Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation-Reference-Cited by-同舟云学术

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Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation

Published:2021 Issue: Volume: Page:73-108
ISSN:
Container-title:Control Allocation for Spacecraft Under Actuator Faults
language:
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Author:

Hu Qinglei,Li Bo,Xiao Bing,Zhang Youmin

Publisher

Springer Singapore

Link

http://link.springer.com/content/pdf/10.1007/978-981-16-0439-3_5

Reference32 articles.

1. Haj Brahim, I., Chaabane, M., Mehdi,D. (2017) Fault-tolerant control for T-S fuzzy descriptor systems with sensor faults: an lmi approach. International Journal of Fuzzy Systems volume 19: 516–527

2. Yang, G.H., Ye, D. (2008) Adaptive fault-tolerant H$$\infty $$ control against sensor failures. IET Control Theory and Applications 2(2): 95–107

3. Guo,J.X., Tao,G., Liu, Y. (2014) Adaptive actuator failure and structural damage compensation of nasa generic transport model. Journal of Dynamic Systems, Measurement, and Control 136(3): 031009

4. Cai, W.C., Liao, X.H., Song, D.Y. (2008) Indirect robust adaptive fault-tolerant control for attitude tracking of spacecraft. Journal of Guidance, Control, and Dynamics 31(5): 1456–1463

5. Sun, L. (2020) Adaptive fault-tolerant constrained control of cooperative spacecraft rendezvous and docking. IEEE Transactions on Industrial Electronics 67(4): 3107–3115

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Fully-actuated System Approach for Spacecraft Attitude Control with Input Saturation;2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA);2023-07-14

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