反辐射导弹的角度型制导方法研究

唐道光; 张意; 刘叙含; 王乔; 李涛; 杨丹

doi:10.15892/j.cnki.djzdxb.2022.03.002

弹箭与制导学报 >

2022 , Vol. 42 >Issue 3: 5 - 10

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2022.03.002

反辐射导弹的角度型制导方法研究

唐道光 ¹ ,
张意 ² ,
刘叙含 ² ,
王乔 ² ,
李涛 ² ,
杨丹 ³

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¹ 中北大学电气与控制工程学院,太原 030051
² 西安现代控制技术研究所, 西安 710065
³ 西南计算机有限责任公司技术中心,重庆 400060

唐道光(1979—),男,重庆合川人,讲师,研究方向:飞行器嵌入式制导控制系统、自主可控计算机系统及网络安全。

收稿日期: 2021-11-10

网络出版日期: 2025-02-03

基金资助

国家自然科学基金面上项目(61873247)

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Research on Angle Type Guidance Method for Anti-radar Missiles

TANG Daoguang ¹ ,
ZHANG Yi ² ,
LIU Xuhan ² ,
WANG Qiao ² ,
LI Tao ² ,
YANG Dan ³

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¹ School of Electrical and Control Engineering, North University of China, Taiyuan 030051, China
² Xi’an Modern Control Technology Research Institute, Xi’an 710065, China
³ Technology Center, Southwest Computer Co., Ltd., Chongqing 400060, China

Received date: 2021-11-10

Online published: 2025-02-03

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摘要

在推导最优比例导引的基础上,提出了比例导引、积分比例导引和速度追踪的视线角和弹道倾角表达式。针对积分比例导引和速度追踪的高阶动力学系统,建立了具有初始航向误差的制导模型。通过对脱靶量的对比分析,说明了积分比例导引和速度追踪的制导性能。

关键词： 反辐射导弹; 制导方法; 积分比例导引; 速度追踪

本文引用格式

唐道光 , 张意 , 刘叙含 , 王乔 , 李涛 , 杨丹 . 反辐射导弹的角度型制导方法研究[J]. 弹箭与制导学报, 2022 , 42(3) : 5 -10 . DOI: 10.15892/j.cnki.djzdxb.2022.03.002

Abstract

Based on the derivation of optimal proportional navigation, the new expressions with line of sight angle and trajectory angle for proportional navigation, integral proportional navigation and velocity pursuit are proposed. The guidance model with initial heading error is developed when considering a high order dynamics system for the integral proportional navigation and velocity pursuit. Comparative analysis results of miss distance demonstrate the guidance performance of integral proportional navigation and velocity pursuit.

Key words： anti-radar missile; guidance method; integral proportion navigation; velocity pursuit

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