The problem of transferring alignment between two airborne inertial navigator platforms is treated using the Kalman filter approach. The important parameters are identified and exercised over a reasonable range to establish accuracy trade-offs. Suggestions are provided for improving the accuracy of Kalman filter transfer alignment through more complex maneuvers of the carrying aircraft. (Author)


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    Titel :

    The Kalman Filter in Transfer Alignment of Airborne Inertial Guidance Systems


    Beteiligte:
    A. A. Sutherland (Autor:in) / A. Gelb (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    45 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch