Disturbance observer-based performance guaranteed fault-tolerant control for multi-spacecraft formation reconfiguration with collision avoidance

In this study, the issue of the performance guaranteed fault-tolerant control for formation reconfiguration with collision avoidance in the multi-spacecraft system subjects to space perturbations and thruster faults is investigated. A new nonlinear iterative learning disturbance observer is construc...

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Bibliographic Details
Published inAerospace science and technology Vol. 133; p. 108099
Main Authors Jia, Qingxian, Gui, Yule, Wu, Yunhua, Zhang, Chengxi
Format Journal Article
LanguageEnglish
Published Elsevier Masson SAS 01.02.2023
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ISSN1270-9638
1626-3219
DOI10.1016/j.ast.2022.108099

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Summary:In this study, the issue of the performance guaranteed fault-tolerant control for formation reconfiguration with collision avoidance in the multi-spacecraft system subjects to space perturbations and thruster faults is investigated. A new nonlinear iterative learning disturbance observer is constructed to accurately reconstruct the synthesized disturbance no matter it is time-varying or not. Then, an exponential artificial potential function with a simple structure and low computation requirement is designed to avoid collision between spacecrafts. A nonsingular terminal sliding mode fault-tolerant control method is explored to accomplish fault-tolerant formation reconfiguration with collision avoidance ability and prescribed robust performance. Finally, numerical simulations and comparisons are performed to validate the effectiveness and superiority of the proposed approaches.
ISSN:1270-9638
1626-3219
DOI:10.1016/j.ast.2022.108099