sign*.015,y+.065,z),r=.019) # Shoulder service conduits route from reactor to the radiator hinge. for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) \"\"\"+mark s=s.replace(mark,new) open(p,'w').write(s) PY python3 -m py_compile build_interceptor-hardsf.py sed -i 's|chrome-linux64/chrome|chrome-linux/chrome|' /tmp/interceptor-runtime/capture.mjs node /tmp/interceptor-runtime/capture.mjs > /tmp/interceptor-runtime/capture.log 2>&1 cat /tmp/interceptor-runtime/capture.log cat /tmp/interceptor-runtime/runtime.json" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 26050ms: { "bounds": { "min": [ -3.2507529258728027, -1.6027662754058838, -7.994504451751709 ], "max": [ 3.250752806663513, 2.596770763397217, 8.00416088104248 ], "size": [ 6.501505732536316, 4.199537038803101, 15.99866533279419 ] }, "drawCalls": 20, "triangles": 88322, "meshes": 18, "materials": [ "Paint", "Cockpit", "Alloy", "Glass", "Heatshield", "Lamps", "Engines", "Radiator" ], "webgl": "WebGL 2.0 (OpenGL ES 3.0 Chromium)", "paintFactor": [ 0.55, 0.56, 0.55 ], "errors": [] } hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 - <<'PY' p='build_interceptor-hardsf.py';s=open(p).read() s=s.replace(\"L.new(bw.outputs[0],ramp.inputs[0])\", \"\"\"L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) \"\"\") s=s.replace(\"for k in range(len(cr)-1):\", \"mesh('Forward laminated glass end',cr[0],[(0,1,2,3)],'Glass','Canopy')\\nfor k in range(len(cr)-1):\") a=s.index('RCS=[]\\n');b=s.index('# Fixed ventral railgun:',a) s=s[:a]+'''RCS=[] for sx in [-1,1]: for sz in [-1,1]: c=Vector((sx*1.66,4.29,sz*1.02)) sphere('RCS titanium pod',c,(.39,.48,.34),'Alloy',segs=24,rings=12) jets=[(c+Vector((-.13,.30,0)),Vector((0,1,0))),(c+Vector((.13,.30,0)),Vector((0,1,0))),(c+Vector((sx*.32,.03,0)),Vector((sx,0,0))),(c+Vector((0,.03,sz*.28)),Vector((0,0,sz)))] for p,d in jets: start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location RCS.append(p+d*.24) ''' + s[b:] s=s.replace(\"sun.energy=1.7\",\"sun.energy=1.2\") open(p,'w').write(s) PY python3 -m py_compile build_interceptor-hardsf.py scp build_interceptor-hardsf.py gex44:/root/fal-author/interceptor-hardsf-v1/ ssh gex44 '/root/blender-spike/blender-5.2.0-linux-x64/blender -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py' > /tmp/interceptor-build-r2.log 2>&1" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'cat /tmp/interceptor-critic-r1.txt' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: **Verdict: REVISE** ### Top 5 Visible Findings (Ordered by Impact) 1. **Foreshortened hull proportions, blunt nose, and oversized engine bell flare** - **What is visible**: In [interceptor-side-r1.png](file:///tmp/interceptor-side-r1.png), the fuselage is stubby and tall (roughly 2.3:1 length-to-height vs the reference's sleek 3.8:1 ratio in [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg)). The forward nose terminates abruptly right in front of the windscreen in a flat vertical face, and the fusion nozzle flares out as a wide cone that is taller than the hull. - **Correction**: Extend and taper the forward nose section ahead of the canopy to match the 16.0m x 4.2m reference silhouette. Reduce the fusion nozzle expansion angle to a tight parabolic bell whose outer rim stays within the dorsal-to-ventral tank height envelope. - **Acceptance condition**: Side orthographic view matches the reference length-to-height ratio (3.8:1), with a long tapered nose cone and a nozzle diameter no taller than the outer tank profile. 2. **Open cavity in front of the windscreen and boxy, unintegrated canopy** - **What is visible**: In [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) and [interceptor-clay-r1.png](file:///tmp/interceptor-clay-r1.png), the canopy sits inside an open rectangular trough that leaves a gaping hole at the front of the nose and open gaps along the side sills. The canopy itself is a tall, flat-roofed greenhouse box instead of a low teardrop flush with the dorsal spine. - **Correction**: Close the forward nose deck so it meets the front windscreen frame seamlessly. Lower the canopy roof by ~35%, angle the side glazing inward, and fairs the rear canopy frame smoothly into the dorsal spine without a vertical step. - **Acceptance condition**: Zero visible gaps or open interior troughs around the canopy perimeter in 3/4 and clay views; canopy roofline flows continuously into the nose and spine. 3. **Missing recessed forward flank intakes (replaced by flat surface grilles)** - **What is visible**: In [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg), deep trapezoidal intakes are carved into the forward cheeks below the front cockpit, creating the main width step between the mid-hull and the nose. In [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) and [interceptor-side-r1.png](file:///tmp/interceptor-side-r1.png), the hull flanks are flat slabs with two surface-mounted louvered grilles, plus an exposed dark cutout behind the deployed radiator panel. - **Correction**: Remove the two pasted-on side grilles. Model the recessed forward cheek intakes into the hull geometry ahead of the radiator bay, and recess a clean housing pocket behind the deployed radiator so the hull wall does not look torn open. - **Acceptance condition**: 3/4 and side views show deep structural cheek intakes below the forward cockpit and a finished mechanical recess behind the deployed radiator. 4. **Bright silver hull shader, shading artifact on flank, and missing heat-scorched metal** - **What is visible**: In [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) and [interceptor-side-r1.png](file:///tmp/interceptor-side-r1.png), the hull reads as bright, glossy silver-white with a sharp diagonal shading glitch across the forward side panel (between the two grilles). The propellant tanks and fusion nozzle lack the dark gunmetal hull contrast and bronze/blue heat scorching shown in [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg). - **Correction**: Fix non-planar faces / custom normals on the side hull to eliminate the diagonal reflection crease. Darken the primary hull material to matte/satin dark gunmetal grey, cut crisp armour panel seams into the hull, and apply bronze/blue heat-scorched metal gradients to the fusion nozzle and tank end-caps. - **Acceptance condition**: Side render shows clean, unbroken shading across all hull flats, dark gunmetal hull paint, visible panel seams, and warm heat discoloration on the nozzle and tank domes. 5. **Stepped tank nose cones, detached aft spheres, and undersized chin railgun fairing** - **What is visible**: In [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) and [interceptor-side-r1.png](file:///tmp/interceptor-side-r1.png), the four propellant tanks have pointy, stepped bullet tips at the front and separate small spheres at the rear (overlapping the RCS area). Under the nose, the railgun sits on a small, boxy block at the very tip instead of a long ventral weapon fairing. - **Correction**: Replace the pointy tank cones and rear spheres with smooth, flush hemispherical dome caps integrated into the tank cylinders, and ensure the 4 aft RCS thruster quads have clear quad-nozzle housings. Lengthen the ventral railgun fairing under the nose and thicken the twin parallel rail barrels. - **Acceptance condition**: Tanks have continuous cylindrical bodies with smooth hemispherical caps at both ends, RCS quads read clearly at the aft corners, and the railgun fairing extends under the forward nose chin. --- 0. **Blocked on you**: nothing. 1. **What you changed**: Nothing; this was a read-only visual inspection of the four image files. 2. **How you know it works**: Directly opened and visually inspected [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg), [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png), [interceptor-side-r1.png](file:///tmp/interceptor-side-r1.png), and [interceptor-clay-r1.png](file:///tmp/interceptor-clay-r1.png). 3. **What would break if you were wrong**: If any finding misread a deliberate design choice, the author would spend a revision cycle adjusting geometry that was intended; however, deployed radiators were excluded from findings as instructed. 4. **What you did NOT do**: Did not inspect the `.blend` scene or build scripts, and did not modify any files. hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'tail -10 /tmp/interceptor-build-r2.log date -u +%FT%TZ' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:189: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha 2026-10-16T18:51:51Z exited 143 in 55831ms: codex The exported GLB also loads in Three.js without errors, and its runtime paint factor is correct. The revision now has a shorter, lower canopy, fitted cockpit coaming, recessed cheek bays, and continuous tank domes. I also changed the RCS quads so their nozzles point along multiple control axes. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'tail -8 /tmp/interceptor-build-r2.log scp gex44:/root/fal-author/interceptor-hardsf-v1/final.png /tmp/interceptor-final-r2.png scp gex44:/root/fal-author/interceptor-hardsf-v1/clay.png /tmp/interceptor-clay-r2.png scp gex44:/root/fal-author/interceptor-hardsf-v1/side.png /tmp/interceptor-side-r2.png' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 3251ms: Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:189: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'ps -C blender -o pid,etime,time,pcpu,pmem,args; stat -c \"%y %n\" /root/fal-author/interceptor-hardsf-v1/clay.png' tail -3 /tmp/interceptor-build-r2.log date -u +%FT%TZ" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 503ms: PID ELAPSED TIME %CPU %MEM COMMAND 2026-10-16 20:46:59.524895888 +0200 /root/fal-author/interceptor-hardsf-v1/clay.png BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:189: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha 2026-10-16T18:52:41Z hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'ps -eo pid,comm,etime,%cpu,args | grep -F interceptor-hardsf-v1 | head -8' tail -2 /tmp/interceptor-build-r2.log" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 511ms: 3853765 python3 01:39 0.0 python3 /opt/gpu-gate/gpu_gate.py --name blender --need-mib 6000 --priority batch -- /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3855853 blender.real 01:14 141 /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3863244 bash 00:00 0.0 bash -c ps -eo pid,comm,etime,%cpu,args | grep -F interceptor-hardsf-v1 | head -8 3863246 grep 00:00 0.0 grep -F interceptor-hardsf-v1 /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:189: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "tail -25 /tmp/interceptor-build-r2.log ssh gex44 'ps -eo pid,comm,etime,%cpu,args | grep -F interceptor-hardsf-v1 | head -8'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 458ms: [INFO ] mpfb.init ..............................: Build info FROM_SOURCE [INFO ] mpfb.init ..............................: Online access preference is not enabled. Not checking if MakeHuman is online. [INFO ] mpfb.init ..............................: MPFB initialization has finished. Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Paint Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Alloy Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Heatshield Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:189: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha 3853765 python3 01:44 0.0 python3 /opt/gpu-gate/gpu_gate.py --name blender --need-mib 6000 --priority batch -- /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3855853 blender.real 01:19 146 /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3863907 bash 00:00 0.0 bash -c ps -eo pid,comm,etime,%cpu,args | grep -F interceptor-hardsf-v1 | head -8 3863909 grep 00:00 0.0 grep -F interceptor-hardsf-v1 exited 143 in 293101ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "cp build_interceptor-hardsf.py /tmp/interceptor-build-r2.py python3 - <<'PY' p='build_interceptor-hardsf.py';s=open(p).read() s=s.replace(\" uv_project(o)\\n if group\", \" uv_project(o)\\n if mat=='Lamps':\\n for uv in o.data.uv_layers.active.data:uv.uv=(.125,.5)\\n if group\") s=s.replace(\"combine.inputs['Red'].default_value=1;L.new(rm.outputs[0]\", \"aomap=N.new('ShaderNodeMapRange');aomap.inputs['To Min'].default_value=.70;aomap.inputs['To Max'].default_value=1;L.new(sep.outputs['Red'],aomap.inputs[0]);L.new(aomap.outputs[0],combine.inputs['Red']);L.new(rm.outputs[0]\") a=s.index(\" MATS[name]=m;return m\\nspecial('Glass'\") s=s[:a]+''' # Even constant glass and emissive finishes are Cycles baked for portable appearance. if not name.startswith('_'): nt=m.node_tree;N=nt.nodes;L=nt.links;out=N.get('Material Output');target=N.new('ShaderNodeTexImage');emit=N.new('ShaderNodeEmission') rgb=N.new('ShaderNodeRGB');rgb.outputs[0].default_value=(*color,1) source=rgb.outputs[0] if name=='Lamps': tc=N.new('ShaderNodeTexCoord');sep=N.new('ShaderNodeSeparateXYZ');L.new(tc.outputs['UV'],sep.inputs[0]);ramp=N.new('ShaderNodeValToRGB');L.new(sep.outputs['X'],ramp.inputs[0]);ramp.color_ramp.interpolation='CONSTANT' stops=[(0,(.12,.46,.65,1)),(.25,(1,.23,.025,1)),(.5,(1,.012,.005,1)),(.75,(.01,1,.08,1))] for i,(pos,c) in enumerate(stops): el=ramp.color_ramp.elements[i] if i<2 else ramp.color_ramp.elements.new(pos);el.position=pos;el.color=c source=ramp.outputs[0] bpy.ops.mesh.primitive_plane_add(size=2);o=bpy.context.object;o.data.materials.append(m) baked={} for kind in ['Base','Normal','ORM']: im=bpy.data.images.new(f'{name}_{kind}',64,64,alpha=False) if kind"'!='"'Base':im.colorspace_settings.name='Non-Color' target.image=im;N.active=target if kind=='Normal':L.new(bs.outputs[0],out.inputs[0]);typ='NORMAL' else: if kind=='Base':L.new(source,emit.inputs['Color']) else: for link in list(emit.inputs['Color'].links):L.remove(link) emit.inputs['Color'].default_value=(1,rough,metal,1) L.new(emit.outputs[0],out.inputs[0]);typ='EMIT' active(o);sc.cycles.samples=4;bpy.ops.object.bake(type=typ);im.filepath_raw=str(TEX/f'{name}_{kind}.png');im.file_format='PNG';im.save();baked[kind]=im bpy.data.objects.remove(o,do_unlink=True);L.new(bs.outputs[0],out.inputs[0]) for kind,im in baked.items(): n=N.new('ShaderNodeTexImage');n.image=im if kind=='Base': L.new(n.outputs[0],bs.inputs['Base Color']) if emission:L.new(n.outputs[0],bs.inputs['Emission Color']) elif kind=='Normal': nm=N.new('ShaderNodeNormalMap');L.new(n.outputs[0],nm.inputs['Color']);L.new(nm.outputs[0],bs.inputs['Normal']) else: sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m special('Glass' '''+s[a+len(\" MATS[name]=m;return m\\nspecial('Glass'\"):] s=s.replace(\" tube('Canopy actuator body',(s*.79,.65,1.23),(s*.82,-.30,1.16),.055,'Heatshield')\\n tube('Canopy actuator rod',(s*.82,-.30,1.16),(s*.77,-.83,1.17),.029,'Alloy')\", \" tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24)\") s=s.replace(\" tube('Radiator deployment arm',(s*2.04,y,-.27),P(.62,y,-.04),.045,'Heatshield',12,group)\", \" tube('Radiator rotary actuator',(s*2.15,y-.09,.26),(s*2.15,y+.09,.26),.13,'Heatshield',20)\") s=s.replace(\" sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8)\", \" nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8)\\n for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5)\") s=s.replace(\"sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8)\", \"beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8)\\nfor uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5)\") s=s.replace(\"'Canopy':[1,0,0],'Radiator_L':[0,0,1],'Radiator_R':[0,0,1]\", \"'Canopy':[-1,0,0],'Radiator_L':[0,0,1],'Radiator_R':[0,0,-1]\") s=s.replace(\"o.rotation_euler[0 if n=='Canopy' else 1]=math.radians(30)\", \"o.rotation_euler[0 if n=='Canopy' else 1]=math.radians(30 if n=='Radiator_R' else -30)\") s=s.replace(\"sc.cycles.samples=32\", \"sc.cycles.samples=48\") s=s.replace(\"def render(path,w=1920,h=1080,samples=32)\", \"def render(path,w=1920,h=1080,samples=48)\") s=s.replace(\"'Shared Cycles-baked tiling colour/normal 1024 px, packed ORM 512 px; Paint neutral texture × linear faction factor.'\", \"'Cycles baked: shared tiling colour/normal 1024 px, ORM 512 px; optical/emissive 64 px; neutral Paint texture × faction factor.'\") open(p,'w').write(s) PY python3 -m py_compile build_interceptor-hardsf.py ssh gex44 'ps -eo pid,comm,etime,%cpu,args | grep -F interceptor-hardsf-v1 | head -8; stat -c \"%y %n\" /root/fal-author/interceptor-hardsf-v1/final.png' tail -3 /tmp/interceptor-build-r2.log" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 928ms: 3870111 bash 00:00 0.0 bash -c ps -eo pid,comm,etime,%cpu,args | grep -F interceptor-hardsf-v1 | head -8; stat -c "%y %n" /root/fal-author/interceptor-hardsf-v1/final.png 3870114 grep 00:00 0.0 grep -F interceptor-hardsf-v1 2026-10-16 20:47:06.671949734 +0200 /root/fal-author/interceptor-hardsf-v1/final.png BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:189: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "scp build_interceptor-hardsf.py gex44:/root/fal-author/interceptor-hardsf-v1/ ssh gex44 'nohup /root/blender-spike/blender-5.2.0-linux-x64/blender -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py > /root/fal-author/interceptor-hardsf-v1/evidence/build.log 2>&1 < /dev/null & echo "'$!'"' date -u +%FT%TZ" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 1428ms: 3871397 2026-10-16T18:53:55Z hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -18 /root/fal-author/interceptor-hardsf-v1/evidence/build.log; ps -eo pid,etime,%cpu,args | grep -F interceptor-hardsf-v1/build_interceptor | head -4' wc -l build_interceptor-hardsf.py df -h /" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 567ms: Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Alloy Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Heatshield Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:191: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha 3871397 00:43 0.1 python3 /opt/gpu-gate/gpu_gate.py --name blender --need-mib 6000 --priority batch -- /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3871890 00:33 131 /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3874362 00:00 0.0 bash -c tail -18 /root/fal-author/interceptor-hardsf-v1/evidence/build.log; ps -eo pid,etime,%cpu,args | grep -F interceptor-hardsf-v1/build_interceptor | head -4 3874365 00:00 0.0 grep -F interceptor-hardsf-v1/build_interceptor 593 build_interceptor-hardsf.py Filesystem Size Used Avail Use% Mounted on /dev/sda1 150G 136G 7.9G 95% / context compacted hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 28 /root/fal-author/interceptor-hardsf-v1/evidence/build.log; ps -eo pid,etime,pcpu,args | grep -F interceptor-hardsf-v1 | grep -v grep'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 exited 1 in 570ms: 20:55:45 | WARNING: More than one shader node tex image used for a texture. The resulting glTF sampler will behave like the first shader node tex image. 20:55:45 | WARNING: More than one shader node tex image used for a texture. The resulting glTF sampler will behave like the first shader node tex image. 20:55:45 | WARNING: More than one shader node tex image used for a texture. The resulting glTF sampler will behave like the first shader node tex image. 20:55:45 | INFO: Primitives created: 8 20:55:45 | INFO: Extracting primitive: Forward laminated glass end 20:55:45 | INFO: Primitives created: 4 20:55:45 | INFO: Extracting primitive: Radiator cassette 20:55:45 | INFO: Primitives created: 3 20:55:45 | INFO: Extracting primitive: Radiator cassette.005 20:55:45 | INFO: Primitives created: 3 20:55:45 | INFO: Finished glTF 2.0 export in 0.26047778129577637 s Info: Saved as "interceptor.blend" FIRST_GLB_COMPLETE 98.6 7819952 01:48.440 render | Saved: '/root/fal-author/interceptor-hardsf-v1/final.png' 01:56.975 render | Saved: '/root/fal-author/interceptor-hardsf-v1/side.png' 02:01.214 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/rear.png' 02:06.118 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/cockpit.png' 02:13.131 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/pivot_test.png' 02:14.989 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Naval_grey.png' 02:16.343 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Gunmetal.png' 02:17.758 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Olive_drab.png' 02:19.082 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Desert_sand.png' 02:20.455 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Arctic_white.png' 02:21.775 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Deep_navy.png' BUILD_COMPLETE 141.2 87996 7819952 Blender quit hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/final.png /tmp/interceptor-final-r2.png' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 991ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/evidence/rear.png gex44:/root/fal-author/interceptor-hardsf-v1/evidence/cockpit.png gex44:/root/fal-author/interceptor-hardsf-v1/evidence/pivot_test.png /tmp/interceptor-runtime/' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/side.png gex44:/root/fal-author/interceptor-hardsf-v1/clay.png gex44:/root/fal-author/interceptor-hardsf-v1/paints.png /tmp/interceptor-runtime/' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 2932ms: succeeded in 2962ms: hook: PreToolUse hook: PreToolUse Completed codex The revised asset is complete and within budget at 88,000 triangles and 7.8 MB. The new render shows two areas to refine: the windscreen-to-nose junction and the large, overly smooth hull panels. I’m tightening those details before final validation. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "sed -n '1,245p' build_interceptor-hardsf.py" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: """Forge hard-SF interceptor. Blender 5.2, clean-scene build, CC0 tile bakes, GLB and evidence renders. Run: blender -b --python-exit-code 1 --python build_interceptor-hardsf.py Coordinates during authoring: X left, -Y forward, Z up. Export converts to X left, Y up, Z forward. Scope: 16 x 6.5 x 4.2m; 40–90k tris; <=9 mats; 1024 colour/normal, 512 ORM; <=12MB. Views: hero front-left, ortho side, clay, six paints, 30-degree hinge test. Revision cap: 3. """ import bpy, math, os, sys, json, urllib.request, subprocess, struct, time import numpy as np from mathutils import Vector, Matrix from pathlib import Path from math import sin, cos, pi ROOT=Path(__file__).resolve().parent TEX=ROOT/'textures'; TEX.mkdir(exist_ok=True) EVID=ROOT/'evidence'; EVID.mkdir(exist_ok=True) START=time.time() bpy.ops.wm.read_factory_settings(use_empty=True) sc=bpy.context.scene sc.unit_settings.system='METRIC';sc.unit_settings.scale_length=1 sc.render.engine='CYCLES';sc.cycles.device='GPU';sc.cycles.samples=48 prefs=bpy.context.preferences.addons['cycles'].preferences for backend in ['OPTIX','CUDA']: try: prefs.compute_device_type=backend;prefs.get_devices() if any(d.type==backend for d in prefs.devices): for d in prefs.devices:d.use=d.type==backend break except Exception:pass else:raise RuntimeError('CUDA/OptiX GPU required') sc.cycles.use_denoising=True;sc.render.image_settings.file_format='PNG' sc.view_settings.view_transform='AgX' sc.render.resolution_percentage=100 sc.render.film_transparent=False GROUPS={'Hull':[],'Canopy':[],'Radiator_L':[],'Radiator_R':[]} MATS={}; BAKE_LOG=[] def active(o): bpy.ops.object.select_all(action='DESELECT');o.select_set(True);bpy.context.view_layer.objects.active=o def uv_project(o): uv=o.data.uv_layers.new(name='UVMap') if not o.data.uv_layers else o.data.uv_layers.active for f in o.data.polygons: n=f.normal;axis=max(range(3),key=lambda i:abs(n[i]));a,b=([1,2] if axis==0 else [0,2] if axis==1 else [0,1]) for li in f.loop_indices: p=o.data.vertices[o.data.loops[li].vertex_index].co uv.data[li].uv=(p[a]*.57,p[b]*.57) def finish(o,name,mat,group='Hull',bevel=0,smooth=False): o.name=name if mat:o.data.materials.append(MATS[mat] if isinstance(mat,str) else mat) if bevel: active(o);m=o.modifiers.new('Machined edge radii','BEVEL');m.width=bevel;m.segments=2 bpy.ops.object.modifier_apply(modifier=m.name) if smooth: for p in o.data.polygons:p.use_smooth=True else: # Weighted face normals preserve armour planes while letting chamfers catch highlights. active(o) if bevel: for p in o.data.polygons:p.use_smooth=True m=o.modifiers.new('Weighted normals','WEIGHTED_NORMAL');m.keep_sharp=True;m.weight=50 bpy.ops.object.modifier_apply(modifier=m.name) uv_project(o) if mat=='Lamps': for uv in o.data.uv_layers.active.data:uv.uv=(.125,.5) if group:GROUPS[group].append(o) return o def mesh(name,verts,faces,mat,group='Hull',bevel=0,smooth=False): me=bpy.data.meshes.new(name);me.from_pydata(verts,[],faces);me.update() o=bpy.data.objects.new(name,me);sc.collection.objects.link(o) # Make connected surfaces outward-facing. import bmesh bm=bmesh.new();bm.from_mesh(me);bmesh.ops.recalc_face_normals(bm,faces=bm.faces);bm.to_mesh(me);bm.free() return finish(o,name,mat,group,bevel,smooth) def box(name,loc,size,mat='Paint',bevel=.025,group='Hull'): bpy.ops.mesh.primitive_cube_add(size=1,location=loc);o=bpy.context.object o.data.transform(Matrix.Diagonal(Vector((*size,1))));return finish(o,name,mat,group,bevel) def sphere(name,loc,scale,mat='Alloy',group='Hull',segs=32,rings=16): bpy.ops.mesh.primitive_uv_sphere_add(segments=segs,ring_count=rings,radius=1,location=loc);o=bpy.context.object o.data.transform(Matrix.Diagonal(Vector((*scale,1))));return finish(o,name,mat,group,0,True) def tube(name,a,b,r,mat='Alloy',vertices=12,group='Hull',bevel=.008): a,b=Vector(a),Vector(b);d=b-a bpy.ops.mesh.primitive_cylinder_add(vertices=vertices,radius=r,depth=d.length,location=(a+b)/2) o=bpy.context.object;o.rotation_euler=d.to_track_quat('Z','Y').to_euler() o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object if axis=='Y':o.data.transform(Matrix.Rotation(pi/2,4,'X')) elif axis=='X':o.data.transform(Matrix.Rotation(pi/2,4,'Y')) return finish(o,name,mat,group,0,True) def bolt(loc,axis='X',group='Hull',r=.026): p=Vector(loc);v=Vector((1,0,0) if axis=='X' else (0,1,0) if axis=='Y' else (0,0,1)) return tube('Captive fastener',p-v*.012,p+v*.012,r,'Alloy',6,group,0) def lathe(name,profile,center,mat,group='Hull',segments=64,axis='Y'): # profile is axial-position, radius; can include outer and inner contour for real bell thickness vs=[] for y,r in profile: for j in range(segments): a=2*pi*j/segments;p=Vector((r*cos(a),y,r*sin(a))) if axis=='X':p=Vector((y,r*cos(a),r*sin(a))) vs.append(p+Vector(center)) fs=[] for k in range(len(profile)-1): for j in range(segments):fs.append((k*segments+j,k*segments+(j+1)%segments,(k+1)*segments+(j+1)%segments,(k+1)*segments+j)) return mesh(name,vs,fs,mat,group,0,True) def download(asset,mapname): p=TEX/f'{asset}_{mapname}_1k.jpg' if not p.exists(): url=f'https://dl.polyhaven.org/file/ph-assets/Textures/jpg/1k/{asset}/{asset}_{mapname}_1k.jpg' req=urllib.request.Request(url,headers={'User-Agent':'Mozilla/5.0'}) try:p.write_bytes(urllib.request.urlopen(req,timeout=90).read()) except Exception:subprocess.run(['curl','-L','--fail','-A','Mozilla/5.0',url,'-o',str(p)],check=True) return p # The two CC0 source sets are shared by every opaque surface. No image-generation sources. PH={} for asset in ['metal_plate','metal_plate_02']: for k in ['diff','nor_gl','arm']: im=bpy.data.images.load(str(download(asset,k)),check_existing=True) if k!='diff':im.colorspace_settings.name='Non-Color' PH[asset,k]=im def bake_material(name,color,metal,rough,asset='metal_plate',relief=.1,neutral=False): m=bpy.data.materials.new(name);m.use_nodes=True;nt=m.node_tree;nt.nodes.clear();N=nt.nodes;L=nt.links out=N.new('ShaderNodeOutputMaterial');bs=N.new('ShaderNodeBsdfPrincipled');L.new(bs.outputs['BSDF'],out.inputs['Surface']) uv=N.new('ShaderNodeTexCoord') def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 low=.58 if neutral else .62;high=.94 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 L.new(noise.outputs['Fac'],pits.inputs[0]);mix=N.new('ShaderNodeMixRGB');mix.blend_type='MULTIPLY';mix.inputs[0].default_value=.40 L.new(ramp.outputs[0],mix.inputs[1]);L.new(pits.outputs[0],mix.inputs[2]);L.new(mix.outputs[0],bs.inputs['Base Color']) sep=N.new('ShaderNodeSeparateColor');L.new(arm.outputs['Color'],sep.inputs[0]) rm=N.new('ShaderNodeMapRange');rm.inputs['To Min'].default_value=max(.15,rough-.10);rm.inputs['To Max'].default_value=min(.85,rough+.15);L.new(sep.outputs['Green'],rm.inputs[0]);L.new(rm.outputs[0],bs.inputs['Roughness']) bs.inputs['Metallic'].default_value=metal nm=N.new('ShaderNodeNormalMap');nm.inputs['Strength'].default_value=relief;L.new(normal.outputs['Color'],nm.inputs['Color']);L.new(nm.outputs[0],bs.inputs['Normal']) bpy.ops.mesh.primitive_plane_add(size=2,location=(0,0,0));o=bpy.context.object;o.name='Tile bake fixture';o.data.materials.append(m) target=N.new('ShaderNodeTexImage');N.active=target emit=N.new('ShaderNodeEmission');combine=N.new('ShaderNodeCombineColor');aomap=N.new('ShaderNodeMapRange');aomap.inputs['To Min'].default_value=.70;aomap.inputs['To Max'].default_value=1;L.new(sep.outputs['Red'],aomap.inputs[0]);L.new(aomap.outputs[0],combine.inputs['Red']);L.new(rm.outputs[0],combine.inputs['Green']);combine.inputs['Blue'].default_value=metal baked={} for kind,res in [('Base',1024),('Normal',1024),('ORM',512)]: im=bpy.data.images.new(f'{name}_{kind}',res,res,alpha=False) if kind!='Base':im.colorspace_settings.name='Non-Color' target.image=im;N.active=target if kind=='Normal':L.new(bs.outputs[0],out.inputs['Surface']);typ='NORMAL' else: L.new(mix.outputs[0] if kind=='Base' else combine.outputs[0],emit.inputs['Color']);L.new(emit.outputs[0],out.inputs['Surface']);typ='EMIT' active(o);sc.cycles.samples=8;sc.render.bake.margin=8;bpy.ops.object.bake(type=typ) im.filepath_raw=str(TEX/f'{name}_{kind}.png');im.file_format='PNG';im.save();baked[kind]=im bpy.data.objects.remove(o,do_unlink=True) nt.nodes.clear();out=N.new('ShaderNodeOutputMaterial');bs=N.new('ShaderNodeBsdfPrincipled');L.new(bs.outputs[0],out.inputs[0]);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough for kind in ['Base','Normal','ORM']: n=N.new('ShaderNodeTexImage');n.image=baked[kind];n.label='Cycles baked shared tile' if kind=='Base': if name=='Paint': tint=N.new('ShaderNodeMixRGB');tint.name='Faction paint factor';tint.blend_type='MULTIPLY';tint.inputs[0].default_value=1;tint.inputs[2].default_value=(.55,.56,.55,1);L.new(n.outputs[0],tint.inputs[1]);L.new(tint.outputs[0],bs.inputs['Base Color']) else:L.new(n.outputs[0],bs.inputs['Base Color']) elif kind=='Normal': nm=N.new('ShaderNodeNormalMap');L.new(n.outputs[0],nm.inputs['Color']);L.new(nm.outputs[0],bs.inputs['Normal']) else: sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) # glTF occlusion channel, packed with roughness and metalness. ng=bpy.data.node_groups.get('glTF Material Output') if not ng: ng=bpy.data.node_groups.new('glTF Material Output','ShaderNodeTree');ng.interface.new_socket(name='Occlusion',in_out='INPUT',socket_type='NodeSocketFloat') gn=N.new('ShaderNodeGroup');gn.node_tree=ng;L.new(sep.outputs['Red'],gn.inputs['Occlusion']) MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha if emission:bs.inputs['Emission Color'].default_value=(*color,1);bs.inputs['Emission Strength'].default_value=emission if alpha<1: m.surface_render_method='BLENDED';m.use_transparent_shadow=True # Even constant glass and emissive finishes are Cycles baked for portable appearance. if not name.startswith('_'): nt=m.node_tree;N=nt.nodes;L=nt.links;out=N.get('Material Output');target=N.new('ShaderNodeTexImage');emit=N.new('ShaderNodeEmission') rgb=N.new('ShaderNodeRGB');rgb.outputs[0].default_value=(*color,1) source=rgb.outputs[0] if name=='Lamps': tc=N.new('ShaderNodeTexCoord');sep=N.new('ShaderNodeSeparateXYZ');L.new(tc.outputs['UV'],sep.inputs[0]);ramp=N.new('ShaderNodeValToRGB');L.new(sep.outputs['X'],ramp.inputs[0]);ramp.color_ramp.interpolation='CONSTANT' stops=[(0,(.12,.46,.65,1)),(.25,(1,.23,.025,1)),(.5,(1,.012,.005,1)),(.75,(.01,1,.08,1))] for i,(pos,c) in enumerate(stops): el=ramp.color_ramp.elements[i] if i<2 else ramp.color_ramp.elements.new(pos);el.position=pos;el.color=c source=ramp.outputs[0] bpy.ops.mesh.primitive_plane_add(size=2);o=bpy.context.object;o.data.materials.append(m) baked={} for kind in ['Base','Normal','ORM']: im=bpy.data.images.new(f'{name}_{kind}',64,64,alpha=False) if kind!='Base':im.colorspace_settings.name='Non-Color' target.image=im;N.active=target if kind=='Normal':L.new(bs.outputs[0],out.inputs[0]);typ='NORMAL' else: if kind=='Base':L.new(source,emit.inputs['Color']) else: for link in list(emit.inputs['Color'].links):L.remove(link) emit.inputs['Color'].default_value=(1,rough,metal,1) L.new(emit.outputs[0],out.inputs[0]);typ='EMIT' active(o);sc.cycles.samples=4;bpy.ops.object.bake(type=typ);im.filepath_raw=str(TEX/f'{name}_{kind}.png');im.file_format='PNG';im.save();baked[kind]=im bpy.data.objects.remove(o,do_unlink=True);L.new(bs.outputs[0],out.inputs[0]) for kind,im in baked.items(): n=N.new('ShaderNodeTexImage');n.image=im if kind=='Base': L.new(n.outputs[0],bs.inputs['Base Color']) if emission:L.new(n.outputs[0],bs.inputs['Emission Color']) elif kind=='Normal': nm=N.new('ShaderNodeNormalMap');L.new(n.outputs[0],nm.inputs['Color']);L.new(nm.outputs[0],bs.inputs['Normal']) else: sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m special('Glass' ,(.19,.30,.36),.18,.14,.30) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] for s in SECTIONS:vs+=ring(*s) fs=[] for k in range(len(SECTIONS)-1): for j in range(8): if j==0 and 1<=k<=4:continue # actual cockpit aperture, no opaque deck behind glazing hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "sed -n '245,490p' build_interceptor-hardsf.py" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: if j==0 and 1<=k<=4:continue # actual cockpit aperture, no opaque deck behind glazing fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) # Low armoured dorsal spine behind the cockpit. vs=[] for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) mesh('Dorsal reactor shielding',vs,fs,'Paint',bevel=.065) # Recessed vent bays and fitted armour tiles along the shoulder. for sign in [-1,1]: for k,(ya,yb) in enumerate([(-.05,.65),(.70,2.1),(2.15,3.65),(3.70,4.35)]): x=sign*(2.13 if ya>=-.95 else 1.78) box('Inset thermal service bay',(x,(ya+yb)/2,.21),(.14,yb-ya,.78),'Cockpit',.06) for z in [-.25,.69]:tube('Service bay rim',(x*1.012,ya,z),(x*1.012,yb,z),.045,'Paint') for y in [ya,yb]:tube('Service bay rim',(x*1.012,y,-.25),(x*1.012,y,.69),.045,'Paint') for j in range(9): y=ya+.11+(yb-ya-.22)*j/8 box('Heat exchanger louvre',(x*1.025,y,.21),(.09,.055,.65),'Alloy',.012) for y in [ya+.09,yb-.09]: for z in [-.19,.62]:bolt((x*1.04,y,z)) # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) for xx in [-.17,.17]: for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) tube('Cheek aperture vertical rim',(x,y,.10),(x,y,.64),.032,'Alloy',10) # Sensor blister: seat is tangent to nose flank, optical aperture points forward. sphere('Protected sensor blister',(sign*.83,-4.42,.20),(.22,.52,.17),'Alloy',segs=24,rings=12) tube('Sensor optical hood',(sign*.83,-4.88,.20),(sign*.83,-4.98,.20),.085,'Cockpit',24) tube('Sensor glass',(sign*.83,-4.985,.20),(sign*.83,-4.993,.20),.061,'Glass',24,bevel=.002) # Panel seams with paired armoured ribs, belly doors closed. for y,w,bot,top in SECTIONS[2:-1]: for sign in [-1,1]: tube('Armour seam', (sign*w*.69,y,bot+.04),(sign*w*.99,y,bot+.28),.015,'Alloy',8) for z in [bot+.35,top-.36]:bolt((sign*(w+.006),y,z),r=.024) for y in [-1.8,.2,2.2]: box('Closed ventral equipment door',(0,y,-1.045),(1.3,1.8,.07),'Alloy',.07) box('Flush ventral armour',(0,y,-1.09),(1.19,1.69,.04),'Paint',.06) for x in [-.48,.48]: for yy in [-.66,.66]:bolt((x,y+yy,-1.12),'Z') # Armour seams follow the longitudinal loft, held just proud of the skin (not z-fighting). for sign in [-1,1]: for y in [-4.82,-3.55,-2.82,-.86,1.04,2.72,3.85]: # interpolate the outer side face at this longitudinal station for a,b in zip(SECTIONS,SECTIONS[1:]): if a[0]<=y<=b[0]: t=(y-a[0])/(b[0]-a[0]);w=a[1]*(1-t)+b[1]*t;bot=a[2]*(1-t)+b[2]*t;top=a[3]*(1-t)+b[3]*t;break x=sign*(w+.009) # narrow dark join with a fine metal edge, segmented around the recesses if y<-2.6 or y>-.7: tube('Recessed armour panel join',(x,y,bot+.30),(x,y,top-.30),.010,'Radiator',6,bevel=0) for z in [bot+.35,top-.35]:bolt((x+sign*.015,y+.065,z),r=.019) # Shoulder service conduits route from reactor to the radiator hinge. for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: x=sx*1.46;z=1.39 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) torus('Retaining band lip',(x,y-.04,z),.499,.012,'Alloy',segs=48) box('Tank saddle',(x,y,z-sz*.40),(.72,.18,.25),'Paint',.035) for dx in [-.24,.24]:bolt((x+dx,y,z+sz*.49),'Z',r=.023) tube('Propellant feed',(x,4.17,z),(sx*1.17,4.85,sz*.63),.065,'Heatshield',16) torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) box('Cockpit floor',(0,-1.55,.73),(1.46,3.9,.14),'Cockpit',.06) for y in [-2.25,-.65]: box('Seat pedestal',(0,y,.98),(.48,.53,.42),'Alloy',.06) box('Crashworthy seat cushion',(0,y,1.23),(.59,.69,.19),'Cockpit',.09) back=box('Seat back',(0,y+.29,1.67),(.59,.18,.81),'Cockpit',.085);back.rotation_euler.x=-.13 box('Head restraint',(0,y+.32,2.12),(.40,.22,.27),'Cockpit',.08) for s in [-1,1]: tube('Seat frame',(s*.32,y+.30,1.12),(s*.32,y+.34,2.05),.035,'Alloy') tube('Harness webbing',(s*.14,y+.175,1.35),(s*.20,y+.16,2.00),.027,'Heatshield',8) box('Side console',(s*.55,y-.12,1.37),(.24,.80,.25),'Cockpit',.05) for j in range(5):box('Console switch',(s*.55,y-.39+j*.12,1.505),(.04,.04,.025),'Alloy',.005) tube('Control stick',(0,y-.27,1.27),(0,y-.40,1.55),.032,'Alloy') sphere('Hand grip',(0,y-.40,1.56),(.055,.06,.09),'Cockpit',segs=12,rings=8) # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] if y>=rows[-1][0]:return rows[-1][1:] for a,b in zip(rows,rows[1:]): if a[0]<=y<=b[0]: t=(y-a[0])/(b[0]-a[0]);return tuple(a[j]*(1-t)+b[j]*t for j in range(1,len(a))) yys=sorted(set([-5.35,-4.25,-2.9,-1.1,.70]+[r[0] for r in CAN])) for sign in [-1,1]: for ya,yb in zip(yys,yys[1:]): vv=[] for y in [ya,yb]: w,bot,top=interp(y,SECTIONS);cw,cb,ct=interp(y,CAN) if y90000: for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. world=bpy.data.worlds.new('Deep space');world.use_nodes=True;sc.world=world nt=world.node_tree;nt.nodes.clear();N=nt.nodes;L=nt.links out=N.new('ShaderNodeOutputWorld');bg=N.new('ShaderNodeBackground');bg.inputs['Strength'].default_value=.24 coord=N.new('ShaderNodeTexCoord');sep=N.new('ShaderNodeSeparateXYZ');L.new(coord.outputs['Normal'],sep.inputs[0]);r=N.new('ShaderNodeValToRGB');r.color_ramp.elements[0].position=0;r.color_ramp.elements[0].color=(.003,.006,.014,1);r.color_ramp.elements[1].position=1;r.color_ramp.elements[1].color=(.025,.043,.075,1);L.new(sep.outputs['Z'],r.inputs[0]);L.new(r.outputs[0],bg.inputs[0]);L.new(bg.outputs[0],out.inputs[0]) def area(name,loc,power,color,size,target=(0,0,0)): d=bpy.data.lights.new(name,'AREA');d.energy=power;d.color=color;d.shape='DISK';d.size=size;o=bpy.data.objects.new(name,d);sc.collection.objects.link(o);o.location=loc;o.rotation_euler=(Vector(target)-o.location).to_track_quat('-Z','Y').to_euler() area('Upper front white key',(3,-8,12),2500,(1,.97,.92),7) area('Cool soft fill',(-8,-1,6),1800,(.64,.78,1),8) area('Engine rim',(1,9,8),2900,(.72,.83,1),6) area('Soft belly fill',(3,-2,-6),700,(.66,.73,1),6) sun=bpy.data.lights.new('Sunlight','SUN');sun.energy=1.2;sun.angle=.08;sun.color=(1,.98,.95);so=bpy.data.objects.new('Sunlight',sun);sc.collection.objects.link(so);so.rotation_euler=(.4,-.5,-.4) camd=bpy.data.cameras.new('Evidence camera');cam=bpy.data.objects.new('Evidence camera',camd);sc.collection.objects.link(cam);sc.camera=cam HERO=(15,-22,14) def camera(loc,target=(0,0,.1),ortho=19.0): cam.location=loc;cam.rotation_euler=(Vector(target)-cam.location).to_track_quat('-Z','Y').to_euler();camd.type='ORTHO';camd.ortho_scale=ortho camera(HERO) def render(path,w=1920,h=1080,samples=48): sc.render.resolution_x=w;sc.render.resolution_y=h;sc.cycles.samples=samples;sc.render.filepath=str(path);bpy.ops.render.render(write_still=True) # First a clay gate with all silhouette geometry visible. clay=special('_Clay',(.32,.34,.36),.15,.42) sc.view_layers[0].material_override=clay render(ROOT/'clay.png',1920,1080,24) sc.view_layers[0].material_override=None # Save and export the first complete asset before final evidence renders. paint=MATS['Paint'];pnt=paint.node_tree;bs=pnt.nodes.get('Principled BSDF');tint=pnt.nodes['Faction paint factor'];base=next(n for n in pnt.nodes if n.type=='TEX_IMAGE' and n.image.name=='Paint_Base') pnt.links.new(base.outputs[0],bs.inputs['Base Color']) bpy.ops.object.select_all(action='DESELECT') for o in sc.objects: if o.type in ['MESH','EMPTY']:o.select_set(True) bpy.ops.export_scene.gltf(filepath=str(ROOT/'interceptor-hardsf.glb'),export_format='GLB',use_selection=True,export_yup=True,export_apply=False,export_texcoords=True,export_normals=True,export_materials='EXPORT',export_cameras=False,export_lights=False,export_extras=True) # Make the runtime paint and glass contracts explicit in the GLB JSON. p=ROOT/'interceptor-hardsf.glb';raw=p.read_bytes();jl,jt=struct.unpack_from(' # Author and critic loop for a Blender asset Use this for any authored asset that will be judged by eye: a hero prop, a character, a building, an environment. Skip it for a mechanical re-export. ## Seats | Seat | Who | Owns | | --- | --- | --- | | Author | Astra (operator law: Blender work goes to Astra) | Geometry, authored materials, UVs, bakes, Blender renders, the export | | Runtime | The root, or one worker when the shader work is real | Loading the export in the game's actual three.js path, captures, measured costs | | Critic | A different model family from the author, reading the real images | Findings only. Never edits the asset | The critic must open the actual capture files. A critic that cannot read images says so and returns BLOCKED; it never writes a visual verdict from metrics or from the author's description. ## Budget - Default: **3 revisions, at most 2 critic passes per revision.** The brief may set another cap. - A cap is an execution limit, not acceptance. Cap reached with open visual findings = `REVISE` reported as such, never a `PASS`. - No unattended improvement loop past the cap. ## Before the first render Write in the task folder: scope, target cameras (gameplay view, hero, rear, closest required view), output paths, budgets (triangles, exported vertices, texture bytes and GPU memory, draw calls) and the revision cap. Budgets are task inputs; do not copy another asset's numbers. Run the [preflight](preflight-and-recovery.md) once: Blender starts and runs a scene operation, a tiny bake and export round-trips through the real loader, one real runtime frame is captured. Integrate a cheap LOW blockout in the runtime at this stage. Scale, axis, camera and material contract problems are found before an expensive bake, not after. ## Each revision keeps - the source revision or parameters that rebuild the previous asset; - real hero, rear and close-up captures, same camera, light, exposure and pose every time; - triangles, exported vertices, primitives, material count, file bytes, texture GPU memory; - runtime draw counters, kept apart from offline estimates; - the critic's findings, the fixes chosen, and the next measured result. ## The critic pass The critic receives the previous AND the current captures and metrics under matched cameras (or an explicit "first revision, no baseline"), the reference image, and the brief. It returns: - **at most five findings**, ordered by impact, each with a stable id, the evidence path (whole view plus crop or image coordinates), the visible symptom, a suggested correction and a **measurable acceptance condition**; - regressions against the previous revision; - resolved / remaining / regressed status of earlier findings on a follow-up pass; - `PASS`, `REVISE` or `BLOCKED`, with the limits of its evidence. It compares against the reference as well as the previous revision: clean topology and progress since last time do not make the asset match the reference. It separates the observed defect from the suspected cause. A small whole-image difference can hide severe local damage (thin trim, stairs, silhouette edges): it inspects crops at each delivered LOD. Design ideas are suggestions, not new acceptance requirements. When the cause could be the asset or the renderer, it asks for the diagnostic captures in [runtime parity](runtime-parity-and-diagnostics.md) (maps off, AO neutral, lightmap off) rather than guessing. ## Rules that stop false passes - A generated concept image is never proof of a working model. Label concepts as concepts; accept only on real renders of the real export. - Requested bakes need bake provenance (what was baked, from what, at what settings) and matched runtime captures with each contribution switched off in turn. Vertex tint and runtime shadows are not substitutes for a requested AO or lightmap bake. - An atlas repair is checked on the full matched views, not only on the crop that was broken: a new layout can fix one edge and turn another face black. - One writer per handoff file. A reply never gets appended to a request file another agent will regenerate. Superseded manifests and failed captures stay on disk. - The author hands the root a compact result: verdict, the few decisive images, the metrics table. Full capture sets stay on disk; the root does not load every image. - A user's rejection or a changed brief reopens any earlier `PASS`. ## Lessons When a revision teaches something that will recur, write it as: evidence path, symptom, cause, intervention, matched before/after result, scope. The root checks it and makes a narrow edit to this skill. Reject task-specific style preferences dressed up as general rules. hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/textures/Paint_Base.png /tmp/interceptor-runtime/Paint_Base.png' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 892ms: hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'command -v geminix' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: /home/claude-agent/bin/geminix hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/textures/metal_plate_diff_1k.jpg /tmp/interceptor-runtime/metal.jpg' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 exec /bin/bash -lc "timeout 220 geminix 'Read-only visual critique. Use image tools to actually open /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg and /tmp/interceptor-final-r2.png plus /tmp/interceptor-runtime/side.png and /tmp/interceptor-runtime/cockpit.png. Compare also /tmp/interceptor-final-r1.png. This is a 16m hard-SF military game asset with 6.5m deployed radiators; budget 90k tris, 12MB. Default Paint factor must remain .55,.56,.55 light grey. Give at most five specific findings and visual acceptance conditions, identify resolved or remaining earlier issues. Current author already plans to reduce canopy/spine height to align with engine rim and tanks, close small triangular gap at windshield foot, strengthen neutral baked wear. Do not edit files or delegate. Return PASS or REVISE from images.' > /tmp/interceptor-critic-r2.txt" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 810ms: hook: PreToolUse hook: PreToolUse Completed codex The side view confirms the canopy sits too high relative to the engine and tanks. I’m lowering it to match the sheet’s profile, closing the windscreen seam, and adding more visible wear to the neutral paint texture so the hull still recolours cleanly. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 - <<'PY' import json p=json.load(open('/tmp/interceptor-polyhaven-catalog.json')) for k,v in p.items(): if any(t in k for t in ['metal','painted']): print(k,v.get('name')) PY" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: black_painted_planks Black Painted Planks blue_metal_plate Blue Metal Plate blue_painted_planks Blue Painted Planks box_profile_metal_sheet Box Profile Metal Sheet concrete_floor_painted Concrete Floor Painted distressed_painted_planks Distressed Painted Planks green_metal_rust Green Metal Rust metal_grate_rusty Metal Grate Rusty metal_plate Metal Plate metal_plate_02 Metal Plate 02 painted_brick Painted Brick painted_concrete Painted Concrete painted_concrete_02 Painted Concrete 02 painted_metal_shutter Painted Metal Shutter painted_plaster_wall Painted Plaster Wall painted_worn_brick Painted Worn Brick peeling_painted_wall Peeling Painted Wall rusty_metal Rusty Metal rusty_metal_02 Rusty Metal 02 rusty_metal_03 Rusty Metal 03 rusty_metal_04 Rusty Metal 04 rusty_metal_05 Rusty Metal 05 rusty_metal_grid Rusty Metal Grid rusty_metal_sheet Rusty Metal Sheet rusty_metal_shutter Rusty Metal Shutter rusty_painted_metal Rusty Painted Metal hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/textures/metal_plate_02_diff_1k.jpg /tmp/interceptor-runtime/metal02.jpg' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 920ms: hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'cp build_interceptor-hardsf.py /tmp/interceptor-build-r3-before.py cat /tmp/interceptor-critic-r2.txt' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: **Verdict: REVISE** ### Resolved vs. Remaining Issues (R1 to R2) * **Resolved in R2 ([interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) vs. [interceptor-final-r2.png](file:///tmp/interceptor-final-r2.png)):** * **Forward side intake opened:** R1 had a flat, grated surface box; R2 cuts a deep recessed intake tunnel closer to [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg). * **Canopy sill sealed:** R1 had a large open gap along the lower side edge of the glass frame; R2 adds a stepped sill plate that closes the side seam. * **Propellant tank domes reshaped:** R1 had pointed, pinched front tank caps with an exposed mounting tab; R2 uses fuller hemispherical domes. * **Panel seams and fasteners added:** Forward fuselage plates and rivets are much clearer in R2. * **Remaining from R1 (including author's planned fixes not yet in R2):** * **Triangular hole at windshield foot** is still open in [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png) (author plans to close). * **Towering canopy and dorsal spine** still sit way above the propellant tanks and engine bell rim in [side.png](file:///tmp/interceptor-runtime/side.png) (author plans to lower). * **Clean, toy-like hull shading** lacks surface breakup and edge wear while keeping the `.55, .56, .55` light grey paint factor (author plans to strengthen neutral baked wear). --- ### Top 5 Specific Findings & Visual Acceptance Conditions 1. **Overall Length-to-Height Proportions & Nose Taper ([side.png](file:///tmp/interceptor-runtime/side.png) vs. [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg))** * **Finding:** Even after lowering the canopy and spine, the hull body is too stubby and thick vertically, and the nose ends in a tall, blunt octagonal block instead of a long, low, needle-like wedge. The main engine bell is also oversized vertically (taller than the entire mid-fuselage). * **Acceptance Condition:** In side view, the fuselage length-to-height ratio matches [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg) (sleek 16m:4.2m profile). The nose tapers continuously into a sharp, low-profile chisel above the railgun, and the engine nozzle outer rim aligns with the top and bottom tank tangent lines. 2. **Canopy Frame Geometry & Glazing Continuity ([cockpit.png](file:///tmp/interceptor-runtime/cockpit.png))** * **Finding:** The canopy frame is built from disconnected cylinder bars ("pipe-frame" look) that protrude past the glass, with visible ball succeeded in 45671ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed apply patch patch: completed /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..8c68258b17cea3a3c0a280327bffd849b8590f03 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -136,8 +136,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +185,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +229,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -248,7 +248,7 @@ hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -320,7 +320,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,7 +328,7 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) @@ -346,7 +346,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.36,.43,.11),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +366,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +386,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +402,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.042,'Alloy',12,'Canopy') for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.043,'Alloy',12,'Canopy') for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +440,16 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint',bevel=.025) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +479,12 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +beacon=sphere('Dorsal beacon',(0,2.24,1.64),(.09,.15,.06),'Lamps',segs=16,rings=8) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +502,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..8c68258b17cea3a3c0a280327bffd849b8590f03 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -136,8 +136,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +185,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +229,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -248,7 +248,7 @@ hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -320,7 +320,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,7 +328,7 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) @@ -346,7 +346,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.36,.43,.11),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +366,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +386,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +402,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.042,'Alloy',12,'Canopy') for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.043,'Alloy',12,'Canopy') for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +440,16 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint',bevel=.025) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +479,12 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +beacon=sphere('Dorsal beacon',(0,2.24,1.64),(.09,.15,.06),'Lamps',segs=16,rings=8) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +502,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'cat /tmp/interceptor-critic-r2.txt' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: **Verdict: REVISE** ### Resolved vs. Remaining Issues (R1 to R2) * **Resolved in R2 ([interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png) vs. [interceptor-final-r2.png](file:///tmp/interceptor-final-r2.png)):** * **Forward side intake opened:** R1 had a flat, grated surface box; R2 cuts a deep recessed intake tunnel closer to [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg). * **Canopy sill sealed:** R1 had a large open gap along the lower side edge of the glass frame; R2 adds a stepped sill plate that closes the side seam. * **Propellant tank domes reshaped:** R1 had pointed, pinched front tank caps with an exposed mounting tab; R2 uses fuller hemispherical domes. * **Panel seams and fasteners added:** Forward fuselage plates and rivets are much clearer in R2. * **Remaining from R1 (including author's planned fixes not yet in R2):** * **Triangular hole at windshield foot** is still open in [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png) (author plans to close). * **Towering canopy and dorsal spine** still sit way above the propellant tanks and engine bell rim in [side.png](file:///tmp/interceptor-runtime/side.png) (author plans to lower). * **Clean, toy-like hull shading** lacks surface breakup and edge wear while keeping the `.55, .56, .55` light grey paint factor (author plans to strengthen neutral baked wear). --- ### Top 5 Specific Findings & Visual Acceptance Conditions 1. **Overall Length-to-Height Proportions & Nose Taper ([side.png](file:///tmp/interceptor-runtime/side.png) vs. [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg))** * **Finding:** Even after lowering the canopy and spine, the hull body is too stubby and thick vertically, and the nose ends in a tall, blunt octagonal block instead of a long, low, needle-like wedge. The main engine bell is also oversized vertically (taller than the entire mid-fuselage). * **Acceptance Condition:** In side view, the fuselage length-to-height ratio matches [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg) (sleek 16m:4.2m profile). The nose tapers continuously into a sharp, low-profile chisel above the railgun, and the engine nozzle outer rim aligns with the top and bottom tank tangent lines. 2. **Canopy Frame Geometry & Glazing Continuity ([cockpit.png](file:///tmp/interceptor-runtime/cockpit.png))** * **Finding:** The canopy frame is built from disconnected cylinder bars ("pipe-frame" look) that protrude past the glass, with visible ball-joint overlaps at vertices, an open triangular hole at the front foot, and a flat rectangular sill slab tacked onto the hull side. * **Acceptance Condition:** Canopy struts are flush, flat-faced armored mullions integrated smoothly into the surrounding hull skin; the front triangular gap is sealed flush with the nose deck; the stepped slab under the sill is faired smoothly into the chine. 3. **Forward Side Intake Cowl Shading & Shape ([cockpit.png](file:///tmp/interceptor-runtime/cockpit.png) & [side.png](file:///tmp/interceptor-runtime/side.png))** * **Finding:** The intake cutout has sharp vertical/horizontal shading pinch artifacts (normal smoothing tearing at the upper and lower corners of the lip) and a paper-thin outer lip, rather than the thick, chamfered trapezoidal intake scoop in [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg). * **Acceptance Condition:** Zero normal-shading creases or dark diagonal triangles around the intake mouth; the intake lip has thick, beveled structural walls with clean hard-edge/weighted-normal transitions. 4. **Nose Railgun Proportion, Mounting, and Barrel Detail ([interceptor-final-r2.png](file:///tmp/interceptor-final-r2.png) & [side.png](file:///tmp/interceptor-runtime/side.png))** * **Finding:** The chin railgun is too short, thin, and boxy, sticking out of the nose tip like a small peg rather than slung under a long ventral fairing with heavy twin rails and perforated barrel shrouds. * **Acceptance Condition:** The ventral gun pod starts well back under the forward fuselage chine and extends past the nose tip with clear upper/lower rail separation, barrel vents, and a solid armoured housing matching the side profile in [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg). 5. **Dorsal Spine Greebles & Propellant Tank Integration ([interceptor-final-r2.png](file:///tmp/interceptor-final-r2.png) & [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png))** * **Finding:** The glowing orange egg-shaped blob on the spine and the two floating saucer-like discs look like untextured primitives, and the propellant tanks sit on top of the hull like bare shiny cylinders rather than recessed into sculpted fairings with heat-scorched domes. * **Acceptance Condition:** Remove or replace the orange egg primitive with flush hard-SF access hatches matching [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg); seat the propellant tanks into contoured hull cradles with darker heat-scorched metallic wear on the end domes and collar rings, while keeping the main hull paint at `.55, .56, .55` light grey with stronger neutral baked AO/dirt/edge wear. --- 0. **Blocked on you**: nothing. 1. **What you changed**: Nothing; this was a read-only visual inspection. 2. **How you know it works**: Inspected [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg), [interceptor-final-r1.png](file:///tmp/interceptor-final-r1.png), [interceptor-final-r2.png](file:///tmp/interceptor-final-r2.png), [side.png](file:///tmp/interceptor-runtime/side.png), and [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png) directly with the image viewer tool. 3. **What would break if you were wrong**: Passing the model now would ship an interceptor with visible mesh gaps at the windshield base, shading artifacts around the intake, pipe-frame canopy bars, and stubby proportions that miss the concept sheet. 4. **What you did NOT do**: Did not inspect the `.glb` geometry, triangle count, or file size directly since this was an image-only critique. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed apply patch patch: completed /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..a0b97c22ff60089c5e06cc50c647c9066920aa6d --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -320,7 +329,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,7 +337,7 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) @@ -346,7 +355,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.36,.43,.11),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +375,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +395,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +411,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +449,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +490,12 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +beacon=sphere('Dorsal beacon',(0,2.24,1.64),(.09,.15,.06),'Lamps',segs=16,rings=8) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +513,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +537,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'python3 -m py_compile build_interceptor-hardsf.py scp build_interceptor-hardsf.py gex44:/root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 1105ms: diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..a0b97c22ff60089c5e06cc50c647c9066920aa6d --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -320,7 +329,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,7 +337,7 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) @@ -346,7 +355,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.36,.43,.11),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +375,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +395,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +411,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +449,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +490,12 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +beacon=sphere('Dorsal beacon',(0,2.24,1.64),(.09,.15,.06),'Lamps',segs=16,rings=8) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +513,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +537,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed apply patch patch: completed /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'python3 -m py_compile build_interceptor-hardsf.py scp build_interceptor-hardsf.py gex44:/root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 828ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'nohup /root/blender-spike/blender-5.2.0-linux-x64/blender -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py > /root/fal-author/interceptor-hardsf-v1/evidence/build.log 2>&1 < /dev/null & echo "'$!'"'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 507ms: 3904414 hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'cat /tmp/interceptor-runtime/index.html cat /tmp/interceptor-runtime/capture.mjs' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: import {chromium} from 'playwright';import fs from 'fs'; const browser=await chromium.launch({headless:true,executablePath:'/home/claude-agent/.cache/ms-playwright/chromium-1223/chrome-linux/chrome',args:['--no-sandbox','--use-angle=swiftshader','--enable-unsafe-swiftshader']});const page=await browser.newPage({viewport:{width:1600,height:900}});let errors=[];page.on('pageerror',e=>errors.push(String(e)));await page.goto('http://127.0.0.1:8347/');await page.waitForFunction(()=>window.done,{timeout:60000});await page.screenshot({path:'/tmp/interceptor-runtime/runtime.png'});fs.writeFileSync('/tmp/interceptor-runtime/runtime.json',JSON.stringify({...await page.evaluate(()=>window.result),errors},null,2));await browser.close(); exec /bin/bash -lc 'df -h / ls -lh' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 exec /bin/bash -lc 'cat /home/claude-agent/.agents/skills/blender-game-assets/scripts/audit_glb.py | head -n 100' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: Filesystem Size Used Avail Use% Mounted on /dev/sda1 150G 137G 7.4G 95% / total 1.1M -rw-rw-r-- 1 claude-agent claude-agent 7.1K Oct 16 18:39 PROMPT.txt drwxrwxr-x 2 claude-agent claude-agent 4.0K Oct 16 19:00 __pycache__ -rw-rw-r-- 1 claude-agent claude-agent 374K Oct 16 19:00 astra.log -rw-rw-r-- 1 claude-agent claude-agent 42K Oct 16 19:00 build_interceptor-hardsf.py -rw-rw-r-- 1 claude-agent claude-agent 4.9K Oct 16 18:37 job.json -rw-rw-r-- 1 claude-agent claude-agent 644K Oct 16 18:34 sheet.jpg -rw-rw-r-- 1 claude-agent claude-agent 1.1K Oct 16 18:37 sheet_prompt.txt -rw-rw-r-- 1 claude-agent claude-agent 21 Oct 16 18:39 started.txt succeeded in 0ms: """Read-only audit of uncompressed GLB triangle meshes; requires numpy. Report mode exits 0 even with findings. --strict exits 1 for findings. Invalid or unsupported input exits 2. This is not a complete glTF validator. """ import argparse import hashlib import json from pathlib import Path import struct import sys import numpy as np def audit(path): data = Path(path).read_bytes() if len(data) < 20 or struct.unpack_from('<4sII', data) != (b'glTF', 2, len(data)): raise ValueError('Invalid GLB v2 header/length') chunks = {} offset = 12 while offset < len(data): if offset + 8 > len(data): raise ValueError('Truncated chunk header') length, kind = struct.unpack_from(' len(data) or kind in chunks: raise ValueError('Invalid, duplicate or truncated GLB chunk') chunks[kind] = data[offset:offset + length] offset += length g = json.loads(chunks[0x4E4F534A]) binary = chunks.get(0x004E4942, b'') compressed = {'KHR_draco_mesh_compression', 'EXT_meshopt_compression'} if compressed.intersection(g.get('extensionsUsed', []) + g.get('extensionsRequired', [])): raise ValueError('Compressed geometry: audit the uncompressed export') buffers = g.get('buffers', []) if len(buffers) != 1 or 'uri' in buffers[0] or buffers[0]['byteLength'] > len(binary): raise ValueError('Expected one embedded geometry buffer') dtypes = {5120: 'i1', 5121: 'u1', 5122: ' v['byteLength'] or base + v['byteLength'] > buffers[0]['byteLength']: raise ValueError('Accessor exceeds declared buffer bounds') return np.ndarray((count, width), dtype=dtype, buffer=binary, offset=base + start, strides=(stride, dtype.itemsize)) rows = [] for mi, mesh in enumerate(g.get('meshes', [])): for pi, primitive in enumerate(mesh['primitives']): if primitive.get('mode', 4) != 4 or primitive.get('targets') or 'KHR_draco_mesh_compression' in primitive.get('extensions', {}): raise ValueError('Only uncompressed TRIANGLES without morph targets supported') attrs = {name: accessor(i) for name, i in primitive['attributes'].items()} pos = attrs['POSITION'] if pos.shape[1] != 3 or g['accessors'][primitive['attributes']['POSITION']].get('normalized'): raise ValueError('Expected non-normalized VEC3 positions') idx = np.arange(len(pos)) if 'indices' in primitive: q = g['accessors'][primitive['indices']] if q['type'] != 'SCALAR' or q['componentType'] not in (5121, 5123, 5125): raise ValueError('Invalid index accessor') idx = accessor(primitive['indices']).ravel() if len(idx) % 3 or (len(idx) and int(idx.max()) >= len(pos)): raise ValueError('Invalid triangle indices') t = pos[idx.reshape(-1, 3)].astype(np.float64) area2 = np.linalg.norm(np.cross(t[:, 1] - t[:, 0], t[:, 2] - t[:, 0]), axis=1) rows.append({'mesh': mesh.get('name', str(mi)), 'primitive': pi, 'triangles': len(idx) // 3, 'zero_area_triangles': int((area2 < 1e-12).sum()), 'nonfinite_attribute_components': sum(int((~np.isfinite(a)).sum()) for a in attrs.values())}) if not rows: raise ValueError('No triangle primitives to audit') # Rig report and duplicate-primitive detection (2026-09-21, after the MengTo rejection gates): # duplicate = two primitives whose POSITION and index buffers hash identically (an action file # carrying a second render mesh); the rig report lists skins, joint names and their parents. seen, duplicates = {}, [] for mi, mesh in enumerate(g.get('meshes', [])): for pi, primitive in enumerate(mesh['primitives']): key = hashlib.sha1(accessor(primitive['attributes']['POSITION']).tobytes() + (accessor(primitive['indices']).tobytes() if 'indices' in primitive else b'')).hexdigest() here = f"{mesh.get('name', str(mi))}[{pi}]" if key in seen: duplicates.append({'primitive': here, 'same_as': seen[key]}) else: seen[key] = here nodes = g.get('nodes', []) parent_of = {} diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 8 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 406ms: Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:197: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "cat > /tmp/interceptor-runtime/contract.py <<'PY' import json,struct,io,sys,hashlib from pathlib import Path from PIL import Image p=Path(sys.argv[1]);b=p.read_bytes();n=struct.unpack_from('3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. codex The next build is baking and rendering now. It includes the lower canopy, flatter armour frames, a sealed forward sill, thicker cheek recess walls, and heat-darkened tank ends. The hinge test also keeps the canopy and radiators attached when each rotates 30 degrees. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 - <<'PY' p='/tmp/interceptor-runtime/index.html' s=open(p).read();s=s.replace('window.done=true;','''const originals=new Map([...materials.values()].map(m=>[m,{map:m.map,normalMap:m.normalMap,aoMap:m.aoMap,roughnessMap:m.roughnessMap,metalnessMap:m.metalnessMap}])); window.setMode=(mode)=>{for(const [m,orig]of originals){Object.assign(m,orig);if(mode==='normal_off')m.normalMap=null;if(mode==='ao_off')m.aoMap=null;if(mode==='maps_off'){m.map=null;m.normalMap=null;m.aoMap=null;m.roughnessMap=null;m.metalnessMap=null;}m.needsUpdate=true;}renderer.render(scene,camera)};window.done=true;''');open(p,'w').write(s) p='/tmp/interceptor-runtime/capture.mjs';s=open(p).read();s=s.replace('await browser.close();',\"\"\"for(const mode of ['normal_off','ao_off','maps_off']){await page.evaluate(m=>window.setMode(m),mode);await page.screenshot({path:'/tmp/interceptor-runtime/runtime_'+mode+'.png'});}await page.evaluate(()=>{window.setMode('default');window.setPaint([.055,.105,.19])});await page.screenshot({path:'/tmp/interceptor-runtime/runtime_navy.png'});await browser.close();\"\"\");open(p,'w').write(s) PY" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 14 /root/fal-author/interceptor-hardsf-v1/evidence/build.log; ps -eo pid,etime,pcpu,args | grep -F interceptor-hardsf-v1 | grep -v grep'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 510ms: Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Heatshield Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:197: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha 3904414 01:02 0.0 python3 /opt/gpu-gate/gpu_gate.py --name blender --need-mib 6000 --priority batch -- /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3904418 01:02 159 /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 12 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 497ms: Info: Baking map saved to internal image, save it externally or pack it BAKED Heatshield Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:197: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 14 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 515ms: Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Heatshield Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:197: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "du -sh /tmp/interceptor-runtime sed -n '118,200p' /home/claude-agent/.agents/skills/blender-game-assets/scripts/audit_glb.py" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: 59M /tmp/interceptor-runtime 'duplicate_primitives': duplicates, 'skins': skins, 'node_names': sorted(n for n in node_names if n), 'note': 'Mesh-local counts, before node transforms/instances. Degenerate threshold: cross-product magnitude < 1e-12 in asset units squared. Not a source-topology or visual-quality verdict.'} for key in ['triangles', 'zero_area_triangles', 'nonfinite_attribute_components']: result[key] = sum(r[key] for r in rows) result['findings'] = [key for key in ['zero_area_triangles', 'nonfinite_attribute_components', 'external_uris', 'duplicate_primitives'] if result[key]] if any(sk['flat_pivot_list'] for sk in skins): result['findings'].append('flat_pivot_list_rig') return result def main(): parser = argparse.ArgumentParser(description=__doc__) parser.add_argument('glb', type=Path) parser.add_argument('--strict', action='store_true') parser.add_argument('--rig', action='store_true', help='print the skin/joint report (always computed; this only keeps it in the output)') parser.add_argument('--require-sockets', default='', help='comma-separated node names that must exist (e.g. target,ground,vfx-hit,vfx-death)') args = parser.parse_args() try: result = audit(args.glb) required = [x.strip() for x in args.require_sockets.split(',') if x.strip()] missing = [x for x in required if x not in result['node_names']] if missing: result['missing_sockets'] = missing result['findings'].append('missing_sockets') if not args.rig: result.pop('skins', None); result.pop('node_names', None) except (ValueError, KeyError, IndexError, TypeError, OSError, struct.error) as exc: print(json.dumps({'status': 'unsupported_or_invalid', 'error': str(exc)})) return 2 print(json.dumps(result, indent=2)) return 1 if args.strict and result['findings'] else 0 if __name__ == '__main__': sys.exit(main()) diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 18 /root/fal-author/interceptor-hardsf-v1/evidence/build.log; ps -eo pid,etime,pcpu,args | grep -F interceptor-hardsf-v1 | grep -v grep'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 601ms: Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Alloy Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Heatshield Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:197: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha 3904414 01:53 0.0 python3 /opt/gpu-gate/gpu_gate.py --name blender --need-mib 6000 --priority batch -- /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3904418 01:53 156 /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 20 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 513ms: 21:02:46 | WARNING: More than one shader node tex image used for a texture. The resulting glTF sampler will behave like the first shader node tex image. 21:02:46 | WARNING: More than one shader node tex image used for a texture. The resulting glTF sampler will behave like the first shader node tex image. 21:02:46 | WARNING: More than one shader node tex image used for a texture. The resulting glTF sampler will behave like the first shader node tex image. 21:02:46 | WARNING: More than one shader node tex image used for a texture. The resulting glTF sampler will behave like the first shader node tex image. 21:02:46 | WARNING: More than one shader node tex image used for a texture. The resulting glTF sampler will behave like the first shader node tex image. 21:02:46 | INFO: Primitives created: 8 21:02:46 | INFO: Extracting primitive: Forward laminated glass end 21:02:46 | INFO: Primitives created: 3 21:02:46 | INFO: Extracting primitive: Radiator cassette 21:02:46 | INFO: Primitives created: 3 21:02:46 | INFO: Extracting primitive: Radiator cassette.005 21:02:46 | INFO: Primitives created: 3 21:02:46 | INFO: Finished glTF 2.0 export in 0.21162629127502441 s Info: Saved as "interceptor.blend" FIRST_GLB_COMPLETE 123.9 8416212 02:16.119 render | Saved: '/root/fal-author/interceptor-hardsf-v1/final.png' 02:27.371 render | Saved: '/root/fal-author/interceptor-hardsf-v1/side.png' 02:33.174 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/rear.png' 02:39.527 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/cockpit.png' diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/final.png /tmp/interceptor-final-r3.png scp gex44:/root/fal-author/interceptor-hardsf-v1/side.png gex44:/root/fal-author/interceptor-hardsf-v1/evidence/cockpit.png /tmp/interceptor-runtime/' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 5000ms: hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..00a7e1f540c8200c93152ecfdceabe90b534e7fb --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,8 +142,8 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) @@ -185,7 +191,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +235,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +252,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -280,10 +289,22 @@ cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +341,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +349,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +370,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +390,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.66 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +410,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +426,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +464,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +505,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +529,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.66));socket('Seat_Copilot',(0,-.65,.66));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +553,15 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. codex The lower profile now follows the sheet much more closely, and the windscreen gap is closed. This render exposed two smaller defects: triangulated shading on the armour and a headrest touching the glass. I’m correcting those before checking the exported asset. ERROR: Reconnecting... 2/5 ERROR: Reconnecting... 3/5 ERROR: Reconnecting... 4/5 ERROR: Reconnecting... 5/5 warning: Falling back from WebSockets to HTTPS transport. stream disconnected before completion: websocket closed by server before response.completed hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "cp build_interceptor-hardsf.py /tmp/interceptor-build-r3.py ssh gex44 'tail -n 3 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 706ms: BUILD_COMPLETE 175.3 87996 8416212 Blender quit hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed apply patch patch: completed /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..8cbee6a268e18d71f1e66a77c7100be54ae35e60 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,21 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'python3 -m py_compile build_interceptor-hardsf.py scp build_interceptor-hardsf.py gex44:/root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 994ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'nohup /root/blender-spike/blender-5.2.0-linux-x64/blender -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py > /root/fal-author/interceptor-hardsf-v1/evidence/build.log 2>&1 < /dev/null & echo "'$!'"'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 528ms: 3928806 diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..8cbee6a268e18d71f1e66a77c7100be54ae35e60 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,21 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/interceptor-hardsf.glb /tmp/interceptor-runtime/interceptor-hardsf.glb python3 /tmp/interceptor-runtime/contract.py /tmp/interceptor-runtime/interceptor-hardsf.glb > /tmp/interceptor-contract-r3.json python3 /home/claude-agent/.agents/skills/blender-game-assets/scripts/audit_glb.py /tmp/interceptor-runtime/interceptor-hardsf.glb --strict > /tmp/interceptor-audit-r3.json' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 exited 1 in 1864ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 - <<'PY' import json for p in ['/tmp/interceptor-contract-r3.json','/tmp/interceptor-audit-r3.json']: d=json.load(open(p)); print(p,{k:v for k,v in d.items()if k in ['verdict','triangles','exported_vertices','primitives','image_gpu_mib_rgba8_with_mips','issues','findings','zero_area_triangles','nonfinite_attribute_components']}) PY" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: /tmp/interceptor-contract-r3.json {'verdict': 'PASS', 'triangles': 87996, 'exported_vertices': 91505, 'primitives': 17, 'image_gpu_mib_rgba8_with_mips': 60.19, 'issues': []} /tmp/interceptor-audit-r3.json {'primitives': [{'mesh': 'Forward laminated glass end', 'primitive': 0, 'triangles': 146, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Forward laminated glass end', 'primitive': 1, 'triangles': 1446, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Forward laminated glass end', 'primitive': 2, 'triangles': 2796, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Radiator cassette', 'primitive': 0, 'triangles': 432, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Radiator cassette', 'primitive': 1, 'triangles': 2740, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Radiator cassette', 'primitive': 2, 'triangles': 1600, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Radiator cassette.005', 'primitive': 0, 'triangles': 452, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Radiator cassette.005', 'primitive': 1, 'triangles': 2720, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Radiator cassette.005', 'primitive': 2, 'triangles': 1600, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Continuous pressure hull', 'primitive': 0, 'triangles': 6980, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Continuous pressure hull', 'primitive': 1, 'triangles': 40906, 'zero_area_triangles': 8, 'nonfinite_attribute_components': 0}, {'mesh': 'Continuous pressure hull', 'primitive': 2, 'triangles': 3556, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Continuous pressure hull', 'primitive': 3, 'triangles': 168, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Continuous pressure hull', 'primitive': 4, 'triangles': 1414, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Continuous pressure hull', 'primitive': 5, 'triangles': 19076, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Continuous pressure hull', 'primitive': 6, 'triangles': 516, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}, {'mesh': 'Continuous pressure hull', 'primitive': 7, 'triangles': 1448, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0}], 'triangles': 87996, 'zero_area_triangles': 8, 'nonfinite_attribute_components': 0, 'findings': ['zero_area_triangles']} diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..8cbee6a268e18d71f1e66a77c7100be54ae35e60 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,21 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'ps -eo pid,ppid,etime,args | grep -F interceptor-hardsf-v1 | grep -v grep'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 559ms: 3928806 1 00:53 python3 /opt/gpu-gate/gpu_gate.py --name blender --need-mib 6000 --priority batch -- /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed apply patch patch: completed /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..14634426e2b49025f222ca142a8e94a256da811e --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,7 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) -print('GEOMETRY',triangles,'triangles',flush=True) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) + print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. world=bpy.data.worlds.new('Deep space');world.use_nodes=True;sc.world=world diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..14634426e2b49025f222ca142a8e94a256da811e --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,7 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) -print('GEOMETRY',triangles,'triangles',flush=True) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) + print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. world=bpy.data.worlds.new('Deep space');world.use_nodes=True;sc.world=world hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "sed -n '566,603p' build_interceptor-hardsf.py ssh gex44 'tail -n 4 /root/fal-author/interceptor-hardsf-v1/evidence/build.log; kill -TERM 3928806'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 473ms: bpy.context.view_layer.update() # Rebuild normals after boolean cuts AND final budget reduction. Large armour planes # use area-weighted normals; smooth round components retain their continuous highlights. for o in OBJECTS.values(): import bmesh bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') bm.to_mesh(o.data);bm.free() for p in o.data.polygons:p.use_smooth=True o.data.set_sharp_from_angle(angle=math.radians(35)) active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. world=bpy.data.worlds.new('Deep space');world.use_nodes=True;sc.world=world nt=world.node_tree;nt.nodes.clear();N=nt.nodes;L=nt.links out=N.new('ShaderNodeOutputWorld');bg=N.new('ShaderNodeBackground');bg.inputs['Strength'].default_value=.24 coord=N.new('ShaderNodeTexCoord');sep=N.new('ShaderNodeSeparateXYZ');L.new(coord.outputs['Normal'],sep.inputs[0]);r=N.new('ShaderNodeValToRGB');r.color_ramp.elements[0].position=0;r.color_ramp.elements[0].color=(.003,.006,.014,1);r.color_ramp.elements[1].position=1;r.color_ramp.elements[1].color=(.025,.043,.075,1);L.new(sep.outputs['Z'],r.inputs[0]);L.new(r.outputs[0],bg.inputs[0]);L.new(bg.outputs[0],out.inputs[0]) def area(name,loc,power,color,size,target=(0,0,0)): d=bpy.data.lights.new(name,'AREA');d.energy=power;d.color=color;d.shape='DISK';d.size=size;o=bpy.data.objects.new(name,d);sc.collection.objects.link(o);o.location=loc;o.rotation_euler=(Vector(target)-o.location).to_track_quat('-Z','Y').to_euler() area('Upper front white key',(3,-8,12),2500,(1,.97,.92),7) area('Cool soft fill',(-8,-1,6),1800,(.64,.78,1),8) area('Engine rim',(1,9,8),2900,(.72,.83,1),6) area('Soft belly fill',(3,-2,-6),700,(.66,.73,1),6) sun=bpy.data.lights.new('Sunlight','SUN');sun.energy=1.2;sun.angle=.08;sun.color=(1,.98,.95);so=bpy.data.objects.new('Sunlight',sun);sc.collection.objects.link(so);so.rotation_euler=(.4,-.5,-.4) camd=bpy.data.cameras.new('Evidence camera');cam=bpy.data.objects.new('Evidence camera',camd);sc.collection.objects.link(cam);sc.camera=cam HERO=(15,-22,14) def camera(loc,target=(0,0,.1),ortho=19.0): cam.location=loc;cam.rotation_euler=(Vector(target)-cam.location).to_track_quat('-Z','Y').to_euler();camd.type='ORTHO';camd.ortho_scale=ortho camera(HERO) def render(path,w=1920,h=1080,samples=48): sc.render.resolution_x=w;sc.render.resolution_y=h;sc.cycles.samples=samples;sc.render.filepath=str(path);bpy.ops.render.render(write_still=True) # First a clay gate with all silhouette geometry visible. clay=special('_Clay',(.32,.34,.36),.15,.42) sc.view_layers[0].material_override=clay render(ROOT/'clay.png',1920,1080,24) sc.view_layers[0].material_override=None # Save and export the first complete asset before final evidence renders. diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..14634426e2b49025f222ca142a8e94a256da811e --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,7 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) -print('GEOMETRY',triangles,'triangles',flush=True) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) + print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. world=bpy.data.worlds.new('Deep space');world.use_nodes=True;sc.world=world hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed apply patch patch: completed /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 -m py_compile build_interceptor-hardsf.py scp build_interceptor-hardsf.py gex44:/root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py ssh gex44 'ps -eo pid,etime,args | grep -F interceptor-hardsf-v1 | grep -v grep'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 exited 1 in 1496ms: diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'nohup /root/blender-spike/blender-5.2.0-linux-x64/blender -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py > /root/fal-author/interceptor-hardsf-v1/evidence/build.log 2>&1 < /dev/null & echo "'$!'"'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 565ms: 3936768 hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 6 /root/fal-author/interceptor-hardsf-v1/evidence/build.log; ps -eo pid,etime,pcpu,args | grep -F interceptor-hardsf-v1 | grep -v grep'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 618ms: Info: Baking map saved to internal image, save it externally or pack it BAKED Heatshield Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator 3936768 00:33 0.0 python3 /opt/gpu-gate/gpu_gate.py --name blender --need-mib 6000 --priority batch -- /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py 3938587 00:08 118 /root/blender-spike/blender-5.2.0-linux-x64/blender.real -b --python-exit-code 1 --python /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'node /tmp/interceptor-runtime/capture.mjs' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. codex The export checks pass for size, materials, textures, sockets, and paint factors. The geometry audit found eight tiny collapsed triangles left by mesh reduction; the final build now removes those and rebuilds the surface normals afterward. hook: PreToolUse hook: PreToolUse Completed 2026-10-16T19:08:13.247221Z ERROR codex_core::tools::router: error=unable to locate image at `/tmp/interceptor-runtime/runtime_normal_off.png`: No such file or directory (os error 2) diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 10 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 507ms: Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Radiator Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:198: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha succeeded in 43885ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'ls -l /tmp/interceptor-runtime/runtime*.png' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: -rw-rw-r-- 1 claude-agent claude-agent 449179 Oct 16 19:08 /tmp/interceptor-runtime/runtime.png -rw-rw-r-- 1 claude-agent claude-agent 447671 Oct 16 19:08 /tmp/interceptor-runtime/runtime_ao_off.png -rw-rw-r-- 1 claude-agent claude-agent 250308 Oct 16 19:08 /tmp/interceptor-runtime/runtime_maps_off.png -rw-rw-r-- 1 claude-agent claude-agent 451767 Oct 16 19:08 /tmp/interceptor-runtime/runtime_navy.png -rw-rw-r-- 1 claude-agent claude-agent 442566 Oct 16 19:08 /tmp/interceptor-runtime/runtime_normal_off.png diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'cat /tmp/interceptor-runtime/runtime.json' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: { "bounds": { "min": [ -3.2505887746810913, -2.031895160675049, -7.9951887130737305 ], "max": [ 3.2494107484817505, 2.168104648590088, 8.004810333251953 ], "size": [ 6.499999523162842, 4.199999809265137, 15.999999046325684 ] }, "drawCalls": 19, "triangles": 88310, "meshes": 17, "materials": [ "Paint", "Alloy", "Cockpit", "Glass", "Radiator", "Heatshield", "Lamps", "Engines" ], "webgl": "WebGL 2.0 (OpenGL ES 3.0 Chromium)", "paintFactor": [ 0.55, 0.56, 0.55 ], "errors": [] } diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 18 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 497ms: Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it BAKED Cockpit /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:198: DeprecationWarning: 'Material.use_nodes' is expected to be removed in Blender 6.0 m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it Info: Baking map saved to internal image, save it externally or pack it GEOMETRY 87989 triangles /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py:581: DeprecationWarning: 'World.use_nodes' is expected to be removed in Blender 6.0 world=bpy.data.worlds.new('Deep space');world.use_nodes=True;sc.world=world diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. codex The GLB loads in Three.js without browser errors at the required dimensions. It uses 19 draw calls, and changing the paint factor leaves the tanks, glazing, weapons, and lights independent. I’m checking the final render set and the six-colour proof next. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 10 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 511ms: 21:09:48 | INFO: Extracting primitive: Forward laminated glass end 21:09:48 | INFO: Primitives created: 3 21:09:48 | INFO: Extracting primitive: Radiator cassette 21:09:48 | INFO: Primitives created: 3 21:09:48 | INFO: Extracting primitive: Radiator cassette.005 21:09:48 | INFO: Primitives created: 3 21:09:48 | INFO: Finished glTF 2.0 export in 0.2317047119140625 s Info: Saved as "interceptor.blend" FIRST_GLB_COMPLETE 118.7 8782724 hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/interceptor-hardsf.glb /tmp/interceptor-runtime/interceptor-hardsf.glb python3 /tmp/interceptor-runtime/contract.py /tmp/interceptor-runtime/interceptor-hardsf.glb > /tmp/interceptor-contract-final.json python3 /home/claude-agent/.agents/skills/blender-game-assets/scripts/audit_glb.py /tmp/interceptor-runtime/interceptor-hardsf.glb --strict > /tmp/interceptor-audit-final.json' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 1878ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 - <<'PY' import json for p in ['/tmp/interceptor-contract-final.json','/tmp/interceptor-audit-final.json']: d=json.load(open(p)); print(p,{k:v for k,v in d.items()if k in ['verdict','triangles','exported_vertices','image_gpu_mib_rgba8_with_mips','issues','findings','zero_area_triangles','nonfinite_attribute_components']}) PY" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: /tmp/interceptor-contract-final.json {'verdict': 'PASS', 'triangles': 87989, 'exported_vertices': 90269, 'image_gpu_mib_rgba8_with_mips': 60.19, 'issues': []} /tmp/interceptor-audit-final.json {'triangles': 87989, 'zero_area_triangles': 0, 'nonfinite_attribute_components': 0, 'findings': []} hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'node /tmp/interceptor-runtime/capture.mjs' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/final.png /tmp/interceptor-final-r4.png scp gex44:/root/fal-author/interceptor-hardsf-v1/side.png /tmp/interceptor-runtime/side.png' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 2075ms: hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "ssh gex44 'tail -n 12 /root/fal-author/interceptor-hardsf-v1/evidence/build.log'" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 485ms: 02:23.160 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/rear.png' 02:30.150 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/cockpit.png' 02:37.534 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/pivot_test.png' 02:39.145 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Naval_grey.png' 02:40.903 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Gunmetal.png' 02:44.189 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Olive_drab.png' 02:47.145 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Desert_sand.png' 02:49.170 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Arctic_white.png' 02:51.185 render | Saved: '/root/fal-author/interceptor-hardsf-v1/evidence/paint_Deep_navy.png' BUILD_COMPLETE 170.8 87989 8782724 Blender quit hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/side.png gex44:/root/fal-author/interceptor-hardsf-v1/clay.png gex44:/root/fal-author/interceptor-hardsf-v1/evidence/cockpit.png gex44:/root/fal-author/interceptor-hardsf-v1/evidence/rear.png /tmp/interceptor-runtime/' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 4063ms: hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "timeout 220 geminix 'Independent image-only final review. Open the actual images: /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg, /tmp/interceptor-final-r4.png, /tmp/interceptor-runtime/side.png, /tmp/interceptor-runtime/cockpit.png, /tmp/interceptor-runtime/rear.png. Compare previous /tmp/interceptor-final-r3.png. A 16m hard-SF interceptor, mandatory light-grey Paint factor .55,.56,.55, radiators deployed, original detailed nose/engine allowed. Current audit is 87989 triangles, 8 materials, 8.78MB, 30 semantic nodes, 1024px colour/normal 512 ORM. Review actual visible construction and silhouette, previous triangle shading, glazing clipping and seam gaps, photographic materials. State resolved and remaining issues, at most five, with concrete image evidence. Return PASS, REVISE or BLOCKED; distinguish required corrections from optional refinements. Do not edit, delegate or invoke other agents.' > /tmp/interceptor-critic-final.txt" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. succeeded in 49046ms: exited 143 in 16367ms: context compacted hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'scp gex44:/root/fal-author/interceptor-hardsf-v1/paints.png /tmp/interceptor-runtime/paints.png && scp gex44:/root/fal-author/interceptor-hardsf-v1/evidence/pivot_test.png /tmp/interceptor-runtime/pivot_test.png' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 2006ms: hook: PreToolUse hook: PreToolUse Completed diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'cat /tmp/interceptor-critic-final.txt' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: **Verdict: PASS** The r4 build ([interceptor-final-r4.png](file:///tmp/interceptor-final-r4.png), [side.png](file:///tmp/interceptor-runtime/side.png), [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png), [rear.png](file:///tmp/interceptor-runtime/rear.png)) resolves the geometry, shading, and material defects from [interceptor-final-r3.png](file:///tmp/interceptor-final-r3.png) while meeting all audit and brief rules (16m hard-SF interceptor, `.55, .56, .55` light-grey paint, deployed radiators, allowed custom nose and engine detail). ### Resolved and Remaining Issues (Max 5) | # | Status | Severity | Evidence & Finding | | :--- | :--- | :--- | :--- | | 1 | **Resolved** | Was Required | **Hull & nose triangle faceting removed:** In [interceptor-final-r3.png](file:///tmp/interceptor-final-r3.png), the forward nose and cheek panels showed harsh diagonal triangle shading and a sharp upward chine spike beside the windshield. In [interceptor-final-r4.png](file:///tmp/interceptor-final-r4.png) and [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png), the hull shading is smooth and the stray chine spike is gone. | | 2 | **Resolved** | Was Required | **Photographic metals and mandatory light-grey paint:** In [interceptor-final-r3.png](file:///tmp/interceptor-final-r3.png), tank domes, radiators, and engine bell had a flat brown tint. In [interceptor-final-r4.png](file:///tmp/interceptor-final-r4.png) and [rear.png](file:///tmp/interceptor-runtime/rear.png), the propellant tanks read as brushed steel with weathered domes, the nozzle reads as dark ribbed alloy, and the hull carries the `.55, .56, .55` light-grey paint with panel seams and fasteners. | | 3 | **Remaining** | Optional refinement | **Cockpit floor cutouts / bright cyan show-through:** In [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png) and [interceptor-final-r4.png](file:///tmp/interceptor-final-r4.png), looking down through the front and lower-side glass panes shows bright cyan-tinted gaps around the seat bases where the cockpit tub floor does not fully block the inner glazing reflection, plus a small step gap between the segmented side sill blocks below the canopy frame. | | 4 | **Remaining** | Optional refinement | **Shallow side intake recess and shading gradient:** In [side.png](file:///tmp/interceptor-runtime/side.png) and [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png), the mid-hull intake is a shallow black-filled box with a vertical normal-map shading gradient directly below it, rather than the deeper faired intake ramp in [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg). | | 5 | **Remaining** | Optional refinement | **Dorsal nose plate seam alignment:** In [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png), the four raised dorsal plates just ahead of the front windshield meet in an X-seam where the forward-most plate edge steps slightly above the smooth nose cone contour. | * **Required corrections:** None. * **Optional refinements:** Seal the lower cockpit tub floor to stop bright cyan show-through under the seats, smooth the vertical shading gradient beneath the side intake box, and flush-fit the front dorsal nose plate lip. --- 0. **Blocked on you**: nothing. 1. **What you changed**: Nothing; this was a read-only visual inspection comparing the r4 renders against r3 and the concept sheet. 2. **How you know it works**: Inspected [sheet.jpg](file:///home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1/sheet.jpg), [interceptor-final-r3.png](file:///tmp/interceptor-final-r3.png), [interceptor-final-r4.png](file:///tmp/interceptor-final-r4.png), [side.png](file:///tmp/interceptor-runtime/side.png), [cockpit.png](file:///tmp/interceptor-runtime/cockpit.png), and [rear.png](file:///tmp/interceptor-runtime/rear.png) directly. 3. **What would break if you were wrong**: If the bright cyan patches inside the lower cockpit glass are noticeable in close-up camera shots, the cockpit interior tub would need a darker closed floor mesh. 4. **What you did NOT do**: Did not inspect the GLB mesh or textures directly on disk, and did not edit any files, as instructed for this image-only review. exec /bin/bash -lc 'cat /tmp/interceptor-runtime/runtime.json; cat /tmp/interceptor-contract-final.json; cat /tmp/interceptor-audit-final.json' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: { "bounds": { "min": [ -3.249982476234436, -2.031895160675049, -7.9951887130737305 ], "max": [ 3.2500174045562744, 2.168104648590088, 8.004810333251953 ], "size": [ 6.4999998807907104, 4.199999809265137, 15.999999046325684 ] }, "drawCalls": 19, "triangles": 88303, "meshes": 17, "materials": [ "Paint", "Alloy", "Cockpit", "Glass", "Radiator", "Heatshield", "Lamps", "Engines" ], "webgl": "WebGL 2.0 (OpenGL ES 3.0 Chromium)", "paintFactor": [ 0.55, 0.56, 0.55 ], "errors": [] }{ "file": "interceptor-hardsf.glb", "sha256": "4e553f969f52a7d0b57a30f06d00bd9a0c91b787315986d76d87807d5959b7e1", "verdict": "PASS", "triangles": 87989, "exported_vertices": 90269, "primitives": 17, "image_gpu_mib_rgba8_with_mips": 60.19, "checks": { "triangle_budget": { "pass": true, "detail": 87989 }, "file_budget": { "pass": true, "detail": 8782724 }, "material_budget": { "pass": true, "detail": [ "Glass", "Cockpit", "Alloy", "Radiator", "Heatshield", "Paint", "Lamps", "Engines" ] }, "paint_factor": { "pass": true, "detail": null }, "glass_blend": { "pass": true, "detail": null }, "emissive_contract": { "pass": true, "detail": null }, "no_cameras_lights": { "pass": true, "detail": null }, "named_nodes": { "pass": true, "detail": [ "Camera_Chase", "Canopy", "Hardpoint_1", "Hardpoint_2", "Light_Beacon", "Light_Nav_L", "Light_Nav_R", "Muzzle_1", "Radiator_L", "Radiator_R", "Seat_Copilot", "Seat_Pilot", "Thruster_1", "Thruster_2", "Thruster_3", "Thruster_4", "Thruster_5", "Thruster_6", "Thruster_7", "Thruster_8", "Thruster_9", "Thruster_10", "Thruster_11", "Thruster_12", "Thruster_13", "Thruster_14", "Thruster_15", "Thruster_16", "Thruster_17", "Hull" ] }, "moving_identity_scale": { "pass": true, "detail": null }, "embedded_images": { "pass": true, "detail": null }, "image_limit": { "pass": true, "detail": [ { "name": "Glass_Normal", "size": [ 64, 64 ], "bytes": 412 }, { "name": "Glass_Base", "size": [ 64, 64 ], "bytes": 415 }, { "name": "Glass_ORM", "size": [ 64, 64 ], "bytes": 415 }, { "name": "Cockpit_Normal", "size": [ 1024, 1024 ], "bytes": 328834 }, { "name": "Cockpit_ORM", "size": [ 512, 512 ], "bytes": 311056 }, { "name": "Cockpit_Base", "size": [ 1024, 1024 ], "bytes": 171945 }, { "name": "Alloy_Normal", "size": [ 1024, 1024 ], "bytes": 94136 }, { "name": "Alloy_ORM", "size": [ 512, 512 ], "bytes": 314880 }, { "name": "Alloy_Base", "size": [ 1024, 1024 ], "bytes": 419733 }, { "name": "Radiator_Normal", "size": [ 1024, 1024 ], "bytes": 80950 }, { "name": "Radiator_ORM", "size": [ 512, 512 ], "bytes": 314917 }, { "name": "Radiator_Base", "size": [ 1024, 1024 ], "bytes": 325058 }, { "name": "Heatshield_Normal", "size": [ 1024, 1024 ], "bytes": 67157 }, { "name": "Heatshield_ORM", "size": [ 512, 512 ], "bytes": 314882 }, { "name": "Heatshield_Base", "size": [ 1024, 1024 ], "bytes": 1336709 }, { "name": "Paint_Normal", "size": [ 1024, 1024 ], "bytes": 80950 }, { "name": "Paint_ORM", "size": [ 512, 512 ], "bytes": 314779 }, { "name": "Paint_Base", "size": [ 1024, 1024 ], "bytes": 864611 }, { "name": "Lamps_Base", "size": [ 64, 64 ], "bytes": 441 }, { "name": "Lamps_Normal", "size": [ 64, 64 ], "bytes": 412 }, { "name": "Lamps_ORM", "size": [ 64, 64 ], "bytes": 413 }, { "name": "Engines_Base", "size": [ 64, 64 ], "bytes": 415 }, { "name": "Engines_Normal", "size": [ 64, 64 ], "bytes": 412 }, { "name": "Engines_ORM", "size": [ 64, 64 ], "bytes": 414 } ] }, "Glass_ORM_limit": { "pass": true, "detail": null }, "Cockpit_ORM_limit": { "pass": true, "detail": null }, "Cockpit_AO_limit": { "pass": true, "detail": null }, "Alloy_ORM_limit": { "pass": true, "detail": null }, "Alloy_AO_limit": { "pass": true, "detail": null }, "Radiator_ORM_limit": { "pass": true, "detail": null }, "Radiator_AO_limit": { "pass": true, "detail": null }, "Heatshield_ORM_limit": { "pass": true, "detail": null }, "Heatshield_AO_limit": { "pass": true, "detail": null }, "Paint_ORM_limit": { "pass": true, "detail": null }, "Paint_AO_limit": { "pass": true, "detail": null }, "Lamps_ORM_limit": { "pass": true, "detail": null }, "Engines_ORM_limit": { "pass": true, "detail": null }, "mesh_nodes_only_expected": { "pass": true, "detail": null } }, "issues": [] } { "file": "interceptor-hardsf.glb", "sha256": "4e553f969f52a7d0b57a30f06d00bd9a0c91b787315986d76d87807d5959b7e1", "bytes": 8782724, "primitive_count": 17, "material_count": 8, "embedded_images": 24, "external_uris": [], "primitives": [ { "mesh": "Forward laminated glass end", "primitive": 0, "triangles": 146, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Forward laminated glass end", "primitive": 1, "triangles": 1446, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Forward laminated glass end", "primitive": 2, "triangles": 2768, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Radiator cassette", "primitive": 0, "triangles": 430, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Radiator cassette", "primitive": 1, "triangles": 2714, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Radiator cassette", "primitive": 2, "triangles": 1600, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Radiator cassette.005", "primitive": 0, "triangles": 434, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Radiator cassette.005", "primitive": 1, "triangles": 2710, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Radiator cassette.005", "primitive": 2, "triangles": 1600, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Continuous pressure hull", "primitive": 0, "triangles": 7760, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Continuous pressure hull", "primitive": 1, "triangles": 40692, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Continuous pressure hull", "primitive": 2, "triangles": 3428, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Continuous pressure hull", "primitive": 3, "triangles": 168, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Continuous pressure hull", "primitive": 4, "triangles": 1414, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Continuous pressure hull", "primitive": 5, "triangles": 18746, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Continuous pressure hull", "primitive": 6, "triangles": 510, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 }, { "mesh": "Continuous pressure hull", "primitive": 7, "triangles": 1423, "zero_area_triangles": 0, "nonfinite_attribute_components": 0 } ], "duplicate_primitives": [], "note": "Mesh-local counts, before node transforms/instances. Degenerate threshold: cross-product magnitude < 1e-12 in asset units squared. Not a source-topology or visual-quality verdict.", "triangles": 87989, "zero_area_triangles": 0, "nonfinite_attribute_components": 0, "findings": [] } diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. codex The final asset passes the geometry and export checks: 87,989 triangles, eight materials, and an 8.78 MB GLB. The canopy and radiators stay attached during the 30° pivot test, and all six paint variants work. I’m collecting the final files and validation evidence now. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'rg --files /tmp/interceptor-runtime; tail -75 build_interceptor-hardsf.py' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: /tmp/interceptor-runtime/interceptor-hardsf.glb /tmp/interceptor-runtime/rear.png /tmp/interceptor-runtime/contract.py /tmp/interceptor-runtime/runtime.png /tmp/interceptor-runtime/capture.log /tmp/interceptor-runtime/index.html /tmp/interceptor-runtime/metal02.jpg /tmp/interceptor-runtime/clay.png /tmp/interceptor-runtime/paints.png /tmp/interceptor-runtime/runtime_navy.png 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/tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-component-testing/references/migration.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/SKILL.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/session-management.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/storage-state.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/video-recording.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/playwright-tests.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/tracing.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/running-code.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/pr-attachments.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/request-mocking.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/test-generation.md /tmp/interceptor-runtime/node_modules/playwright-core/lib/tools/skills/playwright-cli/references/element-attributes.md o.data.set_sharp_from_angle(angle=math.radians(35)) active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. world=bpy.data.worlds.new('Deep space');world.use_nodes=True;sc.world=world nt=world.node_tree;nt.nodes.clear();N=nt.nodes;L=nt.links out=N.new('ShaderNodeOutputWorld');bg=N.new('ShaderNodeBackground');bg.inputs['Strength'].default_value=.24 coord=N.new('ShaderNodeTexCoord');sep=N.new('ShaderNodeSeparateXYZ');L.new(coord.outputs['Normal'],sep.inputs[0]);r=N.new('ShaderNodeValToRGB');r.color_ramp.elements[0].position=0;r.color_ramp.elements[0].color=(.003,.006,.014,1);r.color_ramp.elements[1].position=1;r.color_ramp.elements[1].color=(.025,.043,.075,1);L.new(sep.outputs['Z'],r.inputs[0]);L.new(r.outputs[0],bg.inputs[0]);L.new(bg.outputs[0],out.inputs[0]) def area(name,loc,power,color,size,target=(0,0,0)): d=bpy.data.lights.new(name,'AREA');d.energy=power;d.color=color;d.shape='DISK';d.size=size;o=bpy.data.objects.new(name,d);sc.collection.objects.link(o);o.location=loc;o.rotation_euler=(Vector(target)-o.location).to_track_quat('-Z','Y').to_euler() area('Upper front white key',(3,-8,12),2500,(1,.97,.92),7) area('Cool soft fill',(-8,-1,6),1800,(.64,.78,1),8) area('Engine rim',(1,9,8),2900,(.72,.83,1),6) area('Soft belly fill',(3,-2,-6),700,(.66,.73,1),6) sun=bpy.data.lights.new('Sunlight','SUN');sun.energy=1.2;sun.angle=.08;sun.color=(1,.98,.95);so=bpy.data.objects.new('Sunlight',sun);sc.collection.objects.link(so);so.rotation_euler=(.4,-.5,-.4) camd=bpy.data.cameras.new('Evidence camera');cam=bpy.data.objects.new('Evidence camera',camd);sc.collection.objects.link(cam);sc.camera=cam HERO=(15,-22,14) def camera(loc,target=(0,0,.1),ortho=19.0): cam.location=loc;cam.rotation_euler=(Vector(target)-cam.location).to_track_quat('-Z','Y').to_euler();camd.type='ORTHO';camd.ortho_scale=ortho camera(HERO) def render(path,w=1920,h=1080,samples=48): sc.render.resolution_x=w;sc.render.resolution_y=h;sc.cycles.samples=samples;sc.render.filepath=str(path);bpy.ops.render.render(write_still=True) # First a clay gate with all silhouette geometry visible. clay=special('_Clay',(.32,.34,.36),.15,.42) sc.view_layers[0].material_override=clay render(ROOT/'clay.png',1920,1080,24) sc.view_layers[0].material_override=None # Save and export the first complete asset before final evidence renders. paint=MATS['Paint'];pnt=paint.node_tree;bs=pnt.nodes.get('Principled BSDF');tint=pnt.nodes['Faction paint factor'];base=next(n for n in pnt.nodes if n.type=='TEX_IMAGE' and n.image.name=='Paint_Base') pnt.links.new(base.outputs[0],bs.inputs['Base Color']) bpy.ops.object.select_all(action='DESELECT') for o in sc.objects: if o.type in ['MESH','EMPTY']:o.select_set(True) bpy.ops.export_scene.gltf(filepath=str(ROOT/'interceptor-hardsf.glb'),export_format='GLB',use_selection=True,export_yup=True,export_apply=False,export_texcoords=True,export_normals=True,export_materials='EXPORT',export_cameras=False,export_lights=False,export_extras=True) # Make the runtime paint and glass contracts explicit in the GLB JSON. p=ROOT/'interceptor-hardsf.glb';raw=p.read_bytes();jl,jt=struct.unpack_from('3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 - <<'PY' from pathlib import Path import subprocess, shutil root=Path.cwd(); ev=root/'evidence'; ev.mkdir(exist_ok=True) remote='gex44:/root/fal-author/interceptor-hardsf-v1/' for name in ['interceptor-hardsf.glb','final.png','side.png','clay.png','paints.png','nodes.json','NOTES.md']: subprocess.run(['scp',remote+name,str(root/name)],check=True) for name in ['bake_provenance.json','build.log','pivot_test.png','cockpit.png','rear.png']: subprocess.run(['scp',remote+'evidence/'+name,str(ev/name)],check=True) for src,dst in [('/tmp/interceptor-contract-final.json','contract_audit.json'),('/tmp/interceptor-audit-final.json','geometry_audit.json'),('/tmp/interceptor-critic-final.txt','visual_review.md')]: shutil.copy2(src,ev/dst) for name in ['runtime.json','runtime.png','runtime_navy.png','runtime_normal_off.png','runtime_ao_off.png','runtime_maps_off.png']: shutil.copy2(Path('/tmp/interceptor-runtime')/name,ev/name) print('All requested deliverables and final evidence copied.') PY" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc 'sha256sum build_interceptor-hardsf.py; ssh gex44 sha256sum /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py; df -h /' in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 562ms: 1d84788053f180dd4f6b84d91709787b9325e1401aa36f8f96e7c5fb16ea4a9e build_interceptor-hardsf.py 1d84788053f180dd4f6b84d91709787b9325e1401aa36f8f96e7c5fb16ea4a9e /root/fal-author/interceptor-hardsf-v1/build_interceptor-hardsf.py Filesystem Size Used Avail Use% Mounted on /dev/sda1 150G 138G 6.5G 96% / diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. succeeded in 12318ms: All requested deliverables and final evidence copied. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 - <<'PY' from pathlib import Path import json, struct, hashlib, math from PIL import Image import numpy as np root=Path.cwd(); raw=(root/'interceptor-hardsf.glb').read_bytes(); jl=struct.unpack_from('1e-4:errs.append([n['name'],delta]) assert entry['parent']==(g['nodes'][parents[i]]['name'] if i in parents else None) assert not errs,errs assert len(m['nodes'])==len(g['nodes'])==30 assert len((root/'NOTES.md').read_text().splitlines())==6 assert len(m['paints'])==6 assert m['paints'][0]['linear_rgb']==[.55,.56,.55] assert set(m['axes'])=={'Canopy','Radiator_L','Radiator_R'} for axis in m['axes'].values(): assert abs(sum(x*x for x in axis)-1)<1e-8 runtime=json.loads((root/'evidence/runtime.json').read_text()) assert max(abs(a-b) for a,b in zip(runtime['bounds']['size'],[6.5,4.2,16]))<2e-5 assert max(abs(a-b) for key in ['min','max'] for a,b in zip(runtime['bounds'][key],m['bounding_box'][key]))<2e-5 out={'verdict':'PASS','node_count':30,'manifest_world_positions_match_glb':True,'dimensions_xyz_metres':runtime['bounds']['size'],'notes_lines':6,'script_sha256':hashlib.sha256((root/'build_interceptor-hardsf.py').read_bytes()).hexdigest(),'glb_sha256':hashlib.sha256(raw).hexdigest(),'renders':{}} for name in ['final.png','side.png','clay.png','paints.png']: with Image.open(root/name) as im: size=im.size;im.verify() out['renders'][name]=list(size) assert size==((1920,720) if name=='paints.png' else (1920,1080)) (root/'evidence/delivery_check.json').write_text(json.dumps(out,indent=2)+'\\n') print(json.dumps(out,indent=2)) print((root/'NOTES.md').read_text()) PY" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 202ms: { "verdict": "PASS", "node_count": 30, "manifest_world_positions_match_glb": true, "dimensions_xyz_metres": [ 6.4999998807907104, 4.199999809265137, 15.999999046325684 ], "notes_lines": 6, "script_sha256": "1d84788053f180dd4f6b84d91709787b9325e1401aa36f8f96e7c5fb16ea4a9e", "glb_sha256": "4e553f969f52a7d0b57a30f06d00bd9a0c91b787315986d76d87807d5959b7e1", "renders": { "final.png": [ 1920, 1080 ], "side.png": [ 1920, 1080 ], "clay.png": [ 1920, 1080 ], "paints.png": [ 1920, 720 ] } } Original 16.0 × 6.5 × 4.2 m hard-SF tandem interceptor; hinged canopy, deployed radiators, railgun, four RCS quads and fusion bell. 87,989 triangles; fixed Hull and three moving mesh nodes; Y up, +Z nose; metre scale. 8 materials: Paint, Alloy, Heatshield, Radiator, Cockpit, Glass, Engines, Lamps. Cycles baked: shared tiling colour/normal 1024 px, ORM 512 px; optical/emissive 64 px; neutral Paint texture × faction factor. CC0 photographic sources: Poly Haven metal_plate and metal_plate_02; https://polyhaven.com/license ; https://polyhaven.com/a/metal_plate ; https://polyhaven.com/a/metal_plate_02 . Reference differences: radiator cassettes are deployed; original cheek armour, twin-rail muzzle and engine framing; no exhaust plume or markings. diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "sed -n '1,80p' build_interceptor-hardsf.py; rg -n 'seed|ROOT|GPU|OPTIX|CUDA|bake|remove' build_interceptor-hardsf.py | head -35; du -sh evidence; rg --files -g '"'!__pycache__/*'"' -g '"'!evidence/*'"' ." in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: """Forge hard-SF interceptor. Blender 5.2, clean-scene build, CC0 tile bakes, GLB and evidence renders. Run: blender -b --python-exit-code 1 --python build_interceptor-hardsf.py Coordinates during authoring: X left, -Y forward, Z up. Export converts to X left, Y up, Z forward. Scope: 16 x 6.5 x 4.2m; 40–90k tris; <=9 mats; 1024 colour/normal, 512 ORM; <=12MB. Views: hero front-left, ortho side, clay, six paints, 30-degree hinge test. Revision cap: 3. """ import bpy, math, os, sys, json, urllib.request, subprocess, struct, time import numpy as np from mathutils import Vector, Matrix from pathlib import Path from math import sin, cos, pi ROOT=Path(__file__).resolve().parent TEX=ROOT/'textures'; TEX.mkdir(exist_ok=True) EVID=ROOT/'evidence'; EVID.mkdir(exist_ok=True) START=time.time() bpy.ops.wm.read_factory_settings(use_empty=True) sc=bpy.context.scene sc.unit_settings.system='METRIC';sc.unit_settings.scale_length=1 sc.render.engine='CYCLES';sc.cycles.device='GPU';sc.cycles.samples=48 prefs=bpy.context.preferences.addons['cycles'].preferences for backend in ['OPTIX','CUDA']: try: prefs.compute_device_type=backend;prefs.get_devices() if any(d.type==backend for d in prefs.devices): for d in prefs.devices:d.use=d.type==backend break except Exception:pass else:raise RuntimeError('CUDA/OptiX GPU required') sc.cycles.use_denoising=True;sc.render.image_settings.file_format='PNG' sc.view_settings.view_transform='AgX' sc.render.resolution_percentage=100 sc.render.film_transparent=False GROUPS={'Hull':[],'Canopy':[],'Radiator_L':[],'Radiator_R':[]} MATS={}; BAKE_LOG=[] def active(o): bpy.ops.object.select_all(action='DESELECT');o.select_set(True);bpy.context.view_layer.objects.active=o def uv_project(o): uv=o.data.uv_layers.new(name='UVMap') if not o.data.uv_layers else o.data.uv_layers.active for f in o.data.polygons: n=f.normal;axis=max(range(3),key=lambda i:abs(n[i]));a,b=([1,2] if axis==0 else [0,2] if axis==1 else [0,1]) for li in f.loop_indices: p=o.data.vertices[o.data.loops[li].vertex_index].co uv.data[li].uv=(p[a]*.57,p[b]*.57) def finish(o,name,mat,group='Hull',bevel=0,smooth=False): o.name=name if mat:o.data.materials.append(MATS[mat] if isinstance(mat,str) else mat) if bevel: active(o);m=o.modifiers.new('Machined edge radii','BEVEL');m.width=bevel;m.segments=2 bpy.ops.object.modifier_apply(modifier=m.name) if smooth: for p in o.data.polygons:p.use_smooth=True else: # Weighted face normals preserve armour planes while letting chamfers catch highlights. active(o) if bevel: for p in o.data.polygons:p.use_smooth=True m=o.modifiers.new('Weighted normals','WEIGHTED_NORMAL');m.keep_sharp=True;m.weight=50 bpy.ops.object.modifier_apply(modifier=m.name) uv_project(o) if mat=='Lamps': for uv in o.data.uv_layers.active.data:uv.uv=(.125,.5) if group:GROUPS[group].append(o) return o def mesh(name,verts,faces,mat,group='Hull',bevel=0,smooth=False): me=bpy.data.meshes.new(name);me.from_pydata(verts,[],faces);me.update() o=bpy.data.objects.new(name,me);sc.collection.objects.link(o) # Make connected surfaces outward-facing. import bmesh bm=bmesh.new();bm.from_mesh(me);bmesh.ops.recalc_face_normals(bm,faces=bm.faces);bm.to_mesh(me);bm.free() return finish(o,name,mat,group,bevel,smooth) def box(name,loc,size,mat='Paint',bevel=.025,group='Hull'): bpy.ops.mesh.primitive_cube_add(size=1,location=loc);o=bpy.context.object o.data.transform(Matrix.Diagonal(Vector((*size,1))));return finish(o,name,mat,group,bevel) def sphere(name,loc,scale,mat='Alloy',group='Hull',segs=32,rings=16): 1:"""Forge hard-SF interceptor. Blender 5.2, clean-scene build, CC0 tile bakes, GLB and evidence renders. 12:ROOT=Path(__file__).resolve().parent 13:TEX=ROOT/'textures'; TEX.mkdir(exist_ok=True) 14:EVID=ROOT/'evidence'; EVID.mkdir(exist_ok=True) 19:sc.render.engine='CYCLES';sc.cycles.device='GPU';sc.cycles.samples=48 21:for backend in ['OPTIX','CUDA']: 28:else:raise RuntimeError('CUDA/OptiX GPU required') 138:def bake_material(name,color,metal,rough,asset='metal_plate',relief=.1,neutral=False): 162: bpy.ops.mesh.primitive_plane_add(size=2,location=(0,0,0));o=bpy.context.object;o.name='Tile bake fixture';o.data.materials.append(m) 165: baked={} 173: active(o);sc.cycles.samples=8;sc.render.bake.margin=8;bpy.ops.object.bake(type=typ) 174: im.filepath_raw=str(TEX/f'{name}_{kind}.png');im.file_format='PNG';im.save();baked[kind]=im 175: bpy.data.objects.remove(o,do_unlink=True) 178: n=N.new('ShaderNodeTexImage');n.image=baked[kind];n.label='Cycles baked shared tile' 192: MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) 195:for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) 202: # Even constant glass and emissive finishes are Cycles baked for portable appearance. 214: baked={} 223: for link in list(emit.inputs['Color'].links):L.remove(link) 226: active(o);sc.cycles.samples=4;bpy.ops.object.bake(type=typ);im.filepath_raw=str(TEX/f'{name}_{kind}.png');im.file_format='PNG';im.save();baked[kind]=im 227: bpy.data.objects.remove(o,do_unlink=True);L.new(bs.outputs[0],out.inputs[0]) 228: for kind,im in baked.items(): 296: bpy.data.objects.remove(cutter,do_unlink=True) 602:render(ROOT/'clay.png',1920,1080,24) 610:bpy.ops.export_scene.gltf(filepath=str(ROOT/'interceptor-hardsf.glb'),export_format='GLB',use_selection=True,export_yup=True,export_apply=False,export_texcoords=True,export_normals=True,export_materials='EXPORT',export_cameras=False,export_lights=False,export_extras=True) 612:p=ROOT/'interceptor-hardsf.glb';raw=p.read_bytes();jl,jt=struct.unpack_from('3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. codex All requested files are now in the job directory. The exported model measures 16.0 × 6.5 × 4.2 m, and all 30 node positions match `nodes.json`. The independent visual review passed; its optional refinements are recorded in `evidence/visual_review.md`. The local disk has about 6.5 GB free. I’m removing the temporary tools I installed for validation. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "rg -n -A 14 -B 3 'handoff|deliver|evidence|Stop|receipt|PASS|release' /home/claude-agent/.agents/skills/blender-game-assets/SKILL.md" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: 30-| --- | --- | 31-| A dense model must become a light one that keeps its look (normal + AO transfer) | [high-to-low baking](reference/high-to-low-baking.md) | 32-| Preparing UVs or a cage, or a bake shows seams, black faces, wrong highlights | [baking and diagnostics](reference/baking-and-diagnostics.md) | 33:| Choosing texture or mesh formats, or the asset is slow to load or heavy in GPU memory (KTX2, WebP, meshopt, Draco) | [asset delivery](reference/asset-delivery.md) | 34-| Before any long bake or scripted export pipeline | [preflight and recovery](reference/preflight-and-recovery.md) | 35-| The asset looks right in Blender and wrong in the game, or the cause could be either | [runtime parity and diagnostics](reference/runtime-parity-and-diagnostics.md) | 36-| The asset will be judged by eye (hero prop, character, building, environment) | [author and critic loop](reference/critic-loop.md) | 37-| Terrain, cliffs or rocks should look weathered (branching gullies and ridges, no simulation) | [terrain erosion](reference/terrain-erosion.md) | 38- 39-These seven are loaded on demand, not by default. Five are ported from vercel-labs/vgpu (see Attribution); terrain erosion uses Rune Skovbo Johansen's filter (MPL 2.0, `scripts/erosion/`). 40- 41-### Choose how to carry each detail before any bake 42- 43-| Detail | Carry it as | 44-| --- | --- | 45-| Silhouette, openings, broad edges, tuft dimples, piping, moving parts | Real low-poly geometry | 46-| Fine bevel curvature and shallow relief the triangle budget cannot afford | Tangent-space normals baked from the dense source | 47-| Permanent cavities and contacts inside a rigid assembly | Baked AO | -- 491-Chimala). Runnable reference code copied under the same license into 492-`reference/` — see `reference/INDEX.md`. 493- 494:`reference/high-to-low-baking.md`, `baking-and-diagnostics.md`, `asset-delivery.md`, 495-`preflight-and-recovery.md` and `runtime-parity-and-diagnostics.md` are ported from 496-vercel-labs/vgpu `skills/vgpu/blender/references/` at commit 68cb1d8d198c (MIT License, 497-Copyright (c) 2025 Vercel, Inc.), adapted from vgpu/WebGPU to the three.js runtime. 498-`reference/critic-loop.md` is distilled from the same repository's asset agent flow. hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed hook: PreToolUse Completed exec /bin/bash -lc "python3 - <<'PY' from pathlib import Path import shutil,json root=Path.cwd() shutil.rmtree(root/'__pycache__',ignore_errors=True) shutil.rmtree(Path('/tmp/interceptor-runtime/node_modules'),ignore_errors=True) print('\\n'.join(f'{p.name}: {p.stat().st_size:,} bytes' for p in sorted(root.iterdir()) if p.is_file() and p.name in ['interceptor-hardsf.glb','build_interceptor-hardsf.py','final.png','side.png','clay.png','paints.png','nodes.json','NOTES.md'])) PY" in /home/claude-agent/forge-build/forge-assets/jobs/interceptor-hardsf-v1 succeeded in 0ms: NOTES.md: 755 bytes build_interceptor-hardsf.py: 43,532 bytes clay.png: 2,338,339 bytes final.png: 2,497,644 bytes interceptor-hardsf.glb: 8,782,724 bytes nodes.json: 8,176 bytes paints.png: 1,473,028 bytes side.png: 2,040,659 bytes diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. hook: PreToolUse hook: PreToolUse Completed mcp: forge/coord_release started mcp: forge/coord_release (completed) hook: PreToolUse hook: PreToolUse Completed mcp: forge/coord_release started mcp: forge/coord_release (completed) diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. codex Delivered all requested files: - [GLB asset](interceptor-hardsf.glb) — 87,989 triangles, 8 materials, 8.78 MB. - [Reproducible Blender script](build_interceptor-hardsf.py). - Renders: [final](final.png), [side](side.png), [clay](clay.png), [six paints](paints.png). - [Node manifest](nodes.json) and [notes/licences](NOTES.md). Verified dimensions, 30° moving-part pivots, recolouring, texture limits, and Three.js loading. Independent visual review passed. Local disk space remaining: approximately 6.5 GB. diff --git a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py index 2eebc493ddb350bd37dd04ec90ebf44188e4d92b..4e1371d3548d965af8c71da7ab0fde3f92044754 --- a/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py +++ b/jobs/interceptor-hardsf-v1/build_interceptor-hardsf.py @@ -88,6 +88,12 @@ o.data.transform(o.rotation_euler.to_matrix().to_4x4());o.rotation_euler=(0,0,0) return finish(o,name,mat,group,bevel,True) +def frame(name,a,b,width=.08,depth=.055,mat='Alloy',group='Canopy'): + a,b=Vector(a),Vector(b);d=b-a + o=box(name,(a+b)/2,(width,depth,d.length+.022),mat,.012,group) + o.data.transform(d.to_track_quat('Z','Y').to_matrix().to_4x4()) + return o + def torus(name,loc,major,minor,mat='Alloy',axis='Y',group='Hull',segs=64): bpy.ops.mesh.primitive_torus_add(major_segments=segs,minor_segments=8,location=loc,major_radius=major,minor_radius=minor) o=bpy.context.object @@ -136,13 +142,14 @@ def tex(k): n=N.new('ShaderNodeTexImage');n.image=PH[asset,k];L.new(uv.outputs['UV'],n.inputs['Vector']);return n diff=tex('diff');normal=tex('nor_gl');arm=tex('arm');bw=N.new('ShaderNodeRGBToBW');L.new(diff.outputs['Color'],bw.inputs[0]) - ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.10;ramp.color_ramp.elements[1].position=.8 - low=.58 if neutral else .62;high=.94 if neutral else 1.15 + ramp=N.new('ShaderNodeValToRGB');ramp.color_ramp.elements[0].position=.035 if neutral else .10;ramp.color_ramp.elements[1].position=.22 if neutral else .8 + low=.52 if neutral else .62;high=.98 if neutral else 1.15 ramp.color_ramp.elements[0].color=tuple(min(1,c*low) for c in color)+(1,) ramp.color_ramp.elements[1].color=tuple(min(1,c*high) for c in color)+(1,) L.new(bw.outputs[0],ramp.inputs[0]) if name=='Heatshield': - ramp.color_ramp.elements[0].color=(.045,.026,.017,1);ramp.color_ramp.elements[1].color=(.14,.18,.25,1) + ramp.color_ramp.elements[0].position=.025;ramp.color_ramp.elements[1].position=.22 + ramp.color_ramp.elements[0].color=(.055,.040,.027,1);ramp.color_ramp.elements[1].color=(.14,.18,.24,1) noise=N.new('ShaderNodeTexNoise');noise.inputs['Scale'].default_value=210;noise.inputs['Detail'].default_value=2;L.new(uv.outputs['UV'],noise.inputs['Vector']) pits=N.new('ShaderNodeValToRGB');pits.color_ramp.elements[0].position=.25;pits.color_ramp.elements[0].color=(.55,.55,.55,1);pits.color_ramp.elements[1].position=.37 @@ -185,7 +192,7 @@ MATS[name]=m;BAKE_LOG.append({'material':name,'device':backend,'samples':8,'base':1024,'normal':1024,'ORM':512,'source':asset,'representation':'shared tiling Cycles EMIT base/ORM and tangent NORMAL bake'}) print('BAKED',name,flush=True) -for args in [('Paint',(1,1,1),.42,.46,'metal_plate',.08,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate',.18,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) +for args in [('Paint',(1,1,1),.60,.37,'metal_plate_02',.12,True),('Alloy',(.40,.43,.46),.88,.28,'metal_plate_02',.15,False),('Heatshield',(.11,.085,.067),.84,.40,'metal_plate_02',.10,False),('Radiator',(.045,.053,.061),.68,.49,'metal_plate_02',.12,False),('Cockpit',(.025,.033,.041),.1,.65,'metal_plate',.08,False)]:bake_material(*args) def special(name,color,metal=0,rough=.3,alpha=1,emission=0): m=bpy.data.materials.new(name);m.use_nodes=True;bs=m.node_tree.nodes.get('Principled BSDF');bs.inputs['Base Color'].default_value=(*color,1);bs.inputs['Metallic'].default_value=metal;bs.inputs['Roughness'].default_value=rough;bs.inputs['Alpha'].default_value=alpha @@ -229,12 +236,12 @@ sep=N.new('ShaderNodeSeparateColor');L.new(n.outputs[0],sep.inputs[0]);L.new(sep.outputs['Green'],bs.inputs['Roughness']);L.new(sep.outputs['Blue'],bs.inputs['Metallic']) BAKE_LOG.append({'material':name,'device':backend,'samples':4,'base':64,'normal':64,'ORM':64,'source':'constant optical finish / emission palette','representation':'Cycles EMIT and tangent NORMAL'}) MATS[name]=m;return m -special('Glass' ,(.19,.30,.36),.18,.14,.30) +special('Glass' ,(.12,.22,.28),.20,.12,.24) special('Engines',(.12,.28,.65),.45,.26,1,1.8) special('Lamps',(.21,.64,.72),.25,.25,1,2) # Main pressure/armour shell; longitudinal stations define the silhouette. -SECTIONS=[(-6.10,.40,-.44,.24),(-5.35,.72,-.65,.63),(-4.25,1.13,-.82,.86),(-2.9,1.55,-.91,1.01),(-1.1,2.02,-1.0,1.13),(.7,2.23,-1.05,1.18),(2.8,2.22,-1.05,1.15),(4.42,1.95,-.91,1.02)] +SECTIONS=[(-6.10,.38,-.38,.10),(-5.35,.72,-.60,.49),(-4.25,1.13,-.82,.79),(-2.9,1.55,-.91,.96),(-1.1,2.02,-1.0,1.07),(.7,2.23,-1.05,1.12),(2.8,2.22,-1.05,1.10),(4.42,1.95,-.91,1.00)] def ring(y,w,bot,top): return [(w*.65,y,top),(-w*.65,y,top),(-w,y,top-.26),(-w,y,bot+.25),(-w*.68,y,bot),(w*.68,y,bot),(w,y,bot+.25),(w,y,top-.26)] vs=[] @@ -246,9 +253,12 @@ fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) fs += [tuple(reversed(range(8))),tuple(range(56,64))] hull_shell=mesh('Continuous pressure hull',vs,fs,'Paint',bevel=.045) +box('Nose sensor bezel',(0,-6.116,-.13),(.51,.048,.26),'Alloy',.045) +box('Recessed nose sensor window',(0,-6.143,-.13),(.40,.018,.16),'Cockpit',.035) +box('Passive optical aperture',(0,-6.155,-.13),(.18,.009,.075),'Glass',.02) # Low armoured dorsal spine behind the cockpit. vs=[] -for s in [(0.65,.83,1.02,2.28),(1.5,.88,1.02,2.25),(3.6,.8,.99,1.91),(4.45,.67,.83,1.43)]:vs+=ring(*s) +for s in [(0.65,.83,1.02,1.68),(1.5,.88,1.02,1.67),(3.6,.8,.99,1.53),(4.45,.67,.83,1.27)]:vs+=ring(*s) fs=[tuple(reversed(range(8))),tuple(range(24,32))] for k in range(3): for j in range(8):fs.append((k*8+j,k*8+(j+1)%8,(k+1)*8+(j+1)%8,(k+1)*8+j)) @@ -268,22 +278,35 @@ # Embedded service hatches on upper shoulder, conforming to the narrowing hull. for y in [.15,1.25,2.5,3.65]: x=sign*1.39 - box('Flush maintenance gasket',(x,y,1.16),(.56,.63,.065),'Cockpit',.065) - box('Armoured maintenance cover',(x,y,1.205),(.51,.58,.055),'Paint',.055) + box('Recessed maintenance cradle',(x,y,1.055),(.56,.63,.18),'Paint',.045) + box('Flush maintenance gasket',(x,y,1.137),(.54,.61,.045),'Cockpit',.045) + box('Armoured maintenance cover',(x,y,1.17),(.51,.58,.055),'Paint',.045) for xx in [-.17,.17]: - for yy in [-.21,.21]:bolt((x+xx,y+yy,1.241),'Z',r=.018) + for yy in [-.21,.21]:bolt((x+xx,y+yy,1.205),'Z',r=.018) # Raised fore shoulder flanks, sculpted as closed angular guards around cooling apertures. - vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.65),(1.7,-2.5,.98),(2.06,-1.0,1.08),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.58),(1.58,-2.5,.85),(1.94,-1.0,.93),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] + vv=[(sign*x,y,z) for x,y,z in [(1.0,-4.45,.55),(1.7,-2.5,.79),(2.06,-1.0,.87),(2.02,-1.0,-.30),(1.62,-2.5,-.4),(1.0,-4.45,-.2),(.9,-4.45,.49),(1.58,-2.5,.70),(1.94,-1.0,.78),(1.90,-1.0,-.21),(1.5,-2.5,-.31),(.9,-4.45,-.13)]] ff=[(0,1,4,5),(1,2,3,4),(6,11,10,7),(7,10,9,8)]+[(i,(i+1)%6,(i+1)%6+6,i+6) for i in range(6)] cheek=mesh('Tapered cheek armour',vv,ff,'Paint',bevel=.04) # A deep, bevelled recessed sensor/thermal bay is cut through both skin layers. cutter=box('Temporary aperture tool',(sign*1.67,-1.87,.37),(1.10,1.33,.66),None,.12,group=None) for target in [hull_shell,cheek]: active(target);mod=target.modifiers.new('Recessed cheek aperture','BOOLEAN');mod.operation='DIFFERENCE';mod.solver='EXACT';mod.object=cutter;bpy.ops.object.modifier_apply(modifier=mod.name) + # Boolean intersection edges must not inherit interpolated pre-cut custom normals. + for p in target.data.polygons:p.use_smooth=False bpy.data.objects.remove(cutter,do_unlink=True) box('Cheek aperture pressure bulkhead',(sign*1.19,-1.87,.37),(.12,1.26,.60),'Cockpit',.065) for j in range(8): box('Recessed cheek heat-exchanger fin',(sign*1.27,-2.38+j*.145,.37),(.075,.035,.48),'Radiator',.008) + # Four substantial sloping walls lead into a pressure-sealed recess. + corners=[(-2.50,.10),(-2.50,.64),(-1.24,.64),(-1.24,.10)] + wall=[] + for depth in [0,1]: + for y,z in corners: + x=1.64+(y+2.50)*.25 if depth==0 else 1.25 + wall.append((sign*x,y,z)) + lining=mesh('Armoured cheek aperture lining',wall,[(0,1,5,4),(1,2,6,5),(2,3,7,6),(3,0,4,7)],'Heatshield') + active(lining);sol=lining.modifiers.new('Recess wall thickness','SOLIDIFY');sol.thickness=.045;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=lining.modifiers.new('Recess wall bevel','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) # Framed opening and surrounding armour remain continuous. for y in [-2.54,-1.20]: x=sign*(1.62 if y<-2 else 1.95) @@ -320,7 +343,7 @@ for z in [-.48,-.61]: tube('Coolant trunk',(sign*2.235,.02,z),(sign*2.235,3.87,z),.026,'Heatshield',10) for y in [.12,1.2,2.3,3.73]:box('Coolant line clamp',(sign*2.24,y,z),(.08,.05,.10),'Alloy',.008) -for y,w,z in [(1.57,.85,2.25),(3.48,.80,1.94)]: +for y,w,z in [(1.57,.85,1.67),(3.48,.80,1.54)]: tube('Dorsal shield panel joint',(-w*.65,y,z+.012),(w*.65,y,z+.012),.014,'Radiator',8) box('Dorsal inspection plate',(0,y-.30,z+.02),(.63,.38,.045),'Paint',.04) for x in [-.24,.24]:bolt((x,y-.30,z+.05),'Z',r=.019) @@ -328,14 +351,17 @@ # Four long cylindrical propellant tanks with domed welded ends and real retaining bands. for sx in [-1,1]: for sz in [-1,1]: - x=sx*1.46;z=1.39 if sz==1 else -1.06 + x=sx*1.46;z=1.20 if sz==1 else -1.06 cap=[] for j in range(13): a=-pi/2+j*pi/24;cap.append((1.28+.49*sin(a),max(.0001,.49*cos(a)))) cap.append((3.52,.49)) for j in range(1,13): a=j*pi/24;cap.append((3.52+.49*sin(a),max(.0001,.49*cos(a)))) - lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank=lathe('Seamless domed propellant vessel',cap,(x,0,z),'Alloy',segments=48) + tank.data.materials.append(MATS['Heatshield']) + for p in tank.data.polygons: + if p.center.y<1.27 or p.center.y>3.53:p.material_index=1 for y in [1.28,3.52]: torus('Tank retaining band',(x,y,z),.497,.038,'Heatshield',segs=48) @@ -346,7 +372,7 @@ torus('Fill cap',(x,1.0,z+sz*.36),.085,.02,'Alloy','Z',segs=24) # Dorsal antenna/sensor covers (no markings). for y in [1.35,3.5]: - sphere('Recessed dorsal sensor',(0,y,2.20 if y<2 else 1.94),(.36,.43,.14),'Alloy',segs=24,rings=12) + sphere('Recessed dorsal sensor',(0,y,1.67 if y<2 else 1.54),(.33,.40,.065),'Alloy',segs=24,rings=12) # Cockpit tub open beneath the transparent hinged canopy. cockpit_start=len(GROUPS['Hull']) @@ -366,9 +392,9 @@ # Instrument panel face sits ahead of each operator. box('Instrument panel',(0,y-.62,1.57),(1.0,.13,.42),'Cockpit',.045) for s in [-1,1]:box('Flight display',(s*.25,y-.695,1.60),(.32,.017,.21),'Lamps',.018) -for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.24 +for o in GROUPS['Hull'][cockpit_start:]:o.location.z-=.80 # Canopy mesh: faceted windscreen and roof with structural bows and rubber seals. -CAN=[(-3.95,.43,1.00,1.13),(-3.0,.66,1.08,1.75),(-1.75,.77,1.14,2.13),(-.50,.79,1.18,2.28),(.72,.77,1.20,2.28)] +CAN=[(-3.95,.43,.92,.99),(-3.0,.66,.98,1.34),(-1.75,.77,1.04,1.57),(-.50,.79,1.08,1.68),(.72,.77,1.10,1.68)] # Fitted solid foredeck and shoulder coaming; actual aperture follows canopy sills. def interp(y,rows): if y<=rows[0][0]:return rows[0][1:] @@ -386,8 +412,11 @@ vv.extend([(sign*w*.65,y,top+.012),(sign*cw,y,cb-.015)]) o=mesh('Fitted cockpit shoulder deck',vv,[(0,1,3,2)],'Paint',bevel=0) active(o);sol=o.modifiers.new('Armour thickness','SOLIDIFY');sol.thickness=.065;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=o.modifiers.new('Coaming edge radius','BEVEL');bev.width=.018;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) for a,b in zip(CAN,CAN[1:]):tube('Fixed cockpit coaming',(sign*a[1],a[0],a[2]-.065),(sign*b[1],b[0],b[2]-.065),.068,'Paint',12) +# Closed forward pressure sill bridges the central triangle before the windscreen. +mesh('Windscreen forward pressure sill',[(0,-4.25,.802),(.43,-3.95,.905),(-.43,-3.95,.905),(0,-4.25,.737),(.43,-3.95,.840),(-.43,-3.95,.840)],[(0,1,2),(5,4,3),(0,3,4,1),(1,4,5,2),(2,5,3,0)],'Paint',bevel=.012) # each station left sill, left roof, right roof, right sill cr=[] for y,w,b,t in CAN:cr.append([(w,y,b),(w*.74,y,t),(-w*.74,y,t),(-w,y,b)]) @@ -399,14 +428,14 @@ active(o);sol=o.modifiers.new('Laminated glass thickness','SOLIDIFY');sol.thickness=.018;bpy.ops.object.modifier_apply(modifier=sol.name) for j in range(4): for k in range(4): - tube('Canopy seal',cr[k][j],cr[k+1][j],.055,'Cockpit',12,'Canopy') - tube('Canopy longitudinal frame',cr[k][j],cr[k+1][j],.037,'Paint',12,'Canopy') + tube('Canopy seal',cr[k][j],cr[k+1][j],.037,'Cockpit',12,'Canopy') + frame('Canopy longitudinal armour',cr[k][j],cr[k+1][j]) for k in range(5): - for j in range(3):tube('Armoured canopy bow',cr[k][j],cr[k][j+1],.052,'Paint',12,'Canopy') + for j in range(3):frame('Armoured canopy bow',cr[k][j],cr[k][j+1],.085,.055) for j in [0,3]:bolt(cr[k][j],'X','Canopy',.022) for s in [-1,1]: - tube('Canopy hinge trunnion',(s*.59,.77,1.27),(s*.82,.77,1.27),.10,'Alloy',24) - tube('Canopy rotary servo',(s*.63,.77,1.27),(s*.88,.77,1.27),.14,'Heatshield',24) + tube('Canopy hinge trunnion',(s*.59,.77,1.17),(s*.82,.77,1.17),.10,'Alloy',24) + tube('Canopy rotary servo',(s*.63,.77,1.17),(s*.88,.77,1.17),.14,'Heatshield',24) # Fusion drive: structural thrust frame, reactor throat, regenerative coolant lines, hollow bell. lathe('Engine pressure chamber',[(4.38,.97),(4.62,1.0),(5.02,.89),(5.25,.60),(5.58,.53)],(0,0,0),'Heatshield',segments=72) @@ -437,13 +466,18 @@ start=len(GROUPS['Hull']);rot=Vector((0,1,0)).rotation_difference(d).to_matrix().to_4x4() lathe('RCS nozzle',[(0,.085),(.18,.117),(.24,.126),(.24,.099),(.08,.05)],(0,0,0),'Heatshield',segments=20) torus('RCS lip',(0,.235,0),.113,.013,'Alloy',segs=20) + lathe('RCS catalyst glow',[(.081,.049),(.082,.001)],(0,0,0),'Engines',segments=20) for o in GROUPS['Hull'][start:]: o.data.transform(rot);o.location=p+rot.to_3x3()@o.location - RCS.append(p+d*.24) + RCS.append((p+d*.24,d)) # Fixed ventral railgun: shroud, twin rails, breech cables and muzzle aperture. box('Railgun breech',(0,-4.85,-.64),(.64,1.72,.53),'Alloy',.10) box('Railgun receiver',(0,-6.08,-.64),(.43,1.40,.34),'Heatshield',.05) for s in [-1,1]: + fair=mesh('Railgun cheek fairing',[(s*x,y,z) for x,y,z in [(.34,-4.5,-.47),(.31,-5.65,-.43),(.24,-6.12,-.54),(.24,-6.12,-.78),(.35,-5.65,-.91),(.40,-4.5,-.91)]],[(0,1,2,3,4,5)],'Paint') + active(fair);sol=fair.modifiers.new('Fairing plate thickness','SOLIDIFY');sol.thickness=.04;bpy.ops.object.modifier_apply(modifier=sol.name) + bev=fair.modifiers.new('Fairing edge radius','BEVEL');bev.width=.015;bev.segments=3;bpy.ops.object.modifier_apply(modifier=bev.name) +for s in [-1,1]: box('Railgun acceleration rail',(s*.12,-6.94,-.64),(.13,2.12,.18),'Alloy',.025) for y in [-6.06,-6.66,-7.25,-7.86]:box('Barrel ceramic isolator',(s*.12,y,-.64),(.16,.08,.22),'Radiator',.012) tube('Breech power bus',(s*.23,-4.1,-.58),(s*.23,-5.95,-.58),.032,'Heatshield',10) @@ -473,12 +507,13 @@ nav=sphere('Navigation lens',(s*2.24,3.72,.69),(.06,.11,.05),'Lamps',segs=16,rings=8) for uv in nav.data.uv_layers.active.data:uv.uv=(.625 if s==1 else .875,.5) box('Retracted ordnance shoe',(s*1.14,.15,-1.04),(.35,.95,.16),'Heatshield',.04) -beacon=sphere('Dorsal beacon',(0,2.24,2.20),(.09,.15,.08),'Lamps',segs=16,rings=8) +box('Beacon bezel',(0,2.24,1.625),(.19,.28,.075),'Alloy',.035) +beacon=box('Dorsal beacon',(0,2.24,1.668),(.12,.21,.025),'Lamps',.012) for uv in beacon.data.uv_layers.active.data:uv.uv=(.375,.5) # Consolidate all rigid assemblies. Keep moving node mesh coordinates relative to the hinge; # never apply transforms to these moving nodes. -PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.27),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} +PIVOTS={'Hull':(0,0,0),'Canopy':(0,.77,1.17),'Radiator_L':(2.16,1.99,.26),'Radiator_R':(-2.16,1.99,.26)} OBJECTS={} for name,objs in GROUPS.items(): bpy.ops.object.select_all(action='DESELECT') @@ -496,11 +531,12 @@ def socket(name,p,parent='Hull'): o=bpy.data.objects.new(name,None);sc.collection.objects.link(o);o.empty_display_size=.18;o.parent=OBJECTS[parent];o.location=Vector(p)-Vector(PIVOTS[parent]);return o socket('Thruster_1',(0,8,0)) -for i,p in enumerate(RCS,2):socket(f'Thruster_{i}',p) +for i,(p,d) in enumerate(RCS,2): + o=socket(f'Thruster_{i}',p);o.rotation_euler=Vector((0,1,0)).rotation_difference(d).to_euler() socket('Muzzle_1',(0,-8.02,-.64)) for i,s in enumerate([1,-1],1):socket(f'Hardpoint_{i}',(s*1.14,-.35,-1.14)) -socket('Seat_Pilot',(0,-2.25,1.05));socket('Seat_Copilot',(0,-.65,1.05));socket('Camera_Chase',(0,12,5.3)) -socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,2.27)) +socket('Seat_Pilot',(0,-2.25,.52));socket('Seat_Copilot',(0,-.65,.52));socket('Camera_Chase',(0,12,5.3)) +socket('Light_Nav_L',(2.25,3.72,.69));socket('Light_Nav_R',(-2.25,3.72,.69));socket('Light_Beacon',(0,2.24,1.70)) # Exact overall dimensions: apply a single coordinate correction to data and node locations, # not object transforms, preserving all hinge frames. bpy.context.view_layer.update() @@ -519,6 +555,26 @@ for o in OBJECTS.values(): active(o);dec=o.modifiers.new('Budget reduction','DECIMATE');dec.ratio=88000/triangles;bpy.ops.object.modifier_apply(modifier=dec.name) triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) +# Final millimetre correction after reduction; moving pivots keep identity scale. +bpy.context.view_layer.update() +pts=[o.matrix_world@v.co for o in OBJECTS.values() for v in o.data.vertices] +lo=Vector([min(p[i] for p in pts) for i in range(3)]);hi=Vector([max(p[i] for p in pts) for i in range(3)]) +F=Vector((6.5/(hi.x-lo.x),16/(hi.y-lo.y),4.2/(hi.z-lo.z)));FM=Matrix.Diagonal(Vector((*F,1))) +for o in list(sc.objects): + if o.type=='MESH':o.data.transform(FM) + o.location=Vector([o.location[i]*F[i] for i in range(3)]) +bpy.context.view_layer.update() +# Rebuild normals after boolean cuts AND final budget reduction. Large armour planes +# use area-weighted normals; smooth round components retain their continuous highlights. +for o in OBJECTS.values(): + import bmesh + bm=bmesh.new();bm.from_mesh(o.data);dead=[f for f in bm.faces if f.calc_area()<1e-8] + if dead:bmesh.ops.delete(bm,geom=dead,context='FACES') + bm.to_mesh(o.data);bm.free() + for p in o.data.polygons:p.use_smooth=True + o.data.set_sharp_from_angle(angle=math.radians(35)) + active(o);wn=o.modifiers.new('Final area weighted shading','WEIGHTED_NORMAL');wn.keep_sharp=True;wn.weight=50;wn.mode='FACE_AREA';bpy.ops.object.modifier_apply(modifier=wn.name) +triangles=sum(len(o.data.polygons) for o in OBJECTS.values()) print('GEOMETRY',triangles,'triangles',flush=True) # Render rig: camera-visible blue gradient, neutral daylight key and cool fill; no ground. tokens used 299,508 Delivered all requested files: - [GLB asset](interceptor-hardsf.glb) — 87,989 triangles, 8 materials, 8.78 MB. - [Reproducible Blender script](build_interceptor-hardsf.py). - Renders: [final](final.png), [side](side.png), [clay](clay.png), [six paints](paints.png). - [Node manifest](nodes.json) and [notes/licences](NOTES.md). Verified dimensions, 30° moving-part pivots, recolouring, texture limits, and Three.js loading. Independent visual review passed. Local disk space remaining: approximately 6.5 GB.