DocumentCode :
1941091
Title :
Disturbance-Observed-Based-Control Design of the Drag-Free Satellite
Author :
Shi Li ; Cao Xibin ; Zhang Jinxiu ; Dong Xiaoguang
Author_Institution :
Res. Center of Spacecraft Technol., Harbin Inst. of Technol., Harbin, China
fYear :
2011
fDate :
5-7 Aug. 2011
Firstpage :
446
Lastpage :
451
Abstract :
The controller design of the drag-free satellite on near-earth orbit is the researching object. After analyzing the characteristics of the main disturbances affecting the drag-free satellite, the disturbance model is established. Adding the disturbance to the system, a disturbance observed based dynamics model of the drag-free satellite is built. Then the mixed H2/H controller is designed and the LMI form is given to solve it. Simulation results verify the stability and feasibility of the controller.
Keywords :
H control; artificial satellites; control system synthesis; linear matrix inequalities; observers; LMI; disturbance-observed-based-control design; drag-free satellite; mixed H2/H∞ controller; Drag; Equations; Mathematical model; Observers; Orbits; Satellites; Symmetric matrices; accelerometer mode; displacement mode; disturbance observer; the drag-free satelLite;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Manufacturing and Automation (ICDMA), 2011 Second International Conference on
Conference_Location :
Zhangjiajie, Hunan
Print_ISBN :
978-1-4577-0755-1
Electronic_ISBN :
978-0-7695-4455-7
Type :
conf
DOI :
10.1109/ICDMA.2011.116
Filename :
6051949
Link To Document :
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