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.
Rapid Determination of Low-Thrust Spacecraft Reachable Sets in Two-Body and Cislunar Problems,
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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.