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