Failure Detection and Isolation for an Asychronous Digital Flight Control System.
AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
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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 AFTIF-16 digital flight control system were modelled. Keywords Theses Hypothetical tests.
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- Manufacturing and Industrial Engineering and Control of Production Systems