DocumentCode :
1732696
Title :
Finite-time consensus control for multiple spacecraft systems under directed communication topology
Author :
Zhang Hai-bo ; Ma Guang-fu ; Mei Jie
Author_Institution :
Beijing Inst. of Control & Eng., Beijing, China
fYear :
2013
Firstpage :
7210
Lastpage :
7215
Abstract :
This paper addresses a distributed finite-time consensus control problem for multiple spacecraft systems under a directed communication topology. Firstly, we propose a finite-time consensus protocol to deal with the finite-time static consensus problem for multiple spacecraft systems. Based on finite-time Lyapunov theory, it is theoretically shown that the states of the spacecraft can achieve static consensus in finite time, that is all spacecraft attitudes converge to a common value and angular velocities converge to zero. Furthermore, the present control algorithm is extended to solve the finite-time dynamic consensus problem for multiple spacecraft systems, that is all spacecraft states converge to the desired dynamic value. The effectiveness of the results is also illustrated by numerical simulations.
Keywords :
Lyapunov methods; aircraft control; angular velocity; convergence of numerical methods; distributed control; space vehicles; topology; angular velocities; directed communication topology; distributed finite-time consensus control problem; dynamic value; finite-time Lyapunov theory; finite-time consensus protocol; finite-time dynamic consensus problem; finite-time static consensus control problem; multiple spacecraft systems; numerical simulations; spacecraft attitude convergence; spacecraft state convergence; Aerodynamics; Educational institutions; Electronic mail; Erbium; Heuristic algorithms; Space vehicles; Topology; Consensus; Distributed; Finite-time; Multiple Spacecraft Systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6640706
Link To Document :
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