DocumentCode
1775577
Title
High-precision attitude control for satellite with repeat ground track orbit
Author
Baolin Wu ; Danwei Wang
Author_Institution
Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
fYear
2014
fDate
18-20 June 2014
Firstpage
1145
Lastpage
1149
Abstract
Repeating ground track orbit is useful for satellite to detect the changes of the interested area with identical viewing conditions repetitively. The attitude control system for this kind of mission is a repetitively-operated dynamic system. An anticipatory iterative learning control (ILC) scheme is proposed to improve the attitude control accuracy for the above attitude control mission. Simulation results show that the attitude control accuracy can be greatly improved by using the anticipatory ILC scheme.
Keywords
artificial satellites; attitude control; iterative methods; learning systems; anticipatory ILC scheme; anticipatory iterative learning control scheme; high-precision attitude control; identical viewing conditions; repeat ground track orbit; repetitively-operated dynamic system; satellite; Accuracy; Adaptive control; Attitude control; Orbits; Quaternions; Satellites; Torque;
fLanguage
English
Publisher
ieee
Conference_Titel
Control & Automation (ICCA), 11th IEEE International Conference on
Conference_Location
Taichung
Type
conf
DOI
10.1109/ICCA.2014.6871083
Filename
6871083
Link To Document