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Automatic control of the Skylab Astronaut Maneuvering Research Vehicle. (1973)

Greenlee, J. E. ; Murtagh, T. B. ; Goodwin, M. A. ; [et al.]

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Publication Date: 2019-07-13

Description: 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.

Keywords: NAVIGATION

Type: AIAA PAPER 73-857 , Guidance and Control Conference; Aug 20, 1973 - Aug 22, 1973; Key Biscayne, FL

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