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