空-空导弹发射的火控技术分析  

Analysis of Fire Control Technique for Air-to-Air Missile Launching

作　　者：王海青[1] 王岩[1] 刘志男 解向军 WANG Haiqing;WANG Yan;LIU Zhinan;XIE Xiangjun(Shenyang Aircraft Design&Research Institute,Shenyang 110035,China;No.1 Military Representative Office of Equipment Department of PLA Air Force in Shenyang 110850,China)

机构地区：[1]沈阳飞机设计研究所,辽宁沈阳110035 [2]空军装备部驻沈阳地区第一军事代表室,辽宁沈阳110850

出　　处：《飞机设计》2020年第2期49-55,共7页Aircraft Design

摘　　要：为保证飞机在空战中发挥导弹的最大攻击能力,文中对空-空导弹发射的火控原理进行了分析,针对空-空导弹的发射特点,详细描述了发射瞬间载机、目标和导弹之间相互的运动关系,以及如何运用拦射瞄准矢量方程改善导弹在末制导段的运动条件,以保证复杂空战环境中对空中目标的有效攻击。文章最后讨论了导弹拦射前置角、目标攻击进入角和导弹离轴角的计算方法及其在座舱显示器上的显示。In order to ensure the maximum attack capability of the missile in air combat,this paper analyses the fire control principle of the air-to-air missile launching.According to the launching characteristics of the air-to-air missile,it describes in detail the movement relationship among the aircraft,the target and the missile at the moment of launching,and how to improve the missile's motion conditions in the terminal guidance phase using the interception aiming vector equation in order to ensure effective attack on air targets in complex air combat environment.At the end of this paper,the calculation methods of missile interception lead angle,tartget attacking entry angle and missile off-boresight angle and their display on cockpit display are discussed.

关 键 词：空-空导弹 导弹攻击区 火控算法 

分 类 号：V247.13[航空宇航科学与技术—飞行器设计] TP15[自动化与计算机技术—控制理论与控制工程]