A fatigue assessment tool for structural monitoring.
Adaptive structural-survivability and SHM research platform for aerospace systems: damage localization, remaining-control-authority analysis, bounded multi-action recovery, resource/uncertainty constraints, executed-command-consistent held-out verification, deterministic replay, HIL campaigns, and a P1 physical-validation path.
DAMOCLES: damage tolerance Monte Carlo life estimation. NASGRO crack growth, Newman-Raju SIFs, inspection planning with POD, and the FAA AC 33.14-1 calibration test case passing the published acceptance bands
Verified LEFM / Paris-law fatigue crack-growth analysis for an idealized aircraft wing skin: finite-width geometry, fracture-toughness boundary, dK threshold, and ordered variable-amplitude block spectrum. Illustrative data, 1213 tests, no runtime dependencies.
A fully local agentic LLM-to-CAD loop for single-material, damage-tolerant bioinspired architectures: Bouligand, woven-lattice and enamel generators, a vision-critic design loop with print certification, and FEA and phase-field fracture verification.
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