DocumentCode
2200934
Title
Attitude control of a satellite around the space station
Author
Zhang, Hong-Hua ; Zhang, Bing
Author_Institution
Beijing Inst. of Control Eng., Chinese Acad. of Space Technol., Beijing, China
Volume
2
fYear
2001
fDate
2001
Firstpage
1529
Abstract
The paper deals with the attitude control of an accompanying satellite (AS) around a space station (SS). The concept of accompanying satellite around the space station is investigated. The reference coordinate frames are described for the AS pointing to the SS. A new control law is proposed for the attitude control of the AS in the presence of some unknown disturbances. The analytical and simulation results show that the proposed control law is very effective in attitude maneuvering and tracking
Keywords
artificial satellites; attitude control; stability; AS; SS; accompanying satellite; attitude control; attitude maneuvering; attitude tracking; control law; reference coordinate frames; space station satellite; unknown disturbances; Analytical models; Attitude control; Control engineering; Earth; Gravity; Inspection; Moon; Satellite ground stations; Space stations; Space technology;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
Conference_Location
Orlando, FL
Print_ISBN
0-7803-7061-9
Type
conf
DOI
10.1109/.2001.981112
Filename
981112
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