DocumentCode :
2279796
Title :
The Non-linear Modeling of Airplane Dynamo Based on BP NN
Author :
Wang Haibo ; Liu Yongzhi
Author_Institution :
Air Force Eng. Univ., Xian, China
Volume :
3
fYear :
2010
fDate :
13-14 March 2010
Firstpage :
917
Lastpage :
920
Abstract :
This paper researches the principle and method of the BP NN modeling, makes use of the BP NN built up the non-linear model of airplane DC dynamo. After the model is trained by the characteristic data of airplane DC dynamo, successfully gets the empty characteristic curve and the voltage-time curve of impact load and impact unload by voltage adjustor. The result proves that the model of airplane DC dynamo which based on BP NN is effective.
Keywords :
DC generators; aircraft; aircraft power systems; backpropagation; electric machine analysis computing; neural nets; BP NN modeling; airplane DC dynamo; characteristic curve; impact load; impact unload; nonlinear modeling; voltage-time curve; Airplanes; Automation; Force measurement; Magnetohydrodynamic power generation; Mechatronics; Neural networks; Paper technology; Signal processing; Training data; Voltage; BP NN; airplane DC dynamo; modeling; voltage adjustor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Measuring Technology and Mechatronics Automation (ICMTMA), 2010 International Conference on
Conference_Location :
Changsha City
Print_ISBN :
978-1-4244-5001-5
Electronic_ISBN :
978-1-4244-5739-7
Type :
conf
DOI :
10.1109/ICMTMA.2010.260
Filename :
5458712
Link To Document :
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