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.
Forward–Backward Indirect Shooting for Low- Thrust Trajectories with Interior Events
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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.