DocumentCode :
2486562
Title :
Control Method of Dynamic Inversion with Neural Network Used for Multi-Variable Nonlinear Flight Control System
Author :
Qian, Kechang ; Li, Jian
Author_Institution :
Ordance Eng. Coll., Shijiazhuang, China
fYear :
2010
fDate :
22-23 May 2010
Firstpage :
1
Lastpage :
4
Abstract :
Aiming at multi-variable nonlinear flight control system, this paper analyzes the analytical inverse system in theory detailedly. By the tracking principle of neural network, a dynamic neural network is presented, which consist of static neural network and integrators. The paper designs a control method of dynamic inversion with neural network used for multi-variable nonlinear flight control system, and makes simulation of flight control system of power parafoil. Simulation results demonstrate that the control method has strong ability of control and robustness.
Keywords :
aerospace control; aerospace simulation; neural nets; analytical inverse system; dynamic inversion; dynamic neural network; flight control system simulation; integrators; multi-variable nonlinear flight control system; power parafoil; static neural network; Aerospace control; Aerospace engineering; Control systems; Educational institutions; Electronic mail; Equations; Neural networks; Nonlinear control systems; Nonlinear dynamical systems; Nonlinear systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Systems and Applications (ISA), 2010 2nd International Workshop on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-5872-1
Electronic_ISBN :
978-1-4244-5874-5
Type :
conf
DOI :
10.1109/IWISA.2010.5473678
Filename :
5473678
Link To Document :
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