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Systems and methods for calculating the approach speed maneuvers aerial refueling

机译:用于计算进近速度机动空中加油的系统和方法

摘要

Systems and methods for calculating the approach speed maneuvers air refueling. The systems include: a) capture means (31) of a sequence of digital frames from the stage of operation located approximation calibrated to know the actual distance corresponding to one pixel of a frame; b) arranged computational means to obtain the coordinates of the relative trajectory of the receiving aircraft (11) relative to the tanker aircraft (13) through the process of a sequence of frames (35, 35 ', 35' ', ...) of approach operation obtained by said capturing means (31) and calculate the speed difference between the receiver aircraft (11) and the tanker aircraft (13) from the path defined by the registered coordinates b1 process). The invention also relates to methods for the calculation of the approach speed.
机译:用于计算进近速度的系统和方法可操纵空中加油。该系统包括:a)来自操作阶段的一系列数字帧的捕获装置(31),该数字帧位于近似校准处,以知道对应于帧的一个像素的实际距离; b)布置的计算装置,以通过一系列框架(35、35',35',...)的处理来获得接收飞机(11)相对于油轮飞机(13)的相对轨迹的坐标。由所述捕获装置(31)获得的进近操作的结果,并根据由注册坐标b1过程定义的路径来计算接收飞机(11)和油轮飞机(13)之间的速度差。本发明还涉及用于计算逼近速度的方法。

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