Device employs only 2 gyro wheels and 3 gimbals to effect control of 3 components of vehicle angular rate; moderate degradation of transient response is experienced, due to increased cross-coupling between vehicle axes; it is shown that gyro controller is efficient device when its energy requirements are compared to those for flywheel controller; digital simulation results presented illustrate time response of attitude control system employing advanced gyro controller.


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    Titel :

    Gyro momentum exchange device for space vehicle attitude control


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Kennedy, H.B. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 5


    Erscheinungsdatum :

    1963


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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    Kim, Young-Won / Lee, Sang-Don / Lee, Chang-Hun et al. | IEEE | 2019



    Twin-gyro attitude control systems.

    HUSTON, R. L. | AIAA | 1966


    Mixed Control Moment Gyro and Momentum Wheel Attitude Control Strategies (AAS 03-558)

    Skelton, C. E. / Hall, C. D. / American Astronautical Society | British Library Conference Proceedings | 2004