一种求解中程空空导弹不可达区的方法

Hanghang You, Qisong Han, Minjian Yu, Huiming Ji, Zelong Ye, Xiaoqiang Zhang
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引用次数: 1

摘要

空空导弹攻击区域是空战态势评估的重要参考,在空战决策中起着重要作用。本文对空空导弹的运动学和动力学特性进行了分析和建模。分别建立了导弹在水平面和垂直平面上的运动方程,并根据比例制导法建立了制导律。针对导弹攻击区域问题,采用黄金分割法进行搜索,利用坐标变换实时计算导弹发射后的位置,最终得到导弹的不可逃逸区域。最后,通过仿真分析验证了该方法的有效性和实用性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Method to Solve the Unreachable Zone of Mid-range Air-to-Air Missile
Air-to-air missile attack area is an important reference for air combat situation assessment and plays an important role in air combat decision-making. In this paper, the kinematics and dynamics characteristics of air-to-air missile are analyzed and modeled. The motion equations of the missile are established in the horizontal plane and the vertical plane respectively, and the guidance law is established according to the proportional guidance method. Aiming at the problem of missile attack area, this paper uses golden section method to search, uses coordinate transformation to calculate the position of the missile after launch in real time, and finally obtains the non-escape area of the missile. Finally, the effectiveness and practicability of this method are verified by simulation analysis.
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