Least-squares-based methods are very popular in the jet engine community for health monitoring purpose. Their isolation capability can be improved by using a prior knowledge on the health parameters that better matches the expected pattern of the solution i.e., a sparse one as accidental faults impact at most one or two component(s) simultaneously. On the other hand, complimentary information about the feasible values of the health parameters can be derived in the form of constraints. The present contribution investigates the effect of the addition of such constraints on the performance of the sparse estimation tool. Due to its quadratic programming formulation, the constraints are integrated in a straightforward manner. Results obtained on a variety of fault conditions simulated with a commercial turbofan model show that the inclusion of constraints further enhance the isolation capability of the sparse estimator. In particular, the constraints help resolve a confusion issue between high pressure compressor and variable stator vanes faults.
Skip Nav Destination
ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition
June 6–10, 2011
Vancouver, British Columbia, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5463-1
PROCEEDINGS PAPER
Constrained Sparse Estimation for Improved Fault Isolation
S. Borguet,
S. Borguet
University of Lie`ge, Lie`ge, Belgium
Search for other works by this author on:
O. Le´onard
O. Le´onard
University of Lie`ge, Lie`ge, Belgium
Search for other works by this author on:
S. Borguet
University of Lie`ge, Lie`ge, Belgium
O. Le´onard
University of Lie`ge, Lie`ge, Belgium
Paper No:
GT2011-45711, pp. 199-208; 10 pages
Published Online:
May 3, 2012
Citation
Borguet, S, & Le´onard, O. "Constrained Sparse Estimation for Improved Fault Isolation." Proceedings of the ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. Volume 3: Controls, Diagnostics and Instrumentation; Education; Electric Power; Microturbines and Small Turbomachinery; Solar Brayton and Rankine Cycle. Vancouver, British Columbia, Canada. June 6–10, 2011. pp. 199-208. ASME. https://doi.org/10.1115/GT2011-45711
Download citation file:
10
Views
Related Proceedings Papers
Related Articles
Constrained Sparse Estimation for Improved Fault Isolation
J. Eng. Gas Turbines Power (December,2011)
A Sparse Estimation Approach to Fault Isolation
J. Eng. Gas Turbines Power (February,2010)
Aircraft Turbofan Engine Health Estimation Using Constrained Kalman Filtering
J. Eng. Gas Turbines Power (April,2005)
Related Chapters
Redundancy Resolution via QP Approach and Unification
Robot Manipulator Redundancy Resolution
Varying Joint-Velocity Limits Handled by QP
Robot Manipulator Redundancy Resolution
Feedback-Aided Minimum Joint Motion
Robot Manipulator Redundancy Resolution