In Chapter 5, an optimization method for variable amplitude input shaping attitude maneuver was proposed. And in Chapter 6, a coupled control method of attitude control and flexible structure vibration control was proposed for attitude tracking of flexible spacecraft with time-varying parameters


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    Title :

    Rigid-Flexible Coupling Control Experiments


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


    Publication date :

    2021-09-16


    Size :

    14 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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