CAJ | 학술논문

为研究歼击机拦截巡航导弹时的拦截阵位问题，构建了歼击机拦截阵位模型。在分析歼击机拦截来袭巡航导弹过程的基础上，根据歼击机的运动模型和歼击机接敌方法，确定了拦截阵位相关参数，并以机载导弹对巡航导弹杀伤概率为目标函数进行仿真研究。仿真结果找出了一定条件下歼击机的最优航向前置角范围，为反巡航导弹作战理论研究提供了参考。
위연구섬격궤란절순항도탄시적란절진위문제，구건료섬격궤란절진위모형。재분석섬격궤란절래습순항도탄과정적기출상，근거섬격궤적운동모형화섬격궤접활방법，학정료란절진위상관삼수，병이궤재도탄대순항도탄살상개솔위목표함수진행방진연구。방진결과조출료일정조건하섬격궤적최우항향전치각범위，위반순항도탄작전이론연구제공료삼고。
For researching the lineup of the fighter plane heading off the cruise missile, the model of the fighter plane heading off the cruise missile lineup is established. Based on analyzing the process of the fighter plane heading off the cruise missile, the parameters of the lineup is confirmed according to the movement model and the adjacency enemy method of the fighter plane. Aiming at the probability of killing the cruise missile, the simulation is carried out. The best course pre-positive-angle range is found, which makes reference for the theory of the fighter plane heading off the cruise missile.