In this article, a pyramid-type single-gimbal control moment gyro system mounted on a space structure is employed to realize the integrated control of singularity avoidance attitude maneuver and vibration suppression. The rest-to-rest attitude maneuver is divided into three sections, in which null motion is applied to achieve the above two objects leading to a better control performance. The effectiveness of the proposed control strategy is verified using numerical simulation examples.


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    Titel :

    Integrated Control of Attitude Maneuver and Vibration Suppression Using Pyramid-Type SGCMGs


    Beteiligte:
    Guo, Jitang (Autor:in) / Chen, Xinlong (Autor:in) / Zhu, Mengping (Autor:in) / Zhou, Qingrui (Autor:in)


    Erscheinungsdatum :

    2022-02-01


    Format / Umfang :

    4637709 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch