Design of Attitude Controller Without Angular Velocity Measurement of Flexible Spacecraft

被引：0
|
作者：
Ding, Qing-Shu [1 ]
Zhang, Ying [1 ]
Zhang, Rui [2 ]
He, Liang [3 ]
机构：
[1] Harbin Inst Technol, Shenzhen Grad Sch, Shenzhen 518055, Peoples R China
[2] Shenzhen Polytech, Shenshen 518055, Peoples R China
[3] Shanghai Aerosp Control Technol Inst, Shanghai 200233, Peoples R China
来源：
2018 37TH CHINESE CONTROL CONFERENCE (CCC) | 2018年
基金：
国家自然科学基金重大项目; 中国国家自然科学基金;
关键词：
Flexible spacecraft; Without angular velocity measurement; Modal variables; Passivity;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, the design of attitude controller is investigated for a class of flexible spacecraft. Two attitude controllers are proposed for flexible spacecraft to guarantee the asymptotic stability of the closed-loop systems without using angular velocity measurement. First, a partial state feedback controller is established when the flexible modal variables are measurable and angular velocity is not available. Second, an observer based feedback controller is developed when both the modal variables and angular velocity are not available. Finally, two numerical examples are provided to illustrate the effectiveness of two given controllers.
引用
收藏
页码：885 / 890
页数：6
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