DocumentCode
3411897
Title
The Application of Variable Structure Bang-Bang Controller on Floating Satellite Simulation System
Author
Zha, Shihong ; Mei, Tao ; Luo, Minzhou ; Zhang, Weizhong ; Chen, Sanfeng
fYear
2007
fDate
5-8 Aug. 2007
Firstpage
3605
Lastpage
3609
Abstract
In this paper, a method of variable structure bang-bang controller is introduced. This controller is designed to implement the accurate control of the pneumatic shaft angle servo system and applied on three shafts of a space floating satellite simulation system. Simulation results show that the static and dynamic performance is excellent. The method is one of the most possible approaches to control the pneumatic PWM shaft angle servo system.
Keywords
aerospace control; artificial satellites; bang-bang control; control system synthesis; pneumatic control equipment; variable structure systems; bang-bang controller; floating satellite simulation system; pneumatic shaft angle servo system; variable structure system; Control systems; Mechanical variables control; Optimal control; Pulse width modulation; Satellites; Servomechanisms; Shafts; Space vector pulse width modulation; Switches; Valves; Bang-Bang control; PWM; floating satellite; variable structure;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2007. ICMA 2007. International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4244-0828-3
Electronic_ISBN
978-1-4244-0828-3
Type
conf
DOI
10.1109/ICMA.2007.4304145
Filename
4304145
Link To Document