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.
Navigation of the Space VLBI Mission - HALCA
1998-05-11
Miscellaneous
No indication
English
Navigation of the Space VLBI Mission - HALCA
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