DocumentCode :
2869102
Title :
Neural network model identification for actuators in a flight control systems
Author :
Huang, Zhiyi ; Zhang, Weiguo ; Gu, Wei ; Liu, Xiaoxiong
Author_Institution :
Coll. of Autom., Northwestern Polytech. Univ., Xi´´an, China
Volume :
13
fYear :
2010
fDate :
22-24 Oct. 2010
Abstract :
The precision system identification models is very important to design and analysis for complex control systems. A model of the actuators in a flight control systems is identified by using BP neural network. An adaptive BP neural network learning algorithm is proposed in this paper, which uses adaptive learn rate and steepest gradient optimization algorithm to train the weights. The improved algorithm is applied to identify the nonlinear actuators. The simulation results show that the performance of the neural network is improved effectively and the output of systems can be identified accurately by using the improved method.
Keywords :
actuators; adaptive control; aerospace control; backpropagation; gradient methods; neurocontrollers; actuators; adaptive BP neural network learning algorithm; flight control systems; neural network model identification; precision system identification models; steepest gradient optimization algorithm; BP neural networks; actuators; adaptive gradient optimization algorithm; model identification;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Application and System Modeling (ICCASM), 2010 International Conference on
Conference_Location :
Taiyuan
Print_ISBN :
978-1-4244-7235-2
Electronic_ISBN :
978-1-4244-7237-6
Type :
conf
DOI :
10.1109/ICCASM.2010.5622899
Filename :
5622899
Link To Document :
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