DocumentCode :
2643328
Title :
Using unknown input observers to detect and isolate sensor faults in a turbofan engine
Author :
Dassanake, S.K. ; Balas, Gary J. ; Bokor, Jozsef
Author_Institution :
Minnesota Univ., Minneapolis, MN, USA
Volume :
2
fYear :
2000
fDate :
2000
Abstract :
An observer based fault detection and isolation method is presented. The method involves combining the unknown input observer theory with the Beard fault detection filter theory to generate a residual signal that has both disturbance decoupling and unidirectional properties. This robust, in the sense of disturbances, residual was used to detect and isolate sensor faults in a turbofan engine model. Finally, the method was successfully extended to detect and isolate sensor faults over a wide range of power input levels by scheduling the observer based on power code
Keywords :
aerospace control; aerospace engines; condition monitoring; fault diagnosis; multivariable control systems; observers; robust control; state-space methods; Beard fault detection filter theory; disturbance decoupling; fault detection; fault isolation; full order observer; power code; residual signal; robust residual; sensor faults; state estimation error; state-space matrices; turbofan engine control; unidirectional properties; unknown input observers; weighted output; Actuators; Engines; Equations; Fault detection; Filtering theory; Filters; Observers; Robustness; State estimation; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
Conference_Location :
Philadelphia, PA
Print_ISBN :
0-7803-6395-7
Type :
conf
DOI :
10.1109/DASC.2000.884916
Filename :
884916
Link To Document :
بازگشت