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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    Titel :

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


    Beteiligte:
    D. P. Payne (Autor:in) / R. B. Shoaf (Autor:in) / H. P. Koesters (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    194 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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