Constrained multi‐observer‐based fault‐tolerant disturbance‐rejection control for rigid spacecraft

Bailiang Lyu; Xiaokui Yue; Chuang Liu

doi:10.1002/rnc.6270

journal article Jul 10, 2022

Constrained multi‐observer‐based fault‐tolerant disturbance‐rejection control for rigid spacecraft

Bailiang Lyu Xiaokui Yue

Chuang Liu

International Journal of Robust and Nonlinear Control Vol. 32 No. 14 pp. 8102-8133 · Wiley

View at Publisher Save 10.1002/rnc.6270

Abstract

AbstractThis article develops a multi‐observer‐based fault‐tolerant disturbance‐rejection control strategy to solve the attitude stabilization problem of spacecraft subject to multisource complex disturbances, for example, external disturbance, measurement error, actuator fault, input constraint. First, two intermediate variables are introduced for multi‐observer design, so that the synergistic estimations of attitude information, actuator fault and external disturbance are obtained simultaneously. Then, a fault‐tolerant disturbance‐rejection control strategy is proposed based on the estimations, and an augmented closed‐loop system is derived. Afterwards, Lyapunov stability analysis is performed to prove the quadratic stability and robust performance, and corresponding conditions in terms of linear matrix inequalities (LMIs) is proved, where the input constraint is satisfied as well. Finally, numerical simulations of a spacecraft attitude control system are performed which demonstrate the effectiveness and superiority of the proposed multi‐observer‐based control strategy.

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Metrics

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Citations

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References

Details

Published: Jul 10, 2022
Vol/Issue: 32(14)
Pages: 8102-8133
License: View

Authors

B

Bailiang Lyu

School of Astronautics Northwestern Polytechnical University Xi'an China; Research & Development Institute of Northwestern Polytechnical University in Shenzhen Shenzhen China

X

Xiaokui Yue

School of Astronautics Northwestern Polytechnical University Xi'an China; Research & Development Institute of Northwestern Polytechnical University in Shenzhen Shenzhen China

C

Chuang Liu

School of Astronautics Northwestern Polytechnical University Xi'an China; Research & Development Institute of Northwestern Polytechnical University in Shenzhen Shenzhen China

Funding

National Natural Science Foundation of China Award: 62103336

China Postdoctoral Science Foundation Award: 2020M683571

Guangdong Basic and Applied Basic Research Foundation Award: 2021A1515110539

Cite This Article

Bailiang Lyu, Xiaokui Yue, Chuang Liu (2022). Constrained multi‐observer‐based fault‐tolerant disturbance‐rejection control for rigid spacecraft. International Journal of Robust and Nonlinear Control, 32(14), 8102-8133. https://doi.org/10.1002/rnc.6270

Constrained multi‐observer‐based fault‐tolerant disturbance‐rejection control for rigid spacecraft

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