Using method developed by C.L.Siegel, G.W.Hill's equations are solved to obtain coordinates of periodic trajectory as Fourier series of time with respect to rotating system of reference; numerical example for satellite of Venus error analysis is undertaken by studying solutions of Hill's equations lying in neighborhood of periodic orbit and corresponding to same value of total energy.


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    Titel :

    Application of Hill's lunar theory to motion of satellites


    Weitere Titelangaben:

    J Astronautical Sciences


    Beteiligte:
    Lanzano, P. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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