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