基于滑模变结构制导律的捕获区分析

doi:10.12305/j.issn.1001-506X.2021.11.33

Abstract

Abstract:

Aiming at the condition setting problem of interceptor's mid-terminal guidance succession, the capture region with sliding mode variable structure guidance law as terminal guidance law is analyzed. Firstly, the relative motion model of missile in terminal guidance section is established based on the background of near space combat. Secondly, based on the sliding mode variable structure control theory, a sliding mode variable structure guidance law which can ensure the interception terminal overload convergent and has good performance is designed as the terminal guidance law, and its stability is analyzed. Thirdly, the condition of zero control interception is analyzed, and the capture region of sliding mode variable structure guidance law is deduced, analyzed and proved theoretically, and the boundary of the capture region is obtained. Finally, simulation experiments under four scenarios are designed to verify the correctness region analysis in the paper.

Key words: capture region, sliding mode variable structure, zero control interception, terminal guidance law

CLC Number:

TJ765

Wanli LI, Jiong LI, Humin LEI, Changxin LUO, Shijie LI. Analysis of capture region based on sliding mode variable structure guidance law[J]. Systems Engineering and Electronics, 2021, 43(11): 3321-3329.

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项目	参数
项目	X/km	Y/km	V/(m·s^-1)
拦截弹	200	38.7	1 600
目标	300	30	3 200

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Analysis of capture region based on sliding mode variable structure guidance law

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