This paper focuses on the fault-tolerant attitude consensus control (FTACC) for a set of satellites with actuator faults. The attitude dynamical models of the satellites are considered as nonlinear systems, suffering from the effects of parameter variations and environmental uncertainties. A fully distributed attitude control protocol is developed without requirement of global information of the networked spacecraft system. Numerical tests and the results of a set of spacecrafts show the effectiveness of the designed fault-tolerant consensus control protocol.


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    Title :

    Distributed Fault-Tolerant Attitude Consensus Control for Multiple Satellites


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Cheng, Ming (author) / Wang, Linbo (author) / Tian, Yu (author) / Liu, Hao (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022



    Publication date :

    2023-01-31


    Size :

    9 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English






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