Attitude stabilization for aircraft under angular velocity constraint

被引：0

作者：

Yu, Bo ^{[1
,2
]}

Wang, LiNan ^{[1
,2
]}

Du, HaiBo ^{[1
,2
]}

Zhou, Jun ^{[1
,2
]}

Wu, Di ^{[3
]}

Ding, ShiHong ^{[4
]}

机构：

[1] Hefei Univ Technol, Sch Elect Engn & Automat, Hefei 230009, Anhui, Peoples R China

[2] Hefei Univ Technol, Anhui Prov Engn Res Ctr Ind Automat, Hefei 230009, Anhui, Peoples R China

[3] Southeast Univ, Sch Automat, Nanjing 210096, Jiangsu, Peoples R China

[4] Jiangsu Univ, Sch Elect & Informat Engn, Zhenjiang 212013, Jiangsu, Peoples R China

来源：

IECON 2020: THE 46TH ANNUAL CONFERENCE OF THE IEEE INDUSTRIAL ELECTRONICS SOCIETY | 2020年

基金：

中国国家自然科学基金;

关键词：

attitude control; angular velocity constraint; finite-time interference compensation; TRACKING; SPACECRAFT;

D O I：

10.1109/iecon43393.2020.9254830

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper mainly investigates the attitude control problem for a spacecraft. Not only angular velocity constraint but also external disturbances are considered in the system model. Under the action of proposed controller, the posture can be converged to the desired value, and the angular velocity can be asymptotically converged to the origin.

引用

页码：5083 / 5087

页数：5

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