In this paper, using the multiple microspacecrafts to carry out attitude takeover stabilization control for the failed spacecraft is studied in the sense of fully actuated system game-based method. According to the attitude dynamics, the fully-actuated system model of the combined spacecraft is established. And the game-based controller of the fully actuated system is designed for the combined spacecraft attitude control. Finally, numerical simulation indicates the effectiveness of the proposed controller.


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    Titel :

    Fully Actuated System Game-Based Attitude Control for Combined Spacecraft


    Beteiligte:
    Duan, Guang-Quan (Autor:in) / Liu, Guo-Ping (Autor:in)


    Erscheinungsdatum :

    14.07.2023


    Format / Umfang :

    423349 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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