Robust adaptive variable structure control of a flexible spacecraft containing input nonlinearity/dead-zone

被引：1

作者：

Hu, Qinglei ^{[1
]}

Ma, Guangfu ^{[1
]}

机构：

[1] Harbin Inst Technol, Dept Control Sci & Engn, Harbin 150001, Peoples R China

来源：

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 2006年 / 49卷 / 165期

关键词：

variable structure control; vibration suppression; flexible spacecraft; attitude maneuver; input nonlinearity;

D O I：

10.2322/tjsass.49.187

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

There is no abstract available for the item entitled Robust adaptive variable structure control of a flexible spacecraft containing input nonlinearity/dead-zone.

引用

页码：187 / 191

页数：5

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