In-flight fault accommodation of safety-critical faults requires rapid detection and remediation. Indeed, for a class of safety-critical faults, detection within a millisecond range is imperative to allow accommodation in time to avert undesired engine behavior. We address these issues with an integrated detection and accommodation scheme. This scheme comprises model-based detection, a bank of binary classifiers, and an accommodation module. The latter biases control signals with pre-defined adjustments to regain operability while staying within established safety limits. The adjustments were developed using evolutionary algorithms to identify optimal biases off-line for multiple faults and points within the flight envelope. These biases are interpolated online for the current flight conditions. High-fidelity simulation results are presented showing accommodation applied to a high-pressure compressor fault on a commercial, high-bypass, twin-spool, turbofan engine throughout the flight envelope.
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October 2007
Technical Papers
Integrated in-Flight Fault Detection and Accommodation: A Model-Based Study
Brent J. Brunell
Brent J. Brunell
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Randal T. Rausch
Kai F. Goebel
Neil H. Eklund
Brent J. Brunell
J. Eng. Gas Turbines Power. Oct 2007, 129(4): 962-969 (8 pages)
Published Online: January 4, 2007
Article history
Received:
September 9, 2005
Revised:
January 4, 2007
Citation
Rausch, R. T., Goebel, K. F., Eklund, N. H., and Brunell, B. J. (January 4, 2007). "Integrated in-Flight Fault Detection and Accommodation: A Model-Based Study." ASME. J. Eng. Gas Turbines Power. October 2007; 129(4): 962–969. https://doi.org/10.1115/1.2720517
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