DocumentCode :
2837048
Title :
Self-Organizing CMAC Control for Flexible Spacecraft Rapid Stabilization
Author :
Wang, Yan ; Tang, Qiang ; Chen, Xinglin ; Cao, Ying
Author_Institution :
Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
fYear :
2011
fDate :
17-18 July 2011
Firstpage :
1
Lastpage :
4
Abstract :
In this paper, an intelligence control is develope for a flexible spacecraft with rapid stabilization. The proposed control is comprised of a neural controller and a slide controller. The self-organizing CMAC controller is utilized to overcome influence with uncertain system parameter, while the slide control law is proposed to achieve system stability. Finally, the simulation results of the flexible spacecraft show a perfect stabilizing response can be achieved using self-organizing CMAC algorithm.
Keywords :
aircraft control; cerebellar model arithmetic computers; neurocontrollers; robust control; self-organising feature maps; space vehicles; uncertain systems; flexible spacecraft; intelligence control; neural controller; rapid stabilization; self-organizing CMAC controller; slide control law; slide controller; system stability; uncertain system parameter; Aerospace electronics; Attitude control; Flexible structures; Mathematical model; Simulation; Space vehicles; Vibrations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Circuits, Communications and System (PACCS), 2011 Third Pacific-Asia Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4577-0855-8
Type :
conf
DOI :
10.1109/PACCS.2011.5990190
Filename :
5990190
Link To Document :
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