During the attitude maneuver of the flexible spacecraft, the attitude movement of the spacecraft body will excite the elastic vibration of the flexible attachment [1–3]. In return, the vibration would induce attitude oscillation after maneuver, which will downgrade the performance of payloads in spacecraft.


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    Title :

    Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft


    Contributors:
    Wang, Jie (author) / Li, Dong-Xu (author)


    Publication date :

    2021-09-16


    Size :

    33 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English