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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    Title :

    Application of Hill's lunar theory to motion of satellites


    Additional title:

    J Astronautical Sciences


    Contributors:
    Lanzano, P. (author)


    Publication date :

    1961


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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