Achieving fast and precise attitude synchronization for multiple rigid spacecraft under user-defined constraints, while managing limited communication bandwidth, remains a key challenge. To address these issues, a kind of distributed constrained attitude control scheme is proposed in this article. The approach guarantees attitude synchronization with a leader spacecraft and ensures adherence to predefined attitude constraints. In addition, an event-triggered communication mechanism is incorporated to reduce communication frequency without sacrificing control performance. The global finite-time stability of the closed-loop system is rigorously proven. Simulation results demonstrate the effectiveness of the proposed method over existing control schemes.


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    Titel :

    Event-Triggered Finite-Time Attitude Control for Multiple Rigid Spacecraft With User-Defined Attitude Constraints


    Beteiligte:
    Wang, Linan (Autor:in) / Wen, Guanghui (Autor:in) / Zhou, Jialing (Autor:in) / Zhu, Huatian (Autor:in)


    Erscheinungsdatum :

    01.06.2025


    Format / Umfang :

    6004542 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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