垂直发射微小型地-空导弹可拦截区的计算  

Algorithm of Intercepted Zone for Vertical Launched Minitype Land-to-Air Missile

作　　者：刘经纬[1] 南英[1] 

机构地区：[1]南昌航空大学自动化学院,江西南昌330063

出　　处：《飞行力学》2008年第5期43-46,共4页Flight Dynamics

摘　　要：建立了导弹及目标的飞行数学模型,给出了地-空导弹可拦截区的计算方法,对导弹及目标的对抗飞行运动进行了仿真。对仿真结果进行综合分析后认为,导弹可拦截区主要由以下因素决定:导弹发动机与机动能力、导弹-目标相对位置与目标的初始速度矢量、目标的机动飞行能力等。所给出的导弹可拦截区算法可以计算出任意情况下的可拦截区。This paper built the mathematical model of the missile-target, and introduced the algorithm of land- to-air missile intercepted zone. Then by employing the algorithm, a great deal of flight numerical simulations have been gotten for intercepted zones considering many kinds of situations, such as different relative positions between the missile and target, target initial velocity vector, target optimal maneuver, and so on. The flight numerical simulation of missile and target was done. Finally, this paper made an analysis of the simulation results.

关 键 词：微小型地-空导弹 可拦截区 飞行数值仿真 

分 类 号：V448.21[航空宇航科学与技术—飞行器设计] TJ762.13[兵器科学与技术—武器系统与运用工程]