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A Hybrid Neural Network-Genetic Algorithm Technique for Aircraft Engine Performance DiagnosticsIn this paper, a model-based diagnostic method, which utilizes Neural Networks and Genetic Algorithms, is investigated. Neural networks are applied to estimate the engine internal health, and Genetic Algorithms are applied for sensor bias detection and estimation. This hybrid approach takes advantage of the nonlinear estimation capability provided by neural networks while improving the robustness to measurement uncertainty through the application of Genetic Algorithms. The hybrid diagnostic technique also has the ability to rank multiple potential solutions for a given set of anomalous sensor measurements in order to reduce false alarms and missed detections. The performance of the hybrid diagnostic technique is evaluated through some case studies derived from a turbofan engine simulation. The results show this approach is promising for reliable diagnostics of aircraft engines.
Document ID
20010069983
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kobayashi, Takahisa
(QSS Group, Inc. Brook Park, OH United States)
Simon, Donald L.
(Army Research Lab. Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2001
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2001-211088
NAS 1.15:211088
AIAA Paper 2001-3763
ARL-TR-1266
E-12931
Report Number: NASA/TM-2001-211088
Report Number: NAS 1.15:211088
Report Number: AIAA Paper 2001-3763
Report Number: ARL-TR-1266
Report Number: E-12931
Meeting Information
Meeting: 37th Joint Propulsion Conference and Exhibit
Location: Salt Lake City, UT
Country: United States
Start Date: July 8, 2001
End Date: July 11, 2001
Sponsors: American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 728-30-20
PROJECT: DA Proj. 1L1-61102-AH-45
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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