| Maneuver planning of a rigid spacecraft with two skew control moment gyros | |
| Gui, Haichao; Jin, Lei; Xu, Shijie | |
| 刊名 | ACTA ASTRONAUTICA
 |
| 2014 | |
| 卷号 | 104页码:293-303 |
| 关键词 | Attitude maneuver Control moment gyro Gimbal motion restriction Single-axis pointing Single-axis rotation |
| ISSN号 | 0094-5765 |
| DOI | 10.1016/j.actaastro.2014.08.010 |
| URL标识 | 查看原文 |
| 收录类别 | SCIE ; EI |
| WOS记录号 | WOS:000343841700029 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/6548029 |
| 专题 | 北京航空航天大学 |
| 推荐引用方式 GB/T 7714 | Gui, Haichao,Jin, Lei,Xu, Shijie. Maneuver planning of a rigid spacecraft with two skew control moment gyros[J]. ACTA ASTRONAUTICA,2014,104:293-303. |
| APA | Gui, Haichao,Jin, Lei,&Xu, Shijie.(2014).Maneuver planning of a rigid spacecraft with two skew control moment gyros.ACTA ASTRONAUTICA,104,293-303. |
| MLA | Gui, Haichao,et al."Maneuver planning of a rigid spacecraft with two skew control moment gyros".ACTA ASTRONAUTICA 104(2014):293-303. |
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