Two-dimensional steering of spacecraft, incorporating time shared digital computer, during orbital transfer maneuver, is investigated; effects of sampling and holding, and pulse width modulation on attitude correction maneuver performed in response to prealignment error are studied; amount of additional fuel consumed for entire orbital transfer maneuver due to initial error is shown to be dependent on 4 factors.


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    Titel :

    Sampled-data velocity vector control of spacecraft


    Weitere Titelangaben:

    ASME -- Paper


    Beteiligte:
    Bender, E.K. (Autor:in)

    Kongress:

    ASME Meeting WA-314 ; 1963 Control



    Erscheinungsdatum :

    1963


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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