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Spurious symptom reduction in fault monitoringPrevious work accomplished on NASA's Faultfinder concept suggested that the concept was jeopardized by spurious symptoms generated in the monitoring phase. The purpose of the present research was to investigate methods of reducing the generation of spurious symptoms during in-flight engine monitoring. Two approaches for reducing spurious symptoms were investigated. A knowledge base of rules was constructed to filter known spurious symptoms and a neural net was developed to improve the expectation values used in the monitoring process. Both approaches were effective in reducing spurious symptoms individually. However, the best results were obtained using a hybrid system combining the neural net capability to improve expectation values with the rule-based logic filter.
Document ID
19930020003
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shontz, William D.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Records, Roger M.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Choi, Jai J.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Cybernetics
Report/Patent Number
NASA-CR-191453
NAS 1.26:191453
Report Number: NASA-CR-191453
Report Number: NAS 1.26:191453
Accession Number
93N29192
Funding Number(s)
CONTRACT_GRANT: NAS1-18027
PROJECT: RTOP 505-64-13-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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