Preliminary orbit determination theories, based on Doppler observations alone, are developed; circular and elliptical preliminary orbits are treated; portions of classical spectroscopic binary star theory that are applicable to problem are pointed out; secular bulge perturbations, which accumulate during observation interval, are taken into account; it is important that they be included if theory is to have practical application; attention is directed to lunar and Martian artificial satellite orbits, but theories are applicable to satellites of other planets as well.


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    Titel :

    Determination of preliminary orbits of artificial lunar and planetary satellites


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Koskela, P.E. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 5


    Erscheinungsdatum :

    1964


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :