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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Published in | Aerospace science and technology Vol. 133; p. 108099 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Masson SAS
01.02.2023
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Subjects | |
Online Access | Get full text |
ISSN | 1270-9638 1626-3219 |
DOI | 10.1016/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. |
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ISSN: | 1270-9638 1626-3219 |
DOI: | 10.1016/j.ast.2022.108099 |