Two-impulse torquing scheme for reorienting spin axis of asymmetric spinning vehicle through large angles is described; if all parameters are nominal and torques are ideally impulsive, scheme is theoretically perfect; mechanization of scheme using body-fixed torquing jets is discussed, and results are illustrated with numerical example; steady-state reorientation error produced by variation in spin speed from its nominal value is examined and found to be small for typical variations.


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    Titel :

    Two-impulse attitude reorientation of asymmetric spinning vehicle


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Grubin, C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :