Fuzzy Adaptive Variable Structure Active Attitude Control of Flexible Spacecraft

被引：1
|
作者：
Qu, Fayi [1 ]
Zhu, Liangkuan [1 ]
Song, Wenlong [1 ]
机构：
[1] NE Forestry Univ, Sch Electromech Engn, Harbin 150040, Peoples R China
来源：
FRONTIERS OF MANUFACTURING AND DESIGN SCIENCE, PTS 1-4 | 2011年 / 44-47卷
关键词：
Flexible Spacecraft; Active Control; Fuzzy Control; Variable Structure Control;
D O I：
10.4028/www.scientific.net/AMM.44-47.2070
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
This paper presents a novel control system design method for the three-axis-rotational tracking and vibration stabilization of a spacecraft with flexible appendages. Based on the sliding control theory, a robust attitude control law is derived to control the attitude motion of spacecraft. For actively suppressing the induced vibration, both fuzzy methods and strain rate feedback (SRF) control methods are presented. Numerical simulations are performed to show the feasibility and effeteness of the proposed methods.
引用
收藏
页码：2070 / 2074
页数：5
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