This article investigates the attitude tracking control of state constrained rigid spacecraft systems with external disturbances. An event-triggered adaptive fuzzy asymptotic backstepping tracking controller is proposed, which makes the spacecraft attitude tracking error asymptotically converge to origin in the presence of inertia uncertainty, external disturbance, and full-state constraints. A novel event-triggered mechanism is established to reduce the waste of communication resources caused by frequent controller updating. A simulation example demonstrates the effectiveness of the control method.


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    Titel :

    Event-Triggered Adaptive Fuzzy Asymptotic Tracking Control for Rigid Spacecraft Attitude Systems With Full-State Constraints and Disturbances


    Beteiligte:
    Xu, Zhiguo (Autor:in) / Zhao, Lin (Autor:in)


    Erscheinungsdatum :

    01.08.2024


    Format / Umfang :

    998822 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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