The present work examines some extensions of the digital autopilot (DAP) capability as programmed in the Apollo Command and Service Module (CSM) onboard computer. Design activity undertaken for a thrust vector control DAP to control a proposed main engine deorbit burn of CSM while still docked to the Orbital Workshop is discussed. The design, implementation, and testing of a reaction control system DAP for the docked Skylab configuration are described along with its adaptation to control of the Apollo/Soyuz docked configuration.


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    Titel :

    Digital attitude control of the Skylab and Apollo/Soyuz orbital assemblies


    Beteiligte:
    Penchuk, A. (Autor:in) / Turnbull, J. F. (Autor:in) / Schlundt, R. W. (Autor:in) / Jones, J. E. (Autor:in)

    Kongress:

    International Federation of Automatic Control, Symposium on Automatic Control in Space ; 1974 ; Tsakhkadzor, Soviet Union


    Erscheinungsdatum :

    1974-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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