The two automatic control modes of the Astronaut Maneuvering Research Vehicle (AMRV) are analyzed: the control moment gyro (CMG) and the rate gyro (RG). The AMRV is an autonomous maneuvering unit which translates and rotates the pilot by means of hand-controller input commands. The CMG normal operation, desaturation, and cage/lock dynamics are described in terms of a realistic AMRV mass property configuration. No propellant is used for normal operation in the CMG mode, and the maximum rotation rate is 5 deg/sec about each AMRV axis. The RG attitude maneuvering and limit cycle submode dynamic are described in terms of the same AMRV mass property configuration.


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    Titel :

    Automatic control of the Skylab Astronaut Maneuvering Research Vehicle.


    Beteiligte:
    Murtagh, T. B. (Autor:in) / Goodwin, M. A. (Autor:in) / Greenlee, J. E. (Autor:in) / Whitsett , C. E. (Autor:in)

    Kongress:

    Guidance and Control Conference ; 1973 ; Key Biscayne, FL


    Erscheinungsdatum :

    01.08.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Automatic control of the Skylab Astronaut Maneuvering Research Vehicle

    MURTAGH, T. / GOODWIN, M. / GREENLEE, J. et al. | AIAA | 1973


    Automatic Control of the Skylab Astronaut Maneuvering Research Vehicle

    T. B. MURTAGH / C. E. WHITSETT / M. A. GOODWIN et al. | AIAA | 1974


    On-orbit performance of the Skylab astronaut maneuvering research vehicle

    Murtagh, T. B. / Mccandless, B., II / Whitsett, C. E. et al. | NTRS | 1974



    Skylab astronaut life support assembly

    Brown, J. T. | NTRS | 1972