DocumentCode :
3520551
Title :
Research on Aero-Engine Sensor Failure Diagnosis with Dual Redundant Predictors Based on Neutral Network
Author :
Sun Yigang ; Ren Daming
Author_Institution :
Aeronaut. Autom. Coll., Civil Aviation Univ. of China, Tianjin, China
fYear :
2011
fDate :
28-29 May 2011
Firstpage :
1
Lastpage :
4
Abstract :
In consideration of the common sensor failures in aero-engine control system, a new approach is proposed using dual redundant predictors based on neutral network in this paper. The neutral network temporal redundant predictor and spatial redundant predictor are created over the time series redundant information of single sensor and the space redundant information of multi-sensor respectively. The threshold-value differentiate method is applied for real-time sensor failure detection. Isolate the fault sensor and use the outputs of spatial redundant predictor to accommodate it. Digital simulation results show that this method is effective and feasible.
Keywords :
aerospace engines; aerospace instrumentation; computerised instrumentation; digital simulation; fault diagnosis; mechanical engineering computing; neural nets; sensor fusion; aero-engine control system; aero-engine sensor failure diagnosis; digital simulation; dual redundant predictors; multisensor; neutral network; spatial redundant predictor; temporal redundant predictor; threshold-value differentiate method; Artificial neural networks; Control systems; Engines; Redundancy; Rotors; Temperature sensors; Training;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Systems and Applications (ISA), 2011 3rd International Workshop on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-9855-0
Electronic_ISBN :
978-1-4244-9857-4
Type :
conf
DOI :
10.1109/ISA.2011.5873346
Filename :
5873346
Link To Document :
بازگشت