DocumentCode
406116
Title
Turbojet modeling in wind milling based on neural network incorporating priori knowledge
Author
Aren, Yu D. ; Zhiwen, Wu
Author_Institution
Sch. of Energy Sci. & Eng., Harbin Inst. of Technol., China
Volume
1
fYear
2003
fDate
14-17 Dec. 2003
Firstpage
82
Abstract
Neural network is an effective method for turbojet modeling in wind milling, but its deficiency in generalization ability has restricted its application in engineering. Nonlinear PCA (principal component analysis), although is very effective in decreasing the dimensions of input variable and subsequently improving neural network´s generalization ability, it has difficulty in finding an appropriate nonlinear transform in engineering application. A method, which can be applied in turbojet modeling in wind milling based on neural network, is proposed in this paper. By incorporating priori knowledge of dynamic and static state of rotor, similar parameters and the relationship between residual power and acceleration, this method not only decreases the neural network´s dimensions reasonably and improves its generation ability greatly, but overcomes difficulties of nonlinear PCA. The simulation results prove the method to be simple and effective.
Keywords
aircraft; generalisation (artificial intelligence); neural nets; principal component analysis; generalization ability; neural network; nonlinear PCA; nonlinear transform; priori knowledge; turbojet modeling; wind milling; Acceleration; Data mining; Input variables; Intelligent networks; Knowledge engineering; Milling; Neural networks; Power engineering and energy; Principal component analysis; Rotors;
fLanguage
English
Publisher
ieee
Conference_Titel
Neural Networks and Signal Processing, 2003. Proceedings of the 2003 International Conference on
Conference_Location
Nanjing
Print_ISBN
0-7803-7702-8
Type
conf
DOI
10.1109/ICNNSP.2003.1279218
Filename
1279218
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