The application of genetic algorithm is discussed in the problem of minimum-fuel consumption orbit manoeuvre of spacecraft. First, the method of operation is introduced. Two examples are then given: one is soft-landing of a lunar probe from lunar satellite orbit to lunar surface; and the other is orbit manoeuvre of lunar probe from a selenocentric hyperbolic orbit to a selenocentric circular orbit. It is shown that the genetic algorithm has good convergence property and high accuracy.


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    Titel :

    Use of genetic algorithm in optimal orbit manoeuvre


    Beteiligte:
    Guoqiang Zeng, (Autor:in) / Xiaoning Xi, (Autor:in) / Xuan Ren, (Autor:in)


    Erscheinungsdatum :

    01.01.2000


    Format / Umfang :

    356839 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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