The purpose of the study is to develop a technique for combining gradiometer and inertial navigation system (INS) outputs that minimizes the navigation and gravity rms errors, and to determine the gradiometer accuracy needed for typical aircraft and marine navigation and gravity-mapping applications.


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    Title :

    Gradiometer-Aided Inertial Navigation


    Contributors:

    Publication date :

    1975


    Size :

    100 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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    Warren G. Heller / Stanley K. Jordan | AIAA | 1976




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