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	Estimate of attitude and position of flying projectile controlled by combined guidance based on magnetometer/GPS
	Yang, Xiao-Jun; Shi, Kun-Lin; Wang, Yi-Lin
刊名	Binggong Xuebao/Acta Armamentarii
	2008
卷号	29期号:2页码:169-173
关键词	Engineering survey technology Unscented transformation
ISSN号	1000-1093
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/4847155
专题	西安交通大学
推荐引用方式 GB/T 7714	Yang, Xiao-Jun,Shi, Kun-Lin,Wang, Yi-Lin. Estimate of attitude and position of flying projectile controlled by combined guidance based on magnetometer/GPS[J]. Binggong Xuebao/Acta Armamentarii,2008,29(2):169-173.
APA	Yang, Xiao-Jun,Shi, Kun-Lin,&Wang, Yi-Lin.(2008).Estimate of attitude and position of flying projectile controlled by combined guidance based on magnetometer/GPS.Binggong Xuebao/Acta Armamentarii,29(2),169-173.
MLA	Yang, Xiao-Jun,et al."Estimate of attitude and position of flying projectile controlled by combined guidance based on magnetometer/GPS".Binggong Xuebao/Acta Armamentarii 29.2(2008):169-173.

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