| 摘要: |
| 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. |
| 关键词: Global attitude regulation, finite-time control, bounded feedback |
| DOI： |
|
| 基金项目:This work was supported by the National Natural Science Foundation of China (Nos. 61304007, 61673153), the Ph.D. Programs Foundation of Ministry of Education of China (No. 20130111120007) and the China Postdoctoral Science Foundation Funded Project (Nos. 2012M521217, 2014T70584). |
|
| Global finite-time attitude regulation using bounded feedback for a rigid spacecraft |
| Y. Zhou,W. Zhu,H. Du |
| (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) |
| 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. |
| Key words: Global attitude regulation, finite-time control, bounded feedback |
