Title :
Adaptive synchronization control of spacecraft with fixed rotational axis
Author :
Hayakawa, Tomohisa
Author_Institution :
Dept. of Mech. & Environ. Inf., Tokyo Inst. of Technol., Tokyo, Japan
Abstract :
An adaptive consensus control framework for the rotational dynamics of multiple spacecraft is developed. Specifically, we assume that the mass moment of inertia of each spacecraft is unknown so that the largest principal axis is uncertain. Even though conservation of momentum does not hold in the adaptive case, attitude synchronization is attained after sufficiently long time has elapsed.
Keywords :
adaptive control; attitude control; space vehicles; synchronisation; adaptive consensus control; adaptive synchronization control; attitude synchronization; fixed rotational axis; multiple spacecraft; rotational dynamics; Adaptive control; Angular velocity; Attitude control; Informatics; Kinematics; Nonlinear equations; Programmable control; Space technology; Space vehicles; Torque control; Selected keywords relevant to the subject;
Conference_Titel :
ICCAS-SICE, 2009
Conference_Location :
Fukuoka
Print_ISBN :
978-4-907764-34-0
Electronic_ISBN :
978-4-907764-33-3
