Orbit determination accuracies using satellite-to-satellite tracking

Details Orbit determination accuracies using satellite-to-satellite tracking Orbit determination accuracies using satellite-to-satellite tracking

Oct 1977

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1977stin...7810988v&link_type=abstract

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Physics

Orbit Calculation, Satellite-To-Satellite Tracking, System Effectiveness, Tracking Networks, Ats 6, Bayes Theorem, Doppler Radar, Geos 3 Satellite, Least Squares Method, Nimbus 6 Satellite, Tdr Satellites

Scientific paper

The uncertainty in relay satellite sate is a significant error source which cannot be ignored in the reduction of satellite-to-satellite tracking data. Based on simulations and real data reductions, it is numerically impractical to use simultaneous unconstrained solutions to determine both relay and user satellite epoch states. A Bayesian or least squares estimation technique with an a priori procedure is presented which permits the adjustment of relay satellite epoch state in the reduction of satellite-to-satellite tracking data without the numerical difficulties introduced by an ill-conditioned normal matrix.

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