According to the structural characteristics of satellite formation, and using the kinematic equations which expressed as fly-around form, designed a model for satellite formation configuration, analysed the relationship between fly-around parameters and the orbital elements, designed a method that meets the mission requirements of the satellite formation configuration, formulated a corresponding operation flow chart, listed several typical satellite formations of simple configuration and complex configuration. Finally, according to the general process of configuration design, obtaioned a configuration based on the requirments, and with the help of software STK and Matlab performed a formation configuration simulation that considering collision avoidance verification and adjustment. The simulation results show that the formation configuration design process and design method are basically right.


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    Titel :

    Based on STK and Matlab Satellite Formation's Configuration Design and Simulation


    Beteiligte:
    Dang, Chang-Ping (Autor:in) / Cai, Yuan-Wen (Autor:in) / Le, Tian (Autor:in) / Zhao, Yi-Bin (Autor:in) / Xin, Chao-Jun (Autor:in)


    Erscheinungsdatum :

    2013


    Format / Umfang :

    6 Seiten




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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