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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    Titel :

    Gradiometer-Aided Inertial Navigation


    Beteiligte:
    W. G. Heller (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    100 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Error Analysis of Two New Gradiometer-Aided Inertial Navigation Systems

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




    On the Application of Gravity Gradiometer for Inertial Navigation System

    Shingu, H. / American Astronautical Society / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1997