Finite-time attitude regulation control for a rigid spacecraft under input saturation

被引：0
|
作者：
Du, Haibo [1 ]
Cheng, Yingying [1 ]
Lie, Yigang [1 ]
机构：
[1] Hefei Univ Technol, Sch Elect Engn & Automat, Hefei 230009, Peoples R China
来源：
2014 11TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA) | 2014年
基金：
中国博士后科学基金;
关键词：
attitude control; finite-time control; input saturation; STABILIZATION; TRACKING; SYSTEMS; STABILITY;
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：
The problem of attitude regulation for a rigid spacecraft under input saturation is studied in this paper. Based on the technique of finite-time control and the model structural features, a novel finite-time attitude controller is proposed. The bound of a proposed finite-time controller can be adjusted to any small level to accommodate the actuation bound in practical implementation. A simulation example is given to demonstrate the efficiency of the proposed method.
引用
收藏
页码：1647 / 1651
页数：5
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