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

Abstract:

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 final state, subject to state constraints. Drawing on recent developments in reachability analysis subject to state constraints, we show that the proposed MOC problem can be stated as an optimization ...

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Publication status:
Published
Peer review status:
Peer reviewed

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Publisher copy:
10.1016/j.ejcon.2022.100758

Authors


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Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
Publisher:
Elsevier
Journal:
European Journal of Control More from this journal
Volume:
69
Article number:
100758
Publication date:
2022-11-17
Acceptance date:
2022-11-06
DOI:
ISSN:
0947-3580
Language:
English
Keywords:
Pubs id:
1300117
Local pid:
pubs:1300117
Deposit date:
2022-11-07

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