Engine health monitoring has been an area of intensive research for more than three decades. Numerous methods have been developed with the goal of performing an accurate assessment of the engine condition. It is generally accepted that a practical implementation of a monitoring tool will rely on a combination of several techniques. In this framework, the present contribution proposes an original approach for coupling two diagnostic tools in order to enhance the capability of an engine health monitoring system. One tool is based on a principal component analysis scheme and the other is based on a Kalman filter technique. The three methodologies are compared and the benefit of the combined tool is demonstrated on simulated fault cases which c...
This paper proposed a method to update the on-line health reference baseline of the On-Board Engine ...
An efficient maintenance plan is an important aspect for aeronautical companies to increase flight s...
peer reviewedIn the frame of turbine engine performance monitoring, system identification procedures...
peer reviewedEngine health monitoring has been an area of intensive research for more than three dec...
In this paper, a bank of Kalman filters is applied to aircraft gas turbine engine sensor and actuato...
In this report, a fault detection and isolation (FDI) system which utilizes a bank of Kalman filters...
AbstractA duty in development of an on-line fault detection algorithm is to make it associate with e...
peer reviewedIn this contribution, an on-line engine performance monitoring is carried out through a...
Fault detection and isolation (FDI) logic plays a crucial role in enhancing the safety and reliabili...
Jet engines are precision machines composed of many expensive parts characterized by a large number ...
A diagnostic method consisting of a combination of Kalman filters and Bayesian Belief Network (BBN) ...
peer reviewedIn an on-line engine performance monitoring, two tasks must be simultaneously carried ...
For turbine engine performance monitoring purposes, system identification techniques are often used ...
peer reviewedA common assumption made in the performance assessment of a turbine engine for aircraft...
Abstract: In this paper, an aero-engine augmented state variable model and a Kalman filter based met...
This paper proposed a method to update the on-line health reference baseline of the On-Board Engine ...
An efficient maintenance plan is an important aspect for aeronautical companies to increase flight s...
peer reviewedIn the frame of turbine engine performance monitoring, system identification procedures...
peer reviewedEngine health monitoring has been an area of intensive research for more than three dec...
In this paper, a bank of Kalman filters is applied to aircraft gas turbine engine sensor and actuato...
In this report, a fault detection and isolation (FDI) system which utilizes a bank of Kalman filters...
AbstractA duty in development of an on-line fault detection algorithm is to make it associate with e...
peer reviewedIn this contribution, an on-line engine performance monitoring is carried out through a...
Fault detection and isolation (FDI) logic plays a crucial role in enhancing the safety and reliabili...
Jet engines are precision machines composed of many expensive parts characterized by a large number ...
A diagnostic method consisting of a combination of Kalman filters and Bayesian Belief Network (BBN) ...
peer reviewedIn an on-line engine performance monitoring, two tasks must be simultaneously carried ...
For turbine engine performance monitoring purposes, system identification techniques are often used ...
peer reviewedA common assumption made in the performance assessment of a turbine engine for aircraft...
Abstract: In this paper, an aero-engine augmented state variable model and a Kalman filter based met...
This paper proposed a method to update the on-line health reference baseline of the On-Board Engine ...
An efficient maintenance plan is an important aspect for aeronautical companies to increase flight s...
peer reviewedIn the frame of turbine engine performance monitoring, system identification procedures...