DocumentCode
3162335
Title
Attitude Consensus of two underactuated spacecraft
Author
Hutagalung, Maclaurin ; Hayakawa, Tomohisa
Author_Institution
Dept. of Mech. & Environ. Inf., Tokyo Inst. of Technol., Tokyo
fYear
2008
fDate
20-22 Aug. 2008
Firstpage
3299
Lastpage
3304
Abstract
A consensus control framework for rotation dynamics of multiple underactuated spacecraft is developed. Following the results by Bullo et al. (2000), we propose a control law that achieves asymptotic consensus between the spacecraft. Finally, we present a numerical example to show efficacy of the proposed approach.
Keywords
asymptotic stability; attitude control; nonlinear control systems; space vehicles; attitude consensus; consensus control; nonlinear control; rotation dynamics; underactuated spacecraft; Angular velocity; Angular velocity control; Attitude control; Backstepping; Convergence; Informatics; Space technology; Space vehicles; State feedback; Trajectory; Underactuated; nonlinear control;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE Annual Conference, 2008
Conference_Location
Tokyo
Print_ISBN
978-4-907764-30-2
Electronic_ISBN
978-4-907764-29-6
Type
conf
DOI
10.1109/SICE.2008.4655234
Filename
4655234
Link To Document