Sampled-data control for spacecraft attitude control systems based on a quaternion model

被引：0
|
作者：
Jiang, Bangxin [1 ]
Liu, Yang [1 ]
Kou, Kit Ian [2 ]
机构：
[1] Zhejiang Normal Univ, Coll Math Phys & Informat Engn, Jinhua 321004, Peoples R China
[2] Univ Macau, Fac Sci & Technol, Dept Math, Macau, Peoples R China
来源：
2017 CHINESE AUTOMATION CONGRESS (CAC) | 2017年
基金：
中国博士后科学基金; 中国国家自然科学基金;
关键词：
Sampled-data control; attitude control; quaternion; Linear Matrix Inequality; linear-quadratic regulator;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, sampled-data control is considered for the attitude control of nonlinear spacecraft control systems. We mainly study a linearized spacecraft model i.e. the linearized inertial pointing spacecraft model. Moreover, it is shown that designed controller globally stabilizes the nonlinear spacecraft system, and locally optimizes the spacecraft performances. The simulation results demonstrate the high performances and asymptotic stability of the proposed method.
引用
收藏
页码：4297 / 4300
页数：4
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