QQ客服 官方微博 反馈留言

	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。