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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    Title :

    Drift of quantized attitude system due to vehicle coning motions


    Additional title:

    SAE-NASA -- Proc


    Contributors:

    Conference:

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



    Publication date :

    1965


    Size :

    4 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :