Ability of pilot to perform rendezvous under various conditions of thrust misalignment and attitude rate damping was investigated by means of 6 degrees of freedom computer simulation through systematic variation of vehicle dynamics; results indicate that manual control of rendezvous can be achieved consistently; results presented regarding pilot performance, fuel consumption, terminal conditions, and ability to hold attitude and follow thrusting schedule, rendezvous vehicle parameters such as displays, controls, and thrust configuration, are discussed.


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    Titel :

    Simulation of manned rendezvous under adverse dynamic conditions


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Beteiligte:
    Roberts, J.B. (Autor:in) / Farber, E.I. (Autor:in) / Larson, C.A. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    20 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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