反辐射导弹的角度型制导方法研究  

Research on Angle Type Guidance Method for Anti-radar Missiles

作　　者：唐道光 张意 刘叙含 王乔 李涛 杨丹 TANG Daoguang;ZHANG Yi;LIU Xuhan;WANG Qiao;LI Tao;YANG Dan(School of Electrical and Control Engineering,North University of China,Taiyuan 030051,China;Xi'an Modern Control Technology Research Institute,Xi'an 710065,China;Technology Center,Southwest Computer Co.,Ltd.,Chongqing 400060,China)

机构地区：[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

出　　处：《弹箭与制导学报》2022年第3期5-10,共6页Journal of Projectiles,Rockets,Missiles and Guidance

基　　金：国家自然科学基金面上项目(61873247)资助。

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。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.

关 键 词：反辐射导弹 制导方法 积分比例导引 速度追踪 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]