Study of satellite rendezvous terminal guidance techniques by means of phase plane analysis and numerical examples; methods of rendezvous differ in type of propulsion used, e.g., on-off or continuous thrusting; mathematical derivation of guidance philosophy commensurate with both propulsion capability and initial condition variations is shown and relationship between throttling capability and launch timing accuracy examined; comparison between propellant requirements for different rendezvous guidance systems.


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    Titel :

    Analysis of guidance techniques for achieving orbital rendezvous


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Beteiligte:
    Felleman, P.G. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    16 pages


    Anmerkungen:

    Numerical examples


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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