Sensor failure detection, isolation, and accommodation using a neural network approach is described. An auto-associative neural network is configured to perform dimensionality reduction on the sensor measurement vector and provide estimated sensor values. The sensor validation scheme is applied in a simulation of the T700 turboshaft engine in closed loop operation. Performance is evaluated based on the ability to detect faults correctly and maintain stable and responsive engine operation. The set of sensor outputs used for engine control forms the network input vector. Analytical redundancy is verified by training networks of successively smaller bottleneck layer sizes. Training data generation and strategy are discussed. The engine maintai...
In the aeronautical field, aircraft reliability is strictly dependent on propulsion systems. Indeed,...
A method for on-line Space Shuttle Main Engine (SSME) anomaly detection and fault typing using a fee...
Sensor failures are a major cause of concern in engine-performance monitoring as they can result in ...
This paper presents the results of applying two different types of neural networks in two different ...
A new method of sensor failure detection, isolation, and accommodation is described using a neural n...
For a dual redundant-control system, which is typical for short-haul aircraft, if a failure is detec...
Accurate gas turbine diagnosis relies on accurate measurements from sensors. Unfortunately, sensors ...
Aircraft engines are complex systems that require high reliability and adequate monitoring to ensure...
This paper applies a previously developed sensor data qualification technique to a commercial aircra...
In this paper the problem of fault diagnosis in an aircraft jet engine is investigated by using an i...
As part of the NASA Aviation Safety Program, a unique model-based diagnostics method that employs ne...
The objective of the advanced detection, isolation, and accommodation (ADIA) program is to improve t...
This paper presents an application of a fault detection and diagnosis scheme for the sensor faults o...
Neural networks have been employed for learning fault behavior from rocket engine simulator paramete...
The role of diagnostic systems in gas turbine operations has changed over the past years from a sing...
In the aeronautical field, aircraft reliability is strictly dependent on propulsion systems. Indeed,...
A method for on-line Space Shuttle Main Engine (SSME) anomaly detection and fault typing using a fee...
Sensor failures are a major cause of concern in engine-performance monitoring as they can result in ...
This paper presents the results of applying two different types of neural networks in two different ...
A new method of sensor failure detection, isolation, and accommodation is described using a neural n...
For a dual redundant-control system, which is typical for short-haul aircraft, if a failure is detec...
Accurate gas turbine diagnosis relies on accurate measurements from sensors. Unfortunately, sensors ...
Aircraft engines are complex systems that require high reliability and adequate monitoring to ensure...
This paper applies a previously developed sensor data qualification technique to a commercial aircra...
In this paper the problem of fault diagnosis in an aircraft jet engine is investigated by using an i...
As part of the NASA Aviation Safety Program, a unique model-based diagnostics method that employs ne...
The objective of the advanced detection, isolation, and accommodation (ADIA) program is to improve t...
This paper presents an application of a fault detection and diagnosis scheme for the sensor faults o...
Neural networks have been employed for learning fault behavior from rocket engine simulator paramete...
The role of diagnostic systems in gas turbine operations has changed over the past years from a sing...
In the aeronautical field, aircraft reliability is strictly dependent on propulsion systems. Indeed,...
A method for on-line Space Shuttle Main Engine (SSME) anomaly detection and fault typing using a fee...
Sensor failures are a major cause of concern in engine-performance monitoring as they can result in ...