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.


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    Title :

    A Closed-Form Solution for Doppler Satellite Navigation


    Contributors:
    Glish, John (author)


    Publication date :

    1971-09-01


    Size :

    1018478 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English