DocumentCode
2968844
Title
The research of real-time estimation method on tether parameters for tethered satellite
Author
Yong, He ; Bin, Liang ; WenFu, Xu ; Cheng, Li
Author_Institution
Shenzhen Grad. Sch., Harbin Inst. of Technol., Shenzhen, China
fYear
2009
fDate
22-24 June 2009
Firstpage
148
Lastpage
153
Abstract
Most existing control methods of tethered satellite system were established on the knowing of tether parameters, but how to get the parameters needs to be solved. In this paper, a real-time estimator is developed to get the parameters. Firstly, we analyze the shortcomings resulting from directly solving the system equations to get tether parameters. Secondly, the equations are simplified and the corresponding problems are thoroughly investigated. And lastly, combing the measurements of a three-axis tether tensiometer with the information of attitude sensor, we use the Extended Kalman Filter to estimate the parameters in real time. The proposed estimator not only reduces the complexity of system model, but also improves the parameters´ precision. Simulation results verify the validity of this method.
Keywords
Kalman filters; artificial satellites; attitude control; parameter estimation; attitude sensor; extended Kalman filter; real-time estimation method; satellite attitude control system; tether parameters; tethered satellite system; Automation; Control systems; Equations; Extraterrestrial measurements; Helium; Length measurement; Parameter estimation; Satellites; Space shuttles; Space technology;
fLanguage
English
Publisher
ieee
Conference_Titel
Information and Automation, 2009. ICIA '09. International Conference on
Conference_Location
Zhuhai, Macau
Print_ISBN
978-1-4244-3607-1
Electronic_ISBN
978-1-4244-3608-8
Type
conf
DOI
10.1109/ICINFA.2009.5204910
Filename
5204910
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