Docking configuration and docking sequence are described for accomplishing orbital refueling mission; docking configuration consists essentially of matched conical surfaces, on docking vehicles, and latching device; mathematical model for studying collision dynamics, effects of guidance errors, attitude errors, and various structural parameters on docking performance; requirements for attitude control; it is concluded that proposed docking configuration is feasible and will accommodate reasonable system errors.


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    Titel :

    Orbital docking dynamics


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Ward, J.W. (Autor:in) / Williams, H.M. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 6 ; p 1360-1364


    Erscheinungsdatum :

    1963


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    ORBITAL DOCKING DYNAMICS

    WARD, J. W. / WILLIAMS, H. M. | AIAA | 1963


    Orbital Docking Simulators

    R. J. Conlon | NTIS | 1965



    Orbital Maneuvering Vehicle (OMV) three-point docking latch

    Myers, W. Neill / Forbes, John C. / Barnes, Wayne L. | NTRS | 1990


    Despinning Orbital Debris Before Docking Using Laser Ablation

    Kumar, Rubbel / Sedwick, Raymond J. | AIAA | 2015