空空作战中导弹攻击距离影响因素分析  

Influencing Factor Analysis of Missile Attack Range in Air-to-air Combat

作　　者：纪德东 段恒宇 JI De-dong;DUAN Heng-yu(Shenyang Aircraft Design and Research Institute,Shenyang 110035,China)

机构地区：[1]沈阳飞机设计研究所,沈阳110035

出　　处：《航空电子技术》2024年第2期1-9,共9页Avionics Technology

摘　　要：在中远距空空作战中,导弹攻击距离受发射速度、发射高度、发射离轴角、发射倾角等多种因素影响。以空空导弹为研究对象,旨在通过设置不同的发射条件和目标机动条件,分析得出影响空空导弹的最大攻击距离的规律。据此,提出一种兼顾空空导弹攻击效能与载机生存能力的空战战术。经仿真验证,采用该战术策略能够显著提高空空导弹攻击距离,并压缩对方空空导弹攻击距离。研究结论对空空作战规律研究、空战策略设计具有重要参考价值。In medium and long range air-to-air operations,missile attack range is subject to various factors such as launching velocity,launching altitude,off-axis angle and inclination angle.By setting different launching conditions of the air-to-air missile and target maneuver scenarios,influence of the mentioned factors associated with missile attack range is concluded.Therefore,a set of tactics balancing air-to-air missile attack eficiency and survivability of aircraft is proposed.Simulation results have shown the obvious improvement of air-to-air missile attack range with such tactics.Meanwhile,air-to-air missile attack range of hostile forces is reduced.Research conclusions are of valuable reference for air-to-air combat rules and strategies.

关 键 词：空空导弹 攻击距离 敏感性分析 战术策略 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计]