A procedure to compute the integer ambiguity problem when a GPS receiver is used in a multiple antenna configuration attached to a rotating spacecraft is presented. The method is applied to a simulation of an experimental satellite which uses the GPS receiver for attitude determination.


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    Title :

    Integer ambiguity resolution in GPS for spinning spacecrafts


    Contributors:


    Publication date :

    1999-10-01


    Size :

    573736 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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