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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    Title :

    Sampled-data velocity vector control of spacecraft


    Additional title:

    ASME -- Paper


    Contributors:

    Conference:

    ASME Meeting WA-314 ; 1963 Control



    Publication date :

    1963


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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