Proceedings of ASME Turbo Expo 2005: Land Sea & Air, June 6-9, 2005, Reno-Tahoe.This paper describes the development of an improved method for reliable, repeatable, and accurate matching of engine performance models to test data. The centerpiece of this approach is a minimum variance estimator algorithm with a priori estimates which addresses both deterministic and probabilistic aspects of the problem. Specific probabilistic aspects include uncertainty in the measurements, prior expectations on model matching parameters, and noise in the power setting parameters. The algorithm is able to produce optimal results using any number of measurements and model matching parameters and can therefore take advantage of all measured data to produce the...
The research in this dissertation develops a system level formulation for the probabilistic analysis...
For turbine engine performance monitoring purposes, system identification techniques are often used ...
Integrated engine-airframe optimal control technology may significantly improve aircraft performance...
Proceedings of ASME Turbo Expo 2005: Land Sea & Air, June 6-9, 2005, Reno-Tahoe.This paper describes...
Presented at the 2003 ISABE Conference, Sept. 1-4, Cleveland, OH.This paper explores the application...
The aim of this study is to explore the possibility of matching a cycle performance model to public ...
This paper presents analytical techniques for aiding system designers in making aircraft engine heal...
Production engine pass-off testing is a compulsory technique adopted to ensure that each engine meet...
The gas turbine engine is a widely used thermodynamic system for aircraft. The demand for quantifyin...
Least-squares health parameter identification techniques, such as the Kalman filter, have been exten...
Gas turbine performance models are usually created in an object oriented manner, where different sta...
Nowadays, turbine engine tests are processed using an open loop, i.e. the measurements are verified ...
Presented at 2003 JANNAF Joint Meeting, 1-5 December, Colorado Springs, CO.The subject of uncertaint...
peer reviewedLeast-squares health parameter identification techniques such as the Kalman filter have...
A requirement for effective aircraft engine performance estimation is the ability to account for eng...
The research in this dissertation develops a system level formulation for the probabilistic analysis...
For turbine engine performance monitoring purposes, system identification techniques are often used ...
Integrated engine-airframe optimal control technology may significantly improve aircraft performance...
Proceedings of ASME Turbo Expo 2005: Land Sea & Air, June 6-9, 2005, Reno-Tahoe.This paper describes...
Presented at the 2003 ISABE Conference, Sept. 1-4, Cleveland, OH.This paper explores the application...
The aim of this study is to explore the possibility of matching a cycle performance model to public ...
This paper presents analytical techniques for aiding system designers in making aircraft engine heal...
Production engine pass-off testing is a compulsory technique adopted to ensure that each engine meet...
The gas turbine engine is a widely used thermodynamic system for aircraft. The demand for quantifyin...
Least-squares health parameter identification techniques, such as the Kalman filter, have been exten...
Gas turbine performance models are usually created in an object oriented manner, where different sta...
Nowadays, turbine engine tests are processed using an open loop, i.e. the measurements are verified ...
Presented at 2003 JANNAF Joint Meeting, 1-5 December, Colorado Springs, CO.The subject of uncertaint...
peer reviewedLeast-squares health parameter identification techniques such as the Kalman filter have...
A requirement for effective aircraft engine performance estimation is the ability to account for eng...
The research in this dissertation develops a system level formulation for the probabilistic analysis...
For turbine engine performance monitoring purposes, system identification techniques are often used ...
Integrated engine-airframe optimal control technology may significantly improve aircraft performance...