| Unified attitude control for spacecraft under velocity and control constraints | |
| Hu, Qinglei; Tan, Xiao | |
| 刊名 | AEROSPACE SCIENCE AND TECHNOLOGY
 |
| 2017 | |
| 卷号 | 67页码:257-264 |
| 关键词 | Spacecraft Attitude control Control input saturation Velocity constraint Anti-unwinding |
| ISSN号 | 1270-9638 |
| DOI | 10.1016/j.ast.2017.04.009 |
| URL标识 | 查看原文 |
| 收录类别 | SCIE ; EI |
| WOS记录号 | WOS:000405053600026 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/5940209 |
| 专题 | 北京航空航天大学 |
| 推荐引用方式 GB/T 7714 | Hu, Qinglei,Tan, Xiao. Unified attitude control for spacecraft under velocity and control constraints[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2017,67:257-264. |
| APA | Hu, Qinglei,&Tan, Xiao.(2017).Unified attitude control for spacecraft under velocity and control constraints.AEROSPACE SCIENCE AND TECHNOLOGY,67,257-264. |
| MLA | Hu, Qinglei,et al."Unified attitude control for spacecraft under velocity and control constraints".AEROSPACE SCIENCE AND TECHNOLOGY 67(2017):257-264. |
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