Fuzzy Control of Fuel Sloshing in a Spacecraft

被引：0

作者：

Navabi, M. ^{[1
]}

Davoodi, Ali ^{[1
]}

机构：

[1] Shahid Beheshti Univ, Fac New Technol Engn, GC, Tehran, Iran

来源：

2018 6TH IRANIAN JOINT CONGRESS ON FUZZY AND INTELLIGENT SYSTEMS (CFIS) | 2018年

关键词：

fuzzy controller; fuel slosh; coupled dynamics;

D O I：

暂无

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 studies effect of fuzzy controller on fuel sloshing dynamics in orbital maneuvering of the spacecraft. For this aim, a mathematical model of coupled dynamics of spacecraft and fuel sloshing is developed. Then, a classic controller is applied on equations of coupled motion, and because this controller has no good responsibility, therefore a fuzzy controller is suggested in this case. Also, its shown fuzzy controller is more robust than classic controller. In both designed controller law, the controller inputs are three moments about center of mass of the spacecraft and two gimbal deflections angles.

引用

页码：123 / 126

页数：4

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