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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    Title :

    Navigation of the Space VLBI Mission - HALCA


    Contributors:
    Mottinger, N. (author) / Ellis, J. (author) / You, T.H. (author)

    Publication date :

    1998-05-11


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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