H ↿/sub> inverse optimal adaptive fault-tolerant attitude control for flexible spacecraft with input saturation

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• 作者：Hai-hui Long 龙海輿/a> ; Jian-kang Zhao 赵健帿/a>…
• 关键词：fault ; tolerant ; attitude control ; inverse optimization ; flexible spacecraft ; adaptive control ; input saturation
• 刊名：Journal of Shanghai Jiaotong University (Science)
• 出版年：2015
• 出版时间：October 2015
• 年：2015
• 卷：20
• 期：5
• 页码：513-527
• 全文大小：909 KB
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• 作者单位：Hai-hui Long 龙海辉 (1)
  Jian-kang Zhao 赵健康 (1)
  Jian-qing Lai 赖剑清 (1)
  
  1. Shanghai Key Laboratory of Navigation and Location Based Services, Shanghai Jiaotong University, Shanghai, 200240, China
  
• 刊物类别：Engineering
• 刊物主题：Electrical Engineering
  Life Sciences
  Architecture
  Chinese Library of Science
  
• 出版者：Shanghai Jiao Tong University Press
• ISSN：1995-8188

文摘

An adaptive inverse optimal attitude controller for flexible spacecraft with fault-free actuator is designed based on adaptive control Lyapunov function and inverse optimal methodology subjected to unknown parameter uncertainties, external disturbances and input saturation. The partial loss of actuator effectiveness and the additive faults are considered simultaneously to deal with actuator faults, and the prior knowledge of bounds on the effectiveness factors of the actuators is assumed to be unknown. A fault-tolerant control version is designed to handle the system with actuator fault by introducing a parameter update law to estimate the lower bound of the partial loss of actuator effectiveness faults. The proposed fault-tolerant attitude controller ensures robustness and stabilization, and it achieves H _∞ optimality with respect to a family of cost functionals. The usefulness of the proposed algorithms is assessed and compared with the conventional approaches through numerical simulations.