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Sensor failure detection for jet enginesThe use of analytical redundancy to improve gas turbine engine control system reliability through sensor failure detection, isolation, and accommodation is surveyed. Both the theoretical and application papers that form the technology base of turbine engine analytical redundancy research are discussed. Also, several important application efforts are reviewed. An assessment of the state-of-the-art in analytical redundancy technology is given.
Document ID
19890004061
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Merrill, Walter C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1988
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-4402
NAS 1.15:101396
NASA-TM-101396
Report Number: E-4402
Report Number: NAS 1.15:101396
Report Number: NASA-TM-101396
Accession Number
89N13432
Funding Number(s)
PROJECT: RTOP 505-62-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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