| Spacecraft attitude maneuver control using two parallel mounted 3-DOF spherical actuators | |
| Li Guidan1; * Li Haike2; Li Bin1 | |
| 刊名 | Chinese Journal of Aeronautics
 |
| 2017 | |
| 卷号 | 第30卷页码:P419-425 |
| 关键词 | Attitude maneuver/Backstepping control/Null motion/Parallel configuration/Singularity/Spherical actuator |
| ISSN号 | 1000-9361 |
| URL标识 | 查看原文 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/2930247 |
| 专题 | 天津大学 |
| 作者单位 | 1.School of Electrical and Information Engineering, Tianjin University, Tianjin, 300072/2.State Grid Tianjin Power Dongli Power Supply Branch, Tianjin, 300300 |
| 推荐引用方式 GB/T 7714 | Li Guidan1,* Li Haike2,Li Bin1. Spacecraft attitude maneuver control using two parallel mounted 3-DOF spherical actuators[J]. Chinese Journal of Aeronautics,2017,第30卷:P419-425. |
| APA | Li Guidan1,* Li Haike2,&Li Bin1.(2017).Spacecraft attitude maneuver control using two parallel mounted 3-DOF spherical actuators.Chinese Journal of Aeronautics,第30卷,P419-425. |
| MLA | Li Guidan1,et al."Spacecraft attitude maneuver control using two parallel mounted 3-DOF spherical actuators".Chinese Journal of Aeronautics 第30卷(2017):P419-425. |
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