DocumentCode
175483
Title
Momentum Management of Chinese space station based on robust H∞
Author
Lin Yue ; Jia Ying-min ; Gao Ya-nan ; Fan Song-tao
Author_Institution
Beijing Inst. of Control Eng., Beijing, China
fYear
2014
fDate
May 31 2014-June 2 2014
Firstpage
418
Lastpage
422
Abstract
For the requirement of multi-structure architecture, a controller based on robust H_∞ is proposed for LVLH angular momentum Management control method. The method is characterized by a combination of robust control and classical pole placement, and gives the system more robustness of parameter variation. Numerical simulation based on accurate dynamic model is proposed. Simulation result shows that controller meets the requirement of different structure of Chinese space station, and do not need to change control rate of system.
Keywords
H∞ control; aerospace control; numerical analysis; pole assignment; robust control; Chinese space station; LVLH angular momentum management control method; classical pole placement; multistructure architecture; numerical simulation; parameter variation; robust H∞; robust H_∞; robust control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location
Changsha
Print_ISBN
978-1-4799-3707-3
Type
conf
DOI
10.1109/CCDC.2014.6852184
Filename
6852184
Link To Document