| Constant-gain EKF algorithm for satellite attitude determination systems | |
| Hua, Song; Huang, Huiyin; Yin, Fangfang; Wei, Chunling | |
| 刊名 | AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
 |
| 2018 | |
| 卷号 | 90页码:1259-1271 |
| 关键词 | Projection method Kalman filter Constant-gain Satellite attitude determination system Star tracker |
| ISSN号 | 1748-8842 |
| DOI | 10.1108/AEAT-03-2017-0088 |
| URL标识 | 查看原文 |
| 收录类别 | SCIE |
| WOS记录号 | WOS:000450641900012 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/5928426 |
| 专题 | 北京航空航天大学 |
| 推荐引用方式 GB/T 7714 | Hua, Song,Huang, Huiyin,Yin, Fangfang,et al. Constant-gain EKF algorithm for satellite attitude determination systems[J]. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY,2018,90:1259-1271. |
| APA | Hua, Song,Huang, Huiyin,Yin, Fangfang,&Wei, Chunling.(2018).Constant-gain EKF algorithm for satellite attitude determination systems.AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY,90,1259-1271. |
| MLA | Hua, Song,et al."Constant-gain EKF algorithm for satellite attitude determination systems".AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY 90(2018):1259-1271. |
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