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A Closed-Form Solution for Doppler Satellite Navigation
Authors:Glish  J
Institution:Control Data Corporation Minneapolis, Minn. 55440;
Abstract:Doppler satellite navigation relies on an initial position estimate with an iterative solution. A closed-form solution of this problem, which forms the basis of a complete analytic treatment, is presented. The solution is exact for arbitrary satellite orbits with an ellipsoid Earth model.
Keywords:
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