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.
Inertial navigator flight-testing experience with Lockheed F-104
J Aircraft
Journal of Aircraft ; 1 , n 3
1964
7 pages
Article (Journal)
English
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AIAA | 1965
|SLUB | 1958
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