The main purpose of this chapter is to calculate the dynamic characteristics of the flexible spacecraft with time-varying parameters based on the model in the previous chapter, and to obtain the dynamic responses of the spacecraft under typical cases


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    Title :

    Rigid-Flexible Coupling Dynamic Analysis of Flexible Spacecraft


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


    Publication date :

    2021-09-16


    Size :

    23 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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