Active Vibration Suppression and Attitude Maneuvers of flexible spacecraft via Fuzzy Sliding Control

被引：2
|
作者：
Zhu, Liangkuan [1 ]
Song, Wenlong [1 ]
Hu, Qinglei [2 ]
机构：
[1] Northeast Forestry Univ, Sch Electromech Engn, Harbin, Heilongjiang Pr, Peoples R China
[2] Harbin Inst Technol, Dept Control Sci & Engn, Harbin, Peoples R China
来源：
2008 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-11 | 2008年
关键词：
Flexible spacecraft; Fuzzy sliding mode control; Attitude maneuvering;
D O I：
10.1109/CCDC.2008.4598014
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 robust control approach is presented for the attitude maneuvering control and vibration damping of a spacecraft with flexible appendages. Firstly, a new attitude maneuvering controller based on the sliding mode control (SMC) is derived to control the attitude motion of spacecraft. Secondly, the discontinuity in the sliding mode controller is smoothed in side a thin boundary layer by using fuzzy logic technique so that the chattering phenomenon is eliminated efficiently. Thirdly, positive position feedback (PPF) is provided to suppress the induced vibration. Numerical simulations demonstrate the feasibility and effectiveness of the control strategy.
引用
收藏
页码：3665 / +
页数：2
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