T-SCvx predicts tight constraints and warm-start solutions with transformers, cutting 6-DoF powered descent guidance solve time by 66% on a Mars landing benchmark.
Propellant-Optimal Powered Descent Guidance,
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Tight Constraint Prediction of Six-Degree-of-Freedom Transformer-based Powered Descent Guidance
T-SCvx predicts tight constraints and warm-start solutions with transformers, cutting 6-DoF powered descent guidance solve time by 66% on a Mars landing benchmark.