A dual comet (Hall Flyby/Tempel 2 Rendezvous) mission, making use of the solar electric propulsion system, is under consideration for a 1985 launch. This paper describes the preliminary navigation system design for this mission. Orbit determination and guidance strategies for each mission phase are discussed. Navigation accuracy analyses and parametric senstivity studies for the Tempel 2 rendezvous approach phase are presented.


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    Titel :

    Navigation system design for a Halley Flyby/Tempel 2 Rendezvous mission using ion drive


    Beteiligte:
    Wood, L. J. (Autor:in) / Hast, S. L. (Autor:in)

    Kongress:

    American Astronautical Society and American Institute of Aeronautics and Astronautics, Astrodynamics Specialist Conference ; 1979 ; Provincetown, MA


    Erscheinungsdatum :

    01.06.1979


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






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