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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（即无敏捷性载机对敏捷性目标、敏捷性载机对无敏捷性目标）下的空空导弹攻击区。并对计算结果进行了分析，得出了飞机敏捷性对导弹攻击区的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。
Based on theories and techniques of flight mechanics and control, missile guidance and attack zone, computer simulation and so on, an agility vector estimation method is proposed for the three-axis direction of the aircraft. A ballistic equations for solving the attack zone are established. Solve the missile attack area. The air-to-air missile attack zone under both cases (ie, no agility carrier agility target and no agility carrier agility target) is obtained through numerical calculation. The results of the calculation are analyzed, and the influence rule of aircraft agility on missile attack area and the optimal strategy of attack and defense are obtained, which provides reference for air combat decision-making and pre-research design of new aircraft.