A methodology for producing simulations of the docking of a rigid spacecraft with any unrestrained flexible structure was studied. A detailed algorithm for the simulation of the docking of a rigid body with a nonuniform unrestrained beam was sought. The values acquired during docking by the variables characterizing the motions of the rigid body and the unrestrained beam were sought.


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    Titel :

    Docking of a rigid spacecraft with unrestrained orbiting flexible structure


    Beteiligte:
    Kane, T. R. (Autor:in)


    Erscheinungsdatum :

    01.04.1983


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :