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...

Description complète

Détails bibliographiques
Auteurs principaux: Vertovec, N, Ober-Blöbaum, S, Margellos, K
Format: Journal article
Langue:English
Publié: Elsevier 2022

Documents similaires