Title :
Rapid detection of faults for safety critical aircraft operation
Author :
Goebel, Kai ; Eklund, Neil ; Brunell, Brent
Author_Institution :
GE Global Res., One Res. Circle, Niskayuna, NY, USA
Abstract :
Fault diagnosis typically assumes a sufficiently large fault signature and enough time for a reliable decision to be reached. However, for a class of safety critical faults on commercial aircraft engines, prompt detection is paramount within a millisecond range to allow accommodation to avert undesired engine behavior. At the same time, false positives must be avoided to prevent inappropriate control action. To address these issues, several advanced features were developed that operate on the residuals of a model based detection scheme. We show that these features pick up system changes reliably within the required time. A bank of binary classifiers determines the presence of the fault as determined by a maximum likelihood hypothesis test. We show performance results for four different faults at various levels of severity and show performance results throughout the entire flight envelope on a high fidelity aircraft engine model.
Keywords :
aerospace computing; aerospace engines; fault diagnosis; maximum likelihood detection; pattern classification; safety-critical software; binary classifiers; commercial aircraft engines; engine behavior; fault detection; fault diagnosis; fault signature; features pick up system; flight envelope; high fidelity aircraft engine; maximum likelihood hypothesis test; model-based detection; rapid detection; reliable decision; safety critical aircraft operation; safety critical faults; Actuators; Air accidents; Air safety; Aircraft propulsion; Engines; Fault detection; Fault diagnosis; Maximum likelihood detection; Modeling; Testing;
Conference_Titel :
Aerospace Conference, 2004. Proceedings. 2004 IEEE
Print_ISBN :
0-7803-8155-6
DOI :
10.1109/AERO.2004.1368144