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A real time microcomputer implementation of sensor failure detection for turbofan enginesAn algorithm was developed which detects, isolates, and accommodates sensor failures using analytical redundancy. The performance of this algorithm was 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
19890019661
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
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
September 6, 2013
Publication Date
August 1, 1989
Subject Category
Computer Operations And Hardware
Report/Patent Number
NAS 1.15:102327
NASA-TM-102327
E-5029
Report Number: NAS 1.15:102327
Report Number: NASA-TM-102327
Report Number: E-5029
Accession Number
89N29032
Funding Number(s)
PROJECT: RTOP 505-62-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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