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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    Title :

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


    Contributors:
    Wang, Linan (author) / Wen, Guanghui (author) / Zhou, Jialing (author) / Zhu, Huatian (author)


    Publication date :

    2025-06-01


    Size :

    6004542 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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