DocumentCode
1630941
Title
Neural Network Integration Fusion Model and Application
Author
Zhang, Xiaodan ; Niu, Zhendong
Author_Institution
Sch. of Comput. Sienstist & Technol., Beijing Inst. of Technol., Beijing
Volume
1
fYear
2008
Firstpage
213
Lastpage
215
Abstract
A new fusion model is proposed, which is the combination of BP neural networks and rough set algorithm, to solve the problems of low precision rate in aircraft engine fault diagnosis by traditional methods. The method realizes feature level fusion of all subjective data and expert experiments on different parts of engine, and the predominance compensation of different models. In simulation experiment, the method proposed in the paper can improve diagnosis precision 5.0% more than expert system.
Keywords
aerospace computing; aerospace engines; backpropagation; fault diagnosis; neural nets; rough set theory; BP neural networks; aircraft engine fault diagnosis; feature level fusion; neural network integration fusion model; rough set algorithm; Aircraft propulsion; Algorithm design and analysis; Application software; Computer networks; Diagnostic expert systems; Fault diagnosis; Intelligent networks; Intelligent systems; Neural networks; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Systems Design and Applications, 2008. ISDA '08. Eighth International Conference on
Conference_Location
Kaohsiung
Print_ISBN
978-0-7695-3382-7
Type
conf
DOI
10.1109/ISDA.2008.331
Filename
4696205
Link To Document