It is shown that gravity gradient field referred to orbiting satellite is dissymmetrical around local instantaneous vertical; in eccentric orbit, periodic forcing function at Schuler frequency is applied to vehicle; latter is supposed to have at least 2 unequal axes of inertia; accordingly, vehicle will oscillate at Schuler frequency of forcing function, natural frequency within orbital plane, and natural frequency perpendicularly to orbital plane; attitude prediction computer suggested should provide information on future attitude deviation during flight history of vehicle.


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    Titel :

    Attitude control of orbiting satellites at high eccentricity


    Weitere Titelangaben:

    ARS J


    Beteiligte:
    Savet, P.H. (Autor:in)

    Erschienen in:

    ARS Journal ; 32 , n 10


    Erscheinungsdatum :

    1962


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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