Master's Thesis · TU Munich · 2025–2026
Fault-Tolerant Control of Propulsive Spacecraft
- Built a modular Python GNC framework (~23,000 lines) for landing trajectory optimisation and actuator-fault analysis of an Apollo-class lunar lander.
- Designed it as a shared core engine (vehicle and actuator models, optimal-control problem formulation, attainable-moment envelopes) reused by nine self-contained study packages.
- Ran automated fault-injection and fault-onset campaigns across 16 fault modes and multiple initial-condition regimes, with result tables and figures generated automatically.