This technical report documents the results of flight test of the Honeywell Laser Inertial Navigational System (LINS), an engineering model of a ring laser gyro strapdown inertial navigation system. The purpose of the testing was to demonstrate strapdown laser inertial navigation system advanced technology and to evaluate the LINS as a potential candidate system to meet future, moderate accuracy, medium cost, inertial navigator needs. The testing was considered developmental, rather than verification, within the meaning of applicable DOD/DDR and E directives.


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    Title :

    Developmental Test of the Honeywell Laser Inertial Navigation System (LINS)


    Contributors:
    D. P. Payne (author) / R. B. Shoaf (author) / H. P. Koesters (author)

    Publication date :

    1975


    Size :

    194 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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