Backstepping-based Attitude Maneuver Control and Active Vibration Reduction of Flexible Spacecraft

被引：2
|
作者：
Zhu, Liangkuan [1 ]
Liu, Yaqiu [1 ]
Wang, Dailin [1 ]
Hu, Qinglei [2 ]
机构：
[1] NE Forestry Univ, Harbin, Heilongjiang Pr, Peoples R China
[2] Harbin Inst Technol, Dept Control Sci & Engn, Harbin, Heilongjiang Pr, Peoples R China
来源：
2008 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-11 | 2008年
关键词：
Flexible spacecraft; Backstepping; Attitude maneuvering;
D O I：
10.1109/CCDC.2008.4597441
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A novel hybrid robust control design method is investigated for a three-axis-rotational maneuver and vibration stabilization of a spacecraft with flexible appendages. Based on the backstepping, a robust attitude control law is derived to control the attitude motion of spacecraft. For actively suppressing the induced vibration, strain rate feedback control methods are presented by using piezoelectric materials as additional sensors and actuators bonded on the surface of the flexible appendages. Numerical simulations demonstrate the feasibility and effectiveness of the control strategy.
引用
收藏
页码：887 / +
页数：2
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