Description of flight profiles and courses flown, and technique used for reduction of data, during flight testing of light weight inertial navigator installed in F-104 interceptor; equipment requirements for system accuracy were established in terms of statistical parameter, circular error probable; major program effort was centered about flight testing of inertial navigator systems in 5 F-104 airplanes; problems discovered in several areas.


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    Title :

    Inertial navigator flight-testing experience with Lockheed F-104


    Additional title:

    J Aircraft


    Contributors:
    Meyer, D.R. (author) / Hodge, K.E. (author)

    Published in:

    Publication date :

    1964


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :