飞机敏捷性与空空导弹攻击区综合研究

基于飞行力学与控制，导弹制导与攻击区，计算机仿真等理论和技术，针对飞机的三轴方向提出了一种敏捷性矢量的估算方法，建立了求解攻击区的弹道方程组，并利用二分法求解导弹攻击区，通过数值计算求得两种情况，（即无敏捷性载机地敏捷性目标，敏捷性载机对无敏捷性目标）下空空导弹攻击区，并对计算结果进行了分析，得出飞机敏捷性对导弹攻击区和影响规律和最优攻防策略，为空战决策和新型飞机的预研设计提供了参考。

Study of Fighter Agility and the Air to Air Missile's Attack Region

Based on flight dynamics and control, missile guidance and attack region,and computer simulation, the paper gives a method to calculate agility vector along the three axis of fighter, founds the equations to calculating the attack region, and uses half divided method to calculating the attack region. The air to air missile's attack regions are got with numerical calculating in two cases that are non agility attack fighter to agility aim fighter and agility attack fighter to non agility aim fighter. Analyses of the calculating results give the laws of fighter agility acting to the missile's attack region, and the optimal attack defense strategy for making a air fighting strategy and designing new type fighter.