Task I encompassed the design, development and procurement of hardware, sensors, and microprocessors for two diagnostic monitoring systems. The first system was installed on the F-14 Hydraulic Flight Simulator on Task II of the program. Task II included the installation of one system on the F-14A Hydraulic Simulator for system component reliability demonstrations. The task also covered simulated component failures and diagnostic system reaction. In Task III, the Diagnostic System was integrated into A6E B/N 155628. The system was debugged and a 12 month flight test schedule. This report covers Task III. (Author)


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    Hydraulic diagnostic monitoring system

    Duzich, J.J. | Tema Archive | 1981


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