DocumentCode
1852134
Title
Robust dynamic inversion control for BTT missiles based on neural network
Author
Shi, Zhen ; Yu, Xiuping ; Cui, JianLin ; Li, Yan
Author_Institution
Autom. Coll., Harbin Eng. Univ., China
Volume
4
fYear
2005
fDate
29 July-1 Aug. 2005
Firstpage
1901
Abstract
A nonlinear control scheme, which is a mixed scheme of inversion system method and neural network adaptation theory, is applied to the design of bank-to-turn (BTT) missiles in this paper. First, the control model, which is based on inversion system method and neural network adaptation theory, is built. Second, the progressive convergence of tracking error is proved theoretically. Then, the on-line neural network is used to dynamically eliminate the influence of inversion error on system; hence this mixed scheme overcomes the shortage of nonlinear dynamical inversion control scheme where a precise mathematic model is necessary. Finally the validity of the control scheme is certified by digital simulation.
Keywords
missile control; neurocontrollers; nonlinear control systems; BTT missile; bank-to-turn missile; digital simulation; inversion system method; neural network adaptation theory; nonlinear dynamical inversion control scheme; tracking error; Control systems; Convergence; Error correction; Mathematical model; Mathematics; Missiles; Neural networks; Nonlinear control systems; Nonlinear dynamical systems; Robust control;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2005 IEEE International Conference
Print_ISBN
0-7803-9044-X
Type
conf
DOI
10.1109/ICMA.2005.1626852
Filename
1626852
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