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A Systematic Approach for Model-Based Aircraft Engine Performance EstimationA requirement for effective aircraft engine performance estimation is the ability to account for engine degradation, generally described in terms of unmeasurable health parameters such as efficiencies and flow capacities related to each major engine module. This paper presents a linear point design methodology for minimizing the degradation-induced error in model-based aircraft engine performance estimation applications. The technique specifically focuses on the underdetermined estimation problem, where there are more unknown health parameters than available sensor measurements. A condition for Kalman filter-based estimation is that the number of health parameters estimated cannot exceed the number of sensed measurements. In this paper, the estimated health parameter vector will be replaced by a reduced order tuner vector whose dimension is equivalent to the sensed measurement vector. The reduced order tuner vector is systematically selected to minimize the theoretical mean squared estimation error of a maximum a posteriori estimator formulation. This paper derives theoretical estimation errors at steady-state operating conditions, and presents the tuner selection routine applied to minimize these values. Results from the application of the technique to an aircraft engine simulation are presented and compared to the estimation accuracy achieved through conventional maximum a posteriori and Kalman filter estimation approaches. Maximum a posteriori estimation results demonstrate that reduced order tuning parameter vectors can be found that approximate the accuracy of estimating all health parameters directly. Kalman filter estimation results based on the same reduced order tuning parameter vectors demonstrate that significantly improved estimation accuracy can be achieved over the conventional approach of selecting a subset of health parameters to serve as the tuner vector. However, additional development is necessary to fully extend the methodology to Kalman filter-based estimation applications.
Document ID
20100006915
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Simon, Donald L.
(NASA Glenn Research Center Cleveland, OH, United States)
Garg, Sanjay
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2010
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-17110
AIAA Paper 2009-1872
NASA/TM-2010-216077
Report Number: E-17110
Report Number: AIAA Paper 2009-1872
Report Number: NASA/TM-2010-216077
Meeting Information
Meeting: Infotech@Aerospace (I@A) Conference
Location: Seattle, WA
Country: United States
Start Date: April 6, 2009
End Date: April 9, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 645846.02.07.03.03.012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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