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. |
个性服务 |
查看访问统计 |
相关权益政策 |
暂无数据 |
收藏/分享 |
除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。
修改评论