DocumentCode
3572775
Title
Station-keeping control method for GEO satellite based on relative orbit dynamics
Author
Yang Wenbo ; Li Shaoyuan ; Li Ning
Author_Institution
Dept. of Autom., Shanghai Jiao Tong Univ., Shanghai, China
fYear
2014
Firstpage
1682
Lastpage
1687
Abstract
Based on the analysis of relative orbit dynamics for GEO (geostationary orbit, GEO) satellite and LQG (Linear Quadratic Gaussian, LQG) algorithm, this paper proposed a station-keeping control method for GEO satellite, which realized north-south station-keeping and west-east station-keeping simultaneously. To further verify the effectiveness of the proposed method, corresponding mathematical simulation is carried out. Simulation results show that the proposed method can obtain good control precision compared with conventional station-keeping control method of GEO satellite. Thus, the proposed method is suitable for station-keeping control of GEO satellite.
Keywords
artificial satellites; linear quadratic control; GEO satellite; LQG algorithm; control precision; geostationary orbit satellite; linear quadratic Gaussian algorithm; mathematical simulation; north-south station-keeping; relative orbit dynamics; station-keeping control method; west-east station-keeping; Acceleration; Control systems; Equations; Mathematical model; Orbits; Satellites; Vectors; GEO satellite; Linear Quadratic Gaussian; relative orbit dynamic; station-keeping;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation (WCICA), 2014 11th World Congress on
Type
conf
DOI
10.1109/WCICA.2014.7052973
Filename
7052973
Link To Document