Application of Fuzzy Controllers for Spacecraft Attitude Control

被引：28

作者：

Cheng, Chin-Hsing ^{[1
]}

Shu, Sheng-Li ^{[1
]}

机构：

[1] Feng Chia Univ, Dept Elect Engn, Taichung 40724, Taiwan

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2009年 / 45卷 / 02期

关键词：

Attitude control; Control systems; Fuzzy logic; Radar tracking; Satellites; Simulation; Steady-state;

D O I：

10.1109/TAES.2009.5089557

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The design of fuzzy controllers for the attitude stabilization of a satellite is proposed. In the first step, the original satellite controllers, two classical linearized controllers, are superseded by two fuzzy controllers. The objective is to obtain faster convergence time and lower steady-state error. The two fuzzy controllers are then consolidated to form one fuzzy controller in the next step, retaining the same effectiveness of control. Simulation tests are performed to demonstrate the effectiveness of the fuzzy controller. Inference disturbances are included in the simulation.

引用

页码：761 / 765

页数：5

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