Derivation of closed-form, exact analytical equations governing 3-dimensional relative motion between vehicles executing rendezvous maneuver in specified flight time is presented; vehicular orbits may be either elliptical, parabolic, or hyperbolic; relationship between observed data and relative position and velocity vectors is given; guidance law required at initiation and termination of rendezvous maneuver is established.


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    Titel :

    Exact closed-form solution to rendezvous problem


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Beteiligte:
    Schwarzbein, Z.E. (Autor:in) / Gersten, R.H. (Autor:in) / Smith, G.E. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    31 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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