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Sensor failure detection for jet engines using analytical redundanceAnalytical redundant sensor failure detection, isolation and accommodation techniques for gas turbine engines are surveyed. Both the theoretical technology base and demonstrated concepts are discussed. Also included is a discussion of current technology needs and ongoing Government sponsored programs to meet those needs.
Document ID
19840016517
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Merrill, W. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:83695
E-2123
NASA-TM-83695
AIAA PAPER 84-1452
Report Number: NAS 1.15:83695
Report Number: E-2123
Report Number: NASA-TM-83695
Report Number: AIAA PAPER 84-1452
Meeting Information
Meeting: Joint Propulsion Conf.
Location: Cincinnati, OH
Country: United States
Start Date: June 11, 1984
End Date: June 13, 1984
Sponsors: SAE, ASME, AIAA
Accession Number
84N24585
Funding Number(s)
PROJECT: RTOP 505-32-6B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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