Finite-time attitude synchronisation for multiple spacecraft

被引：34

作者：

Lyu, Jianting ^{[1
]}

Qin, Jiahu ^{[2
]}

Ma, Qichao ^{[2
]}

Zheng, Wei Xing ^{[3
]}

Kang, Yu ^{[2
,4
]}

机构：

[1] Heilongjiang Univ, Sch Math Sci, Harbin 150080, Peoples R China

[2] Univ Sci & Technol China, Dept Automat, Hefei 230027, Peoples R China

[3] Univ Western Sydney, Sch Comp Engn & Math, Sydney, NSW 2751, Australia

[4] Chinese Acad Sci, Key Lab Technol Geospatial Informat Proc & Applic, Beijing 100190, Peoples R China

来源：

IET CONTROL THEORY AND APPLICATIONS | 2016年 / 10卷 / 10期

基金：

中国国家自然科学基金; 澳大利亚研究理事会;

关键词：

space vehicles; attitude control; Lyapunov methods; graph theory; numerical analysis; finite-time attitude synchronisation problem; multiple spacecrafts; directed communication topology; leaderless formation system; finite-time control laws; homogeneous method; Lyapunov stability theory; numerical simulations; VELOCITY-MEASUREMENTS; COMMUNICATION DELAYS; ADAPTIVE-CONTROL; RIGID BODIES; SYSTEMS; COORDINATION; TRACKING; DESIGN;

D O I：

10.1049/iet-cta.2015.1136

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This study investigates the finite-time attitude synchronisation problem for multiple spacecraft under a directed communication topology. Attitude synchronisation problem for a leaderless formation system without specified reference attitude is studied, and finite-time control laws are proposed and analysed without using neighbours' angular velocity measurements. By applying the graph theory, homogeneous method and Lyapunov stability theory, it is proved that the system is globally finite-time stable and attitude synchronisation can be achieved. Then the obtained control results are extended in the scenario with a stationary leader. Numerical simulations are finally given to demonstrate the effectiveness and feasibility of the obtained results.

引用

页码：1106 / 1114

页数：9

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