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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    Title :

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


    Contributors:
    Guo, Jitang (author) / Chen, Xinlong (author) / Zhu, Mengping (author) / Zhou, Qingrui (author)


    Publication date :

    2022-02-01


    Size :

    4637709 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English