Rendezvous & docking (RVD) include four phases: ground longrang phase, homing phase, approach phase, docking phase. For the optimal rendezvous, most solutions are based on the C-W function. This paper studies the optimal rendezvous solutions which based on the traditional C-W equations, and studies optimal rendezvous solutions which based on the method of nonlinear programming. A recently developed direct optimization technique is employed, which converts the optimal control problem into a nonlinear programming one.


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    Titel :

    The optimal guidance law for rendezvous and docking of spacecraft


    Beteiligte:
    Zhu Lingpu (Autor:in) / Liu Zhenghua (Autor:in) / Wen Nuan (Autor:in)


    Erscheinungsdatum :

    01.08.2016


    Format / Umfang :

    341430 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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