舰载无人机掩护预警直升机诱偏反辐射导弹分析  

Analysis of Shipborne UAV Trick ARM for Covering Early-Warning Helicopter

作　　者：尹成义[1] 谭安胜[1] 

机构地区：[1]海军大连舰艇学院

出　　处：《指挥控制与仿真》2015年第5期19-23,共5页Command Control & Simulation

基　　金：军事类研究生资助课题(2013JY446)

摘　　要：针对反辐射导弹对预警直升机的威胁,给出了舰载无人机携带辐射源诱偏反辐射导弹的基本原理;从反辐射导弹的空间分辨条件和几何运动分析出发,建立了无人机携带辐射源和预警直升机共同组成的两点源诱偏反辐射导弹的数学模型和预警直升机与无人机的最佳间距模型。通过仿真计算,分析了各种因素对诱偏效果的影响。Aimming at the threat of ARM toward shipborne early-warning helicopter,the principle of shipborne UAV carrying radiation source to trick ARM is proposed. Based on spatial resolution condition and the geometry movement analysis of ARM,the mathematic model of two radiation sources decoy system consisted of UAV carrying radiation source and earlywarning helicopter to trick ARM and the best space model between early-warning helicopter and UAV are deduced. Through simulating calculation,various factors influencing on the tricking effect is analyzed.

关 键 词：舰载无人机 舰载预警直升机 反辐射导弹 诱偏 

分 类 号：E926.3[军事—军事装备学] V279[兵器科学与技术—武器系统与运用工程]