The purpose of this study was to design and test a failure detection and isolation subsystem for a triply redundant asychronous digital flight control system. The focus of the research was to analyze the time skew effect in an asychronous environment. A model to estimate the time skew and the time skew related interchannel difference was developed. The design was tested in a simulation environment where the YF-16 longitudinal dynamics and the AFTI/F-16 digital flight control system were modelled.
Failure Detection and Isolation for an Asychronous Digital Flight Control System
1987
192 pages
Report
Keine Angabe
Englisch
Avionics , Digital systems , Flight control systems , Asynchronous systems , Fail safe , Detection , Failure , Isolation , Theses , Skewness , Time , Environments , Simulation , Hybrid computers , Fighter aircraft , AFTI Digital Flight Control System , YF-16 aircraft , FDI(Failure Detection and Isolation) , DFCS(Digital Flight Control Systems)
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