Key navigation issues and capabilities relating to the Voyager 2 Uranus/Neptune mission are presented. Predicted navigation performance at each encounter body (Uranus, Neptune, and Triton) is examined relative to mission navigation requirements and science return capabilities. Orbit determination accuracies are presented for several radio data types and for combinations of radio data with two optical data types. Maneuver strategies designed to accommodate the orbit determination results and satisfy mission navigation requirements are examined. Possible alternate aimpoints and contingency strategies are developed for situations of unexpected loss of propellant or optical navigation capability.


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    Titel :

    Voyager 2 navigation to Uranus and Neptune


    Beteiligte:
    Van Allen, R. E. (Autor:in) / Cesarone, R. J. (Autor:in) / Gray, D. L. (Autor:in)

    Kongress:

    Astrodynamics Conference ; 1982 ; San Diego, CA


    Erscheinungsdatum :

    1982-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Voyager 2 navigation to Uranus and Neptune

    VAN ALLEN, R. / CESARONE, R. / GRAY, D. | AIAA | 1982


    Voyager 2 Uranus and Neptune targeting

    Gray, D. L. / Cesarone, R. J. / Van Allen, R. E. | NTRS | 1982


    Voyager 2 Uranus and Neptune targeting

    GRAY, D. / CESARONE, R. / VAN ALLEN, R. | AIAA | 1982



    Voyager 2 navigation to Uranus

    Gray, D. L. / Taylor, A. H. / Davis, R. P. et al. | NTRS | 1986