Title :
Attitude Consensus of two underactuated spacecraft
Author :
Hutagalung, Maclaurin ; Hayakawa, Tomohisa
Author_Institution :
Dept. of Mech. & Environ. Inf., Tokyo Inst. of Technol., Tokyo
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;
Conference_Titel :
SICE Annual Conference, 2008
Conference_Location :
Tokyo
Print_ISBN :
978-4-907764-30-2
Electronic_ISBN :
978-4-907764-29-6
DOI :
10.1109/SICE.2008.4655234
