| Integration of Star and Inertial Sensors for Spacecraft Attitude Determination | |
| Wang, Kedong; Zhu, Tongqian; Qin, Yujie; Zhang, Chao; Li, Yong | |
| 刊名 | JOURNAL OF NAVIGATION
 |
| 2017 | |
| 卷号 | 70页码:1335-1348 |
| 关键词 | Star sensor Celestial navigation system Inertial navigation system Kalman filter |
| ISSN号 | 0373-4633 |
| DOI | 10.1017/S0373463317000339 |
| URL标识 | 查看原文 |
| 收录类别 | SCIE |
| WOS记录号 | WOS:000412540200010 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/5937595 |
| 专题 | 北京航空航天大学 |
| 推荐引用方式 GB/T 7714 | Wang, Kedong,Zhu, Tongqian,Qin, Yujie,et al. Integration of Star and Inertial Sensors for Spacecraft Attitude Determination[J]. JOURNAL OF NAVIGATION,2017,70:1335-1348. |
| APA | Wang, Kedong,Zhu, Tongqian,Qin, Yujie,Zhang, Chao,&Li, Yong.(2017).Integration of Star and Inertial Sensors for Spacecraft Attitude Determination.JOURNAL OF NAVIGATION,70,1335-1348. |
| MLA | Wang, Kedong,et al."Integration of Star and Inertial Sensors for Spacecraft Attitude Determination".JOURNAL OF NAVIGATION 70(2017):1335-1348. |
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