Title :
A reduced-order distributed observer approach to attitude consensus of multiple rigid spacecraft systems
Author :
He Cai ; Jie Huang
Author_Institution :
Dept. of Mech. & Autom. Eng., Chinese Univ. of Hong Kong, Shatin, China
Abstract :
Recently, we developed a distributed observer approach to study the leader-following consensus problem for multiple rigid spacecraft systems [3]. In this paper, we will further develop a reduced-order distributed observer approach to study the same problem. The proposed approach significantly reduces the orders of the control law and improves the transient response of the closed-loop system.
Keywords :
attitude control; closed loop systems; observers; reduced order systems; space vehicles; transient response; attitude consensus; closed-loop system; leader-following consensus; multiple rigid spacecraft systems; reduced-order distributed observer; transient response; Angular velocity; Attitude control; Bismuth; Decentralized control; Lead; Observers; Space vehicles; Reduced-order observer; attitude consensus; distributed control; rigid spacecraft system;
Conference_Titel :
Information and Automation (ICIA), 2013 IEEE International Conference on
Conference_Location :
Yinchuan
DOI :
10.1109/ICInfA.2013.6720500
