High-precision control method for the satellite with large rotating components

被引：9

作者：

Wang, Feng ^{[1
]}

Wang, Chi ^{[1
]}

Chen, Xue-qin ^{[1
]}

Yue, Cheng-fei ^{[1
]}

Xie, Yi-fei ^{[1
]}

Chai, Li-peng ^{[1
]}

机构：

[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150001, Heilongjiang, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2019年 / 92卷

基金：

中国国家自然科学基金;

关键词：

Rotating component; Dynamic unbalance; Sliding mode control; ROTOR-BEARING SYSTEM; NONLINEAR-SYSTEMS; UNBALANCE;

D O I：

10.1016/j.ast.2019.05.036

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Satellites with large rotating components may accomplish some specific scientific missions and have attracted a great deal of research interests. This paper investigates the control problem of such satellites. The model of the rotating component is carefully studied and both the static and dynamic unbalance are analyzed and demonstrated. To achieve a high precision control with unbalance rejection, a sliding mode control strategy is proposed. Practical simulations are conducted to verify the effectiveness of the proposed controller and simulation results illustrate that both the static and dynamic unbalance are perfectly compensated and a high-precision control is achieved. (C) 2019 Elsevier Masson SAS. All rights reserved.

引用

页码：91 / 98

页数：8

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