DocumentCode
1870640
Title
Simulation research of damping control based on MicroSim system
Author
Wu, Guoqiang ; Sun, Zhaowei ; Zhao, Dan ; Zhang, Weiqing
Author_Institution
Res. Center of Satellite Technol., Harbin Inst. Technol.
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
121
Abstract
In this paper, every composing of MicroSim is introduced, and the work theory of each composing is also introduced. One of the executive machines of MicroSim (reaction wheels) is used to realize the damping mode of micro-satellite. The task of the damping mode is to stop the rotational motion of the microsatellite in each of the three axes. And the simulation result is given under the damping control mode
Keywords
aerospace control; aerospace simulation; artificial satellites; damping; position control; MicroSim system; air bearing; damping control; damping mode; microsatellite; reaction wheels; Artificial satellites; Damping; Employee welfare; Helium; Mathematics; Satellite ground stations; Space technology; Space vehicles; Sun; Wheels; Air Bearing; Damping Mode; Five Degree of Freedom; Microsatellite;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location
Harbin
Print_ISBN
0-7803-9395-3
Type
conf
DOI
10.1109/ISSCAA.2006.1627594
Filename
1627594
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