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WAKE TURBULENCE ANALYZER FOR REAL-TIME VISUALIZATION, DETECTION, AND AVOIDANCE

机译:用于实时可视化,检测和回避的尾流湍流分析仪

摘要

A computer method for determining potential wake turbulence by a first aircraft 10 from wake 12a, 12b generated by a second aircraft 14a, 14b. The computer method includes receiving a signal 16a, 16b generated by the second aircraft 14a, 14b at the first aircraft 10 and transforming the signal 16a, 16b to a first wake turbulence boundary 62, 90, 102, 112 that represents the wake 12a, 12b generated by the second aircraft 14a, 14b. An intersection volume 64, 68, which is representative of a zone of dangerous turbulence interactions, is selected for the first aircraft 10. Based on a determination of intersection between the first wake turbulence boundary 62, 90, 102, 112 and the intersection volume 64, 68, issuing a warning flag if an intersection exists or continue generating the first wake turbulence boundary 62, 90, 102, 112 and determining whether interactions exist.
机译:一种用于确定第一飞行器10从第二飞行器14a,14b产生的尾迹12a,12b潜在的尾流湍流的计算机方法。该计算机方法包括:在第一飞行器10处接收由第二飞行器14a,14b产生的信号16a,16b,并将该信号16a,16b转换成代表尾流12a,12b的第一尾流湍流边界62、90、102、112。由第二飞机14a,14b产生。为第一飞行器10选择代表危险湍流相互作用区域的相交体积64、68。基于对第一尾流湍流边界62、90、102、112与相交体积64之间的相交的确定,68,如果存在相交则发出警告标志或继续产生第一尾流湍流边界62、90、102、112,并确定是否存在相互作用。

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