A relationship is derived for the drift of a coordinate transformation matrix of a quantiz­ed (pulsed) attitude reference system on a ve­hicle undergoing a “coning motion”. Several sour­ces of limit cycle oscillations in missiles and spacecraft are studied to determine the nature of such coning motions. Typical transformation drifts are computed for these system effects.


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    Titel :

    The Drift of a Quantized Attitude System Due to Vehicle Coning Motions


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Schmitt, A. F. (Autor:in)

    Kongress:

    NASA Aerospace Vehicle Flight Control Conference ; 1965



    Erscheinungsdatum :

    01.02.1965




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :