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A preliminary evaluation of a failure detection filter for detecting and identifying control element failures in a transport aircraftThe 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.
Document ID
19850026891
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bundick, W. T. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:87576
NASA-TM-87576
Report Number: NAS 1.15:87576
Report Number: NASA-TM-87576
Accession Number
85N35204
Funding Number(s)
PROJECT: RTOP 505-34-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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