On-line orbit determinative method for satellites with continuous thrust acceleration | |
Li, Heng-Nian; Li, Ji-Sheng; Huang, Yong-Xuan | |
刊名 | Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
![]() |
2010 | |
卷号 | 32期号:9页码:1957-1961 |
关键词 | Continuous thrusts Extend kalman filters Geo-stationary orbits Measurement equations Orbit determination Orbital maneuvers Orbital parameters Research activities |
ISSN号 | 1001-506X |
DOI | 10.3969/j.issn.1001-506X.2010.09.36 |
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/4809542 |
专题 | 西安交通大学 |
推荐引用方式 GB/T 7714 | Li, Heng-Nian,Li, Ji-Sheng,Huang, Yong-Xuan. On-line orbit determinative method for satellites with continuous thrust acceleration[J]. Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics,2010,32(9):1957-1961. |
APA | Li, Heng-Nian,Li, Ji-Sheng,&Huang, Yong-Xuan.(2010).On-line orbit determinative method for satellites with continuous thrust acceleration.Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics,32(9),1957-1961. |
MLA | Li, Heng-Nian,et al."On-line orbit determinative method for satellites with continuous thrust acceleration".Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics 32.9(2010):1957-1961. |
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