Title :
A Closed-Form Solution for Doppler Satellite Navigation
Author_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 :
Closed-form solution; Doppler shift; Earth; Equations; Frequency; Orbits; Radio navigation; Satellite broadcasting; Satellite navigation systems;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1971.310327
