Study of the normal and clamped modes of operation and dynamic response characteristics of the gimbaled control moment gyro (CMG) designed to fulfill the stringent pointing requirements of the Skylab telescope mount when the spacecraft is under the influence of both external and internal torques. The results indicate that the clamped mode of operation provides a feasible approach for significantly improving the system characteristics.


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    Titel :

    Attitude control of an orbiting space vehicle.


    Beteiligte:


    Erscheinungsdatum :

    01.11.1971


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Attitude control of an orbiting space vehicle.

    SUTHERLIN, D. W. / BOLAND, J. S. / BORELLI, M. T. | AIAA | 1971



    Attitude control of a manned earth orbiting space station.

    Billups, C. W. / Grissett, F. R. / Nixon, D. D. et al. | NTRS | 1969


    On the attitude control of a high precision orbiting space interferometer

    Baiocco, P. / Sevaston, G. | British Library Conference Proceedings | 1993