DocumentCode
1374048
Title
A real time microcomputer implementation of sensor failure detection for turbofan engines
Author
DeLaat, John C. ; Merrill, Walter C.
Author_Institution
NASA Lewis Res. Center, Cleveland, OH, USA
Volume
10
Issue
4
fYear
1990
fDate
6/1/1990 12:00:00 AM
Firstpage
29
Lastpage
37
Abstract
An algorithm that detects, isolates, and accommodates sensor failures using analytical redundancy has been developed. The performance of this algorithm has been demonstrated on a full-scale F100 turbofan engine. The algorithm has been implemented in real time on a microprocessor-based controls computer which includes parallel processing and high level language programming. Parallel processing was used to achieve the required computational power for the real-time implementation. High level 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.<>
Keywords
aerospace computing; aerospace engines; microcomputer applications; parallel processing; redundancy; F100; aerospace computing; multivariable control algorithm; parallel processing; real time; redundancy; sensor failure detection; turbofan engines; Algorithm design and analysis; Concurrent computing; Costs; Engines; Failure analysis; High level languages; Microcomputers; Parallel processing; Parallel programming; Software algorithms;
fLanguage
English
Journal_Title
Control Systems Magazine, IEEE
Publisher
ieee
ISSN
0272-1708
Type
jour
DOI
10.1109/37.56275
Filename
56275
Link To Document