Attitude control of a satellite using fuzzy controllers

被引：33

作者：

Cheng, Chin-Hsing ^{[1
]}

Shu, Sheng-Li ^{[1
]}

Cheng, Po-Jen ^{[2
]}

机构：

[1] Feng Chia Univ, Dept Elect Engn, Taichung 407, Taiwan

[2] Nan Jeon Inst Technol, Dept Elect Engn, Yenshui 737, Tainan Hsien, Taiwan

来源：

EXPERT SYSTEMS WITH APPLICATIONS | 2009年 / 36卷 / 03期

关键词：

ROCSAT-1; Fuzzy controller; Attitude stabilization;

D O I：

10.1016/j.eswa.2008.08.053

中图分类号：

TP18 [人工智能理论];

学科分类号：

081104 ; 0812 ; 0835 ; 1405 ;

摘要：

This paper proposes the design of fuzzy controllers for the attitude stabilization of the Republic of China Satellite (ROCSAT-1). In the first step, the original satellite controllers, two classical linearized controllers, are Superseded by two fuzzy controllers. The objective is to obtain faster convergent time and lower steady-state error. The two fuzzy controllers will be consolidated to form one fuzzy controller in the next step, to obtain the same effectiveness of control. To demonstrate a fuzzy controller's performance, interference to disturb the attitude stabilization is added during the simulation. (C) 2008 Elsevier Ltd. All rights reserved.

引用

页码：6613 / 6620

页数：8

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