Global finite-time attitude regulation using bounded feedback for a rigid spacecraft |
| |
Authors: | Y Zhou W Zhu and H Du |
| |
Affiliation: | 1.Anhui Vocational College of Press and Publishing, Hefei Anhui 230601, China; 2.School of Electrical Engineering and Automation, Hefei University of Technology, Hefei Anhui 230009, China,School of Electrical Engineering and Automation, Hefei University of Technology, Hefei Anhui 230009, China and School of Electrical Engineering and Automation, Hefei University of Technology, Hefei Anhui 230009, China |
| |
Abstract: | This paper investigates the problem of global attitude regulation control for a rigid spacecraft under input saturation. Based on the technique of finite-time control and the switching control method, a novel global bounded finite-time attitude regulation controller is proposed. Under the proposed controller, it is shown that the spacecraft attitude can reach the desired attitude in a finite time. In addition, the bound of a proposed attitude controller can be adjusted to any small level to accommodate the actuation bound in practical implementation. |
| |
Keywords: | Global attitude regulation finite-time control bounded feedback |
本文献已被 SpringerLink 等数据库收录! |
| 点击此处可从《控制理论与应用(英文版)》浏览原始摘要信息 |
|
点击此处可从《控制理论与应用(英文版)》下载全文 |
|