| Bounded finite-time attitude tracking control for rigid spacecraft via output feedback | |
| Zhang, Jian; Hu, Qinglei; Wang, Danwei | |
| 刊名 | AEROSPACE SCIENCE AND TECHNOLOGY
 |
| 2017 | |
| 卷号 | 64页码:75-84 |
| 关键词 | Rigid spacecraft Finite-time observer Finite-time control Attitude tracking Actuator saturation |
| ISSN号 | 1270-9638 |
| DOI | 10.1016/j.ast.2017.01.020 |
| URL标识 | 查看原文 |
| 收录类别 | SCIE ; EI |
| WOS记录号 | WOS:000397076800001 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/5941795 |
| 专题 | 北京航空航天大学 |
| 推荐引用方式 GB/T 7714 | Zhang, Jian,Hu, Qinglei,Wang, Danwei. Bounded finite-time attitude tracking control for rigid spacecraft via output feedback[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2017,64:75-84. |
| APA | Zhang, Jian,Hu, Qinglei,&Wang, Danwei.(2017).Bounded finite-time attitude tracking control for rigid spacecraft via output feedback.AEROSPACE SCIENCE AND TECHNOLOGY,64,75-84. |
| MLA | Zhang, Jian,et al."Bounded finite-time attitude tracking control for rigid spacecraft via output feedback".AEROSPACE SCIENCE AND TECHNOLOGY 64(2017):75-84. |
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