Adaptive sliding mode attitude tracking control for flexible spacecraft

被引：0
|
作者：
Geng, Yuanzhuo [1 ]
Li, Chuanjiang [1 ]
Sun, Yanchao [1 ]
Ma, Jingjing [1 ]
机构：
[1] Harbin Inst Technol, Dept Control Sci & Engn, Harbin, Peoples R China
来源：
PROCEEDINGS OF 2016 SIXTH INTERNATIONAL CONFERENCE ON INSTRUMENTATION & MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC 2016) | 2016年
关键词：
attitude tracking control; flexible spacecraft; sliding mode control; adaptive law; vibration suppression;
D O I：
10.1109/IMCCC.2016.69
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 an adaptive sliding mode controller is proposed for attitude tracking of flexible spacecraft, in which adaptive mechanism is adopted to estimate disturbances with unknown upper bounds and inertia parameters. A nonlinear observer is designed to estimate vibration modes of flexible appendages so that the vibration can be actively suppressed. The stability of the closed-loop system is proved by Lyapunov technique. Simulation results show that the proposed algorithms can achieve attitude tracking control and effectively suppress induced vibrations of flexible appendages..
引用
收藏
页码：400 / 404
页数：5
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