空空导弹高抛弹道仿真研究  

Study on Parabola-trajectory Simulation of Air-to-air Missile

作　　者：杨雪榕[1] 梁加红[1] 李晓冬 

机构地区：[1]国防科技大学机电工程与自动化学院,长沙410073 [2]上海机电工程研究所,上海2002332

出　　处：《系统仿真学报》2010年第5期1261-1265,共5页Journal of System Simulation

基　　金：航天支撑技术基金项目(2007-HT-GFKD)

摘　　要：提出了高抛弹道以增加中近程空空导弹的有效攻击距离。为了完成高抛弹道制导任务,分别进行了初制导、中制导和末制导三阶段制导参数仿真分析研究,给出了高抛弹道复合导引规律。建立了三种典型的目标机动模型,并建立了高抛弹道仿真系统。通过对不同高度、距离目标的攻击仿真结果分析,得出了此种弹道的性能特点。仿真结果显示,高抛弹道能够有效提高中近程导弹攻击距离,用于中近程导弹的技术升级。The Parabola-Trajectory was proposed,for the purpose of increase the effective attack range of the short/medium range air-to-air missile.In order to solve the Parabola-Trajectory guidance problem,parabola-trajectory compound guidance law was studied through the separate simulation study of the parameters of the three guidance stages：initial,midcourse and terminal guidance stage.The parabola-trajectory simulation system was built,which includes three typical maneuver targets models.By the analyses of simulation results of attacking various targets with different heights and distances,the characteristics of the trajectory were shown.The simulation shows that the parabola-trajectory can effectively increase the attack range of the missile,and can be used in the missile＇s technical upgrade.

关 键 词：空空导弹 高抛弹道 复合制导律 仿真 

分 类 号：TJ765.1[兵器科学与技术—武器系统与运用工程]