Magnetic Attitude Control Using Fuzzy Logic

被引：4
|
作者：
Heydari, Ali [1 ]
Pourtakdoust, Seid H. [2 ]
机构：
[1] Sharif Univ Technol, Dept Aerosp Engn, Tehran, Iran
[2] Sharif Univ Technol, Ctr Res & Dev Space Sci & Technol, Dept Aerosp Engn, Tehran, Iran
来源：
2009 IEEE CONTROL APPLICATIONS CCA & INTELLIGENT CONTROL (ISIC), VOLS 1-3 | 2009年
关键词：
SUBJECT;
D O I：
10.1109/CCA.2009.5280979
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 fuzzy controller has been suggested for attitude control of magnetic actuated satellites in order to calculate the desired mechanical torque based on the attitude error including error in the angles and their rates. The problem of selecting proper magnetic dipole based on the known desired mechanical torque has been investigated, two different methods for the purpose has been suggested and the performance of the attained fuzzy magnetic attitude controllers has been shown under two different simulated conditions.
引用
收藏
页码：456 / +
页数：3
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