The instruments and data evaluation used for flight testing of two Litton laser gyro strapdown navigation systems in a DO-28 aircraft are described. The reference data based on the platform navigation system CAROUSEL 4a are corrected by application of optimal smoothing techniques. Results of the LTN-90 flight tests are presented and graphs of one of the flight tests are discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flight Testing of Litton Laser Gyro Strapdown System LTN-90 for General Aviation


    Beteiligte:
    H. J. Hotop (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch