DocumentCode
2637269
Title
Parameter identification for orbit of geosynchronous satellites based on Kalman filter
Author
Hu, Xiaoyang ; Qiao, Xiangxin ; Wang, Xin ; Yao, Jun
Author_Institution
Sch. of Equip. Eng., Shenyang Ligong Univ., Shenyang, China
fYear
2011
fDate
21-23 June 2011
Firstpage
1430
Lastpage
1433
Abstract
This paper analyzed physical process of movement of geosynchronous satellites, amendment of booster and measurement of Earth station, established the mathematical models and their linearization; On this base, it gave mathematical model for Kalman filter. Executed simulation for the given mathematical model on the Simplified actual date, simulation result is: Kalman filter effectively reduce estimation error of orbital parameters, it means that parameter identification of orbit has been improved more.
Keywords
Kalman filters; artificial satellites; celestial mechanics; Earth station; Kalman filter; estimation error; geosynchronous satellites; orbital parameters; parameter identification; Acceleration; Earth; Equations; Kalman filters; Mathematical model; Orbits; Satellites; Kalman filter; orbit; parameter identification; synchronous satellite;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics and Applications (ICIEA), 2011 6th IEEE Conference on
Conference_Location
Beijing
ISSN
pending
Print_ISBN
978-1-4244-8754-7
Electronic_ISBN
pending
Type
conf
DOI
10.1109/ICIEA.2011.5975813
Filename
5975813
Link To Document