Introduces maximum-initial-mass optimal control problem for low-thrust transfers, establishes correspondence to minimum-time extremals, and applies it to recover global solutions for a GTO-to-GEO benchmark.
Com- puting Low-Thrust Transfers in the Asteroid Belt, a Comparison between Astrodynamical Manipula- tions and a Machine Learning Approach
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The Maximum Initial Mass
Introduces maximum-initial-mass optimal control problem for low-thrust transfers, establishes correspondence to minimum-time extremals, and applies it to recover global solutions for a GTO-to-GEO benchmark.
- Pretrained Approximators for Low-Thrust Trajectory Cost and Reachability
- Reachability for Low-Thrust Trajectories via Maximum Initial Mass