For further improving the performances of attitude control methods, vibration controllers for flexible appendages have been introduced and the coupling control method has been developed. The basic idea of the coupling control method is to combine the attitude stabilization theory with a vibration controller. The attitude of the platform and elastic vibrations of flexible appendages are controlled simultaneously.


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    Titel :

    Rigid-Flexible Coupling Control Method for Flexible Spacecraft


    Beteiligte:
    Wang, Jie (Autor:in) / Li, Dong-Xu (Autor:in)


    Erscheinungsdatum :

    16.09.2021


    Format / Umfang :

    32 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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