Multi-objective low-thrust spacecraft trajectory design using reachability analysis

One of the fundamental problems in spacecraft trajectory design is finding the optimal transfer trajectory that minimizes the propellant consumption and transfer time simultaneously. We formulate this as a multi-objective optimal control (MOC) problem that involves optimizing over the initial or fin...

Повний опис

Бібліографічні деталі
Автори: Vertovec, N, Ober-Blöbaum, S, Margellos, K
Формат: Journal article
Мова:English
Опубліковано: Elsevier 2022