The article proposes a dynamic time-varying event-triggered strategy to achieve semi-global finite-time rendezvous control of saturated spacecraft. The main idea of the designed dynamic event-triggered strategy is to construct the controller that contains the time-varying high-gain and a dynamic event-triggered mechanism simultaneously. Moreover, a positive lower bound of interevent times is obtained by using the properties of the parametric Lyapunov equation, such that the Zeno phenomenon is eliminated. Finally, the designed dynamic time-varying event-triggered strategy is verified by simulation results.


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    Titel :

    Semiglobal Finite-Time Rendezvous Control of Saturated Spacecraft by Dynamic Time-Varying Event-Triggered Strategy


    Beteiligte:
    Zhang, Kai (Autor:in) / Yang, Xuefei (Autor:in) / Hu, Zhijian (Autor:in) / Li, Meilin (Autor:in) / Li, Tieshan (Autor:in)


    Erscheinungsdatum :

    01.04.2025


    Format / Umfang :

    792582 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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