An iterative method is presented for determining the position on earth of a balloon, correcting for both errors due to terrestrial rotation and errors due to the Doppler effect. An interrogating satellite is used, and a zero wind condition is assumed. The accuracy obtained is on the order of 1 millionth.


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    Title :

    Errors Due to Terrestrial Rotation. Errors Due to Inherent Balloon Speed. Complete Restitution of Localization (Doppler)


    Publication date :

    1972


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English