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对美国X-51A四次飞行试验进行综合研究,在X-51A飞行轨迹的基础上,利用数值方法研究初始高度、速度及爬升角对未来高超声速导弹弹道的影响,分析了临近空间高超声速导弹各阶段弹道特点,最后在MATLAB环境下进行临近空间高超声速导弹弹道仿真,分析了目标速度、高度、飞行时间和水平距离之间的相互关系,为后期有针对性拦截临近空间高超声速导弹提供参考。
Based on the X-51A flight path, the paper studies the effect of the initial altitude, velocity and angle of climb on the trajectory of future hypersonic missiles based on the X-51A flight path. The effects of adjacent space hypersonic missiles Finally, the trajectory simulation of the near-space hypersonic missile is carried out in the MATLAB environment, and the correlation between the target velocity, altitude, flight time and horizontal distance is analyzed to provide reference for the targeted interception of the near-space hypersonic missile in the later stage .