Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints

doi:10.1007/s11633-016-0953-y

CASIA OpenIR > 学术期刊 > Machine Intelligence Research

	Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints
	Hui-Bo Zhou 1,2; Jun-Hong Song 2; Shen-Min Song 2
发表期刊	International Journal of Automation and Computing
ISSN	1476-8186
	2018
卷号	15 期号:2 页码:218-227
摘要	In order to improve the precision of guidance for the missile intercepting maneuvering targets, this paper proposes a sliding mode guidance law with impact angle constraints based on the equation of the relative motion of the missile and the target in a 2D plane. Two finite-time convergent guidance laws are proposed based on the nonsingular terminal sliding mode, while, two exponential convergent guidance laws involving dynamic delay are developed through applying the higher-order nonsingular terminal sliding mode. The simulations denote that, in all the four scenarios of the target0s maneuvering, the guidance laws are able to inhibit the chattering phenomenon of the sliding modes effectively; and from an expected aspect angle, the missiles could attack the targets with high precision and fast speed.
关键词	Autopilot impact angle nonsingular terminal sliding mode finite-time convergent guidance.
DOI	10.1007/s11633-016-0953-y
引用统计	被引频次：7[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://ir.ia.ac.cn/handle/173211/42404
专题	学术期刊_Machine Intelligence Research
作者单位	1.School of Mathematical Sciences, Harbin Normal University, Harbin 150009, China 2.Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China
推荐引用方式 GB/T 7714	Hui-Bo Zhou,Jun-Hong Song,Shen-Min Song. Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints[J]. International Journal of Automation and Computing,2018,15(2):218-227.
APA	Hui-Bo Zhou,Jun-Hong Song,&Shen-Min Song.(2018).Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints.International Journal of Automation and Computing,15(2),218-227.
MLA	Hui-Bo Zhou,et al."Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints".International Journal of Automation and Computing 15.2(2018):218-227.

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