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.
A Closed-Form Solution for Doppler Satellite Navigation
IEEE Transactions on Aerospace and Electronic Systems ; AES-7 , 5 ; 875-878
1971-09-01
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Article (Journal)
Electronic Resource
English
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