The attitude regulation control of rigid-flexible coupling satellites is investigated in this paper. Firstly a state observer is designed to estimate the vibration speed of the flexible appendage. With the adaptive method used to compensate the disturbance, a predefined-time attitude regulation controller is then proposed, under which the attitude of a rigid-flexible coupling satellite can be drawn to the desired point in predefined time and hold steady. Finally a simulation example is provided to illustrate the effectiveness of the proposed attitude controller.


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    Titel :

    Predefined-Time Adaptive Attitude Regulation Control for Rigid-Flexible Coupling Satellites


    Beteiligte:
    Wang, Yunteng (Autor:in) / He, Huiqun (Autor:in) / Xiao, Yan (Autor:in) / Ye, Dong (Autor:in) / Sun, Zhaowei (Autor:in)


    Erscheinungsdatum :

    27.12.2024


    Format / Umfang :

    1089327 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch