DocumentCode
175568
Title
Application of fuzzy optimization control in NSV anti-disturbance
Author
Gao Qian ; He Nai-bao
Author_Institution
Sch. of Comput. Eng., Jiangsu Univ. of Technol., Changzhou, China
fYear
2014
fDate
May 31 2014-June 2 2014
Firstpage
552
Lastpage
554
Abstract
Variable universe fuzzy control based on intelligent control technology is proposed in this paper for the hypersonic flight process of nearspace vehicle (NSV) with severe changes of aero-dynamic parameters and susceptibility on the external disturbances. And the contraction-expansion factor of the fuzzy control is given to modify the scale of universe and reduce the computational cost. By adopting fast fuzzy terminal sliding mode with variable universe in the slow loop controller which is suffering the disturbance, its robustness, the speed of anti-disturbance and control accuracy are enhanced with the adaptively modified fuzzy universe. A demonstration with the Lyapunov function is given to proved that the errors of system could converge to zero in finite time.
Keywords
adaptive control; aerodynamics; attitude control; control system synthesis; fuzzy control; nonlinear control systems; optimal control; space vehicles; variable structure systems; vehicle dynamics; Lyapunov function; NSV anti-disturbance; adaptively modified fuzzy universe; aerodynamic parameters; contraction-expansion factor; control accuracy; fast fuzzy terminal sliding mode; fuzzy optimization control; hypersonic flight process; intelligent control technology; nearspace vehicle; slow loop controller; variable universe fuzzy control; Adaptation models; Educational institutions; Equations; Fuzzy control; Interference; Mathematical model; Vehicles; Fuzzy Control; Nearspace Vehicle; Robust Control; Variable Universe;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location
Changsha
Print_ISBN
978-1-4799-3707-3
Type
conf
DOI
10.1109/CCDC.2014.6852227
Filename
6852227
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