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Semi-optimal co-ordinated manoeuvres for aircraft conflict resolution

机译：解决飞机冲突的半最佳协调演习

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摘要

In this manuscript, a new concept of 2D-semi-optimal-circular-3-arced-path manoeuvres with constant speed for multiple aircraft cooperative conflict resolution is presented. This type of manoeuvres is based on appropriate commands to heading, speed and manoeu-vreing time. According to aircraft turning dynamics, each aircraft manoeuvre is composed of three tangent circular arcs. The optimality of manoeuvres is based on the minimisation of weighted sum of kinetic energy for aircraft two-legged manoeuvres. In comparison, aircraft with lower weight factors bear more responsibility to resolve the conflicts. The effectiveness of the proposed algorithm for real time conflict resolution is guaranteed, where the number of encountering aircraft is less than five. Otherwise, the current method could also be jointed to one of the fast resolution methods, like probabilistic resolution algorithm or genetic algorithm - as a tool to choose the convex domain - to become more computationally effective. Considerable number of case studies has been done to evaluate the effectiveness of the proposed methodology, while some are presented in the paper.
机译：在这份手稿中，提出了一种新的二维恒速半圆3弧路径机动多飞机协作冲突解决方案的概念。这种类型的操纵基于对航向，速度和操纵时间的适当命令。根据飞机的转向动力学，每架飞机的机动动作均由三个切圆弧组成。操纵的最优性是基于飞机两腿操纵的动能加权总和的最小化。相比之下，重量因子较低的飞机将承担更多解决冲突的责任。在遇到飞机数量少于五架的情况下，可以保证所提出算法实时冲突解决的有效性。否则，当前方法也可以与一种快速分辨率方法结合，例如概率分辨率算法或遗传算法-作为选择凸域的工具-使其在计算上更加有效。已经进行了大量案例研究，以评估所提出方法的有效性，而本文中还介绍了一些案例研究。

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