DocumentCode :
2632869
Title :
Small satellite attitude control based on mechanically-pumped fluid loops
Author :
Xiao-wei, Shan ; Xue-qin, Chen ; Yun-hai, Geng ; Shi-jie, Zhang
Author_Institution :
Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin, China
fYear :
2011
fDate :
21-23 June 2011
Firstpage :
149
Lastpage :
153
Abstract :
An attitude control system based on mechanically pumped fluid loops is presented in this article, and the controller consisting of “fluid wheels” is investigated. First, the attitude control system is designed based on the principle that fluid of liquid in the closed loops accelerated by mechanical pumps will generate torques on satellite. Then the mathematical model of the controller is built based on the given structure/distribution. Finally, the closed-loop attitude control system with FMC as actuator is set up. The simulation results demonstrate that the design could improve attitude control capacity while decreasing the system volume/mass and complexity.
Keywords :
actuators; artificial satellites; attitude control; closed loop systems; flow control; torque; FMC; actuator; attitude control capacity; closed loops; closed-loop attitude control system; fluid wheels; mechanical pumps; mechanically-pumped fluid loops; small satellite attitude control; system complexity; system mass; system volume; torque; Attitude control; DC motors; Fluids; Pumps; Satellites; Torque; Wheels; attitude control system; fluid wheel; mechanically-pumped fluid loops; satellite;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Industrial Electronics and Applications (ICIEA), 2011 6th IEEE Conference on
Conference_Location :
Beijing
ISSN :
pending
Print_ISBN :
978-1-4244-8754-7
Electronic_ISBN :
pending
Type :
conf
DOI :
10.1109/ICIEA.2011.5975568
Filename :
5975568
Link To Document :
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