This paper studies multi-spacecraft system attitude consensus control with model uncertainty, sensor faults and time-varying input delay. Attitude dynamics of the spacecraft is described using Euler angles. Predictor-based state transformation method is proposed to get delay-free system states with delay information unknown. Afterwards, descriptor observer is used to estimate system states and sensor disturbances. Disturbance attenuation controller is designed based on system state estimates. Finally, a simulation example demonstrates the system performance under the designed algorithm.


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    Titel :

    Attitude Consensus of Multiple Uncertain Spacecraft Systems with Sensor Faults and Input Delay


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Deng, Yimin (Herausgeber:in) / Li, Yunhan (Autor:in) / Xin, Xing (Autor:in) / Wang, Chunyan (Autor:in) / Zheng, Keyu (Autor:in)

    Kongress:

    International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024



    Erscheinungsdatum :

    04.03.2025


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch