NASA NTRS · 19850026891
A preliminary evaluation of a failure detection filter for detecting and identifying control element failures in a transport aircraft
Abstract
The application of the failure detection filter to the detection and identification of aircraft control element failures was evaluated in a linear digital simulation of the longitudinal dynamics of a B-737 Aircraft. Simulation results show that with a simple correlator and threshold detector used to process the filter residuals, the failure detection performance is seriously degraded by the effects of turbulence.
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Bundick, W. T.. 1985-07-01. A preliminary evaluation of a failure detection filter for detecting and identifying control element failures in a transport aircraft. https://ntrs.nasa.gov/citations/19850026891
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