Distributed safe trajectory optimization for large-scale spacecraft formation reconfiguration

This paper presents a distributed trajectory optimization algorithm for the reconfiguration of large-scale spacecraft formation, which uses a low thrust propulsion system to safely guide the spacecraft formation to a desired formation. Formation reconfiguration is formulated as a trajectory optimiza...

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Bibliographic Details
Published in:Acta astronautica Vol. 214; pp. 125 - 136
Main Authors: Chen, Junyu, Wu, Baolin, Sun, Zhaobo, Wang, Danwei
Format: Journal Article
Language:English
Published: Elsevier Ltd 01.01.2024
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ISSN:0094-5765
Online Access:Get full text
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