Relationship is derived for drift of coordinate transformation matrix of quantized (pulsed) attitude reference system on vehicle undergoing "coning motion"; several sources of limit cycle oscillations in missiles and spacecraft are studied to determine nature of such coning motions; typical transformation drifts are computed for these system effects.


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    Titel :

    Drift of quantized attitude system due to vehicle coning motions


    Weitere Titelangaben:

    SAE-NASA -- Proc


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

    Kongress:

    Proceedings of the SAE-NASA -- Aerospace Vehicle Flight Control Conference ; 1965 Control



    Erscheinungsdatum :

    1965


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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