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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    Title :

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


    Contributors:
    Xu, Zhiguo (author) / Zhao, Lin (author)


    Publication date :

    2024-08-01


    Size :

    998822 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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