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.


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    Title :

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


    Contributors:
    H. J. Hotop (author)

    Publication date :

    1984


    Size :

    43 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English