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	Autopilot and guidance law design considering impact angle and time
	Wang, Xianghua; Tan, Chee Pin; Zhou, Donghua
刊名	IET CONTROL THEORY AND APPLICATIONS
	2018
卷号	12期号:2页码:221-232
关键词	missile control impact (mechanical) autopilot guidance law design impact angle impact time missile flight missile LOS angle missile line-of-sight angle
DOI	10.1049/iet-cta.2016.1525
URL标识	查看原文
公开日期	[db:dc_date_available]
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/4567539
专题	山东大学
作者单位	1.Shandong Univ Sci & Technol, Coll Elect Engn & Automat, Qingdao 266590, Peoples R China. 2.Monash Uni
推荐引用方式 GB/T 7714	Wang, Xianghua,Tan, Chee Pin,Zhou, Donghua. Autopilot and guidance law design considering impact angle and time[J]. IET CONTROL THEORY AND APPLICATIONS,2018,12(2):221-232.
APA	Wang, Xianghua,Tan, Chee Pin,&Zhou, Donghua.(2018).Autopilot and guidance law design considering impact angle and time.IET CONTROL THEORY AND APPLICATIONS,12(2),221-232.
MLA	Wang, Xianghua,et al."Autopilot and guidance law design considering impact angle and time".IET CONTROL THEORY AND APPLICATIONS 12.2(2018):221-232.

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