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<title>AAS 98-192</title><body BGCOLOR="ffffff">
<h2>AAS 98-192</h2>
<h2>SIMULTANEOUS ORBIT DETERMINATION OF LARGE SATELLITE CONSTELLATIONS</h2>
<h4>M. T. Soyka, J. W. Middour - Naval Research Laboratory; J. Fein - Computer Sciences Corp.</h4>
<h2> Abstract </h2>
The techniques of performing simultaneous orbit determination on a large telecommunications satellite constellation are demonstrated.  Using the orbit determination program OCEAN, simulated radiometric two-way ranging is used as the baseline tracking type.  Intersatellite ranging is used as an additional tracking type and for comparison to the two-way ranging solution.  The addition of three-way ranging provides information necessary to determine the relative and absolute system timing.  When satellite states are estimated in a simultaneous solution, intersatellite range and three-way range can provide cross-correlation and full covariance information between satellites.
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