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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    Titel :

    Inertial navigator flight-testing experience with Lockheed F-104


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Meyer, D.R. (Autor:in) / Hodge, K.E. (Autor:in)

    Erschienen in:

    Journal of Aircraft ; 1 , n 3 ; p 141-147


    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :