This paper describes the spacecraft dynamics model and orbit determination strategies developed to meet the stringent trajectory accuracy requirements for generating predicts for the transfer of a stable uplink frequency to the spacecraft and for determining reconstructed orbits for delivery to the NRAO VLBI correlator and the international VLBI science community.


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    Titel :

    Navigation of the Space VLBI Mission - HALCA


    Beteiligte:
    Mottinger, N. (Autor:in) / Ellis, J. (Autor:in) / You, T.H. (Autor:in)

    Erscheinungsdatum :

    11.05.1998


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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