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A real time microcomputer implementation of sensor failure detection for turbofan enginesAn algorithm was developed that detects, isolates, and accommodates sensor failures using analytical redundancy. The performance of this algorithm has been demonstrated on a full-scale F100 turbofan engine. The algorithm was implemented in real-time on a microprocessor-based controls computer which includes parallel processing and high order language programming. Parallel processing was used to achieve the required computational power for the real-time implementation. High order language programming was used in order to reduce the programming and maintenance costs of the algorithm implementation software. The sensor failure algorithm was combined with an existing multivariable control algorithm to give a complete control implementation with sensor analytical redundancy. The real-time microprocessor implementation of the algorithm, which resulted in the successful completion of the algorithm engine demonstration, is described.
Document ID
19900058359
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Delaat, John C.
(NASA Lewis Research Center Cleveland, OH, United States)
Merrill, Walter C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
June 1, 1990
Publication Information
Publication: IEEE Control Systems Magazine
Volume: 10
ISSN: 0272-1708
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ISSN: 0272-1708
Accession Number
90A45414
Distribution Limits
Public
Copyright
Other

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