Reformulates reachability analysis for low-thrust and solar-sail trajectories as a maximum-initial-mass scalar optimization problem and approximates it with residual neural network surrogates.
Com- puting Low-Thrust Transfers in the Asteroid Belt, a Comparison between Astrodynamical Manipula- tions and a Machine Learning Approach
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Reachability for Low-Thrust Trajectories via Maximum Initial Mass
Reformulates reachability analysis for low-thrust and solar-sail trajectories as a maximum-initial-mass scalar optimization problem and approximates it with residual neural network surrogates.