Coupling between pitch and yaw axes of rocket-engine gimbaling system is caused by compliance of structure to which engine and its pitch and yaw gimbaling actuators are mounted; effects of coupling on stability and response of engine gimbaling servos during ground operation and on vehicle attitude control system during flight were analyzed using control system theory; structural compliance characteristics were defined by influence coefficient matrix, elements of which were determined by redundant force analysis; results obtained are presented.


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    Titel :

    On structural compliance-induced coupling in thrust-vector control system


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Curtis, H.S. (Autor:in) / Hagstrom, C.T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :