The space net is a novel and effective approach in solving the spacecraft capturing problem. In this chapter, the attitude control problem of parent satellite is addressed. At first, the disturbance imposed on the parent satellite is analyzed, and the dynamic process of mass ejection is investigated. In addition, the main factors that affect the performance of the net are analyzed, and based on which, the model of the disturbance torque is developed. At the end of this chapter, the numerical simulations are implemented, and the corresponding results validate the effectiveness of the proposed algorithm.


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    Title :

    Attitude Disturbance and Control of Satellite During Space Net Projecting


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Xing, Song (editor) / Chen, Suting (editor) / Wei, Zhanming (editor) / Xia, Jingming (editor) / Gao, Zhijie (author) / Yang, Dongfang (author) / Sun, Fuchun (author)


    Publication date :

    2013-06-15


    Size :

    9 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English