Problems relating to influence of perturbations are analyzed by extension of A.Cayley's development of perturbative function in lunar theory; results are modified for incorporation into Hansen-type theory used by NASA Space Computing Center; theory is applied to orbits of Vanguard I and Explorer VI satellites, and results of computations given.


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    Title :

    Development of lunar and solar perturbations in motion of artificial satellite


    Additional title:

    NASA -- Tech Note


    Contributors:
    Musen, P. (author) / Bailie, A. (author) / Upton, E. (author)


    Publication date :

    1961


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :