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Phugoid peaks trajectory for hypersonic glide vehicles

机译:高超声速滑行飞行器的坡峰轨迹

摘要

A new apparatus and method for determining trajectories for hypersonic glide vehicles significantly reduces integrated, or total, heat load, with little reduction in time to distance and maximum range. The new approach identifies a trajectory having large phugoid oscillations and plotting a glide trajectory along the peaks of the phugoid oscillations. The glide trajectory is determined by calculating a first altitude that results in a maximum lift to drag ratio trajectory having damped or small phugoid oscillations, then calculating a different altitude that results in larger phugoid oscillations, and higher phugoid peaks, and finally plotting a trajectory from the first altitude that follows the peaks of the higher phugoid oscillation trajectory. The thus calculated trajectory can be input into a glide vehicle guidance system for controlling the trajectory of the glide vehicle from a point where it reaches the first altitude.
机译:一种用于确定高超音速滑行飞行器的轨迹的新设备和方法,可以显着减少总的或总的热负荷,而到距离和最大范围的时间却很少减少。新方法识别出具有大的蛇形振动的轨迹,并沿着蛇形振动的峰值绘制滑行轨迹。确定滑行轨迹的方法是:计算导致高度最大的升力/阻力比轨迹具有衰减的或小的浮子振荡的第一高度,然后计算导致更大的浮子振荡和更高的浮子峰的不同高度,最后绘制一条轨迹沿着较高的蛇形振荡轨迹的峰值的第一个高度。这样计算出的轨迹可以输入到滑行车辆引导系统中,以从滑行车辆到达第一高度的点来控制滑行车辆的轨迹。

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