A lightweight, low-cost R and D aircraft inertial navigation system is evaluated for use in Army aircraft. A brief description of the system is followed by a summary of the methods of laboratory, truck, and flight testing employed. Test results are presented and show that the system meets the design goals of 2 to 4 nautical miles/hour. Problem areas uncovered during the tests are discussed in detail and areas of suggested future effort are outlined. (Author)


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    Title :

    Flight Test Report of AN/ASN-82 Inertial Navigation System


    Contributors:
    R. Clark (author)

    Publication date :

    1970


    Size :

    105 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English