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Causal Effects of Landing Parameters on Runway Occupancy Time using Causal Machine Learning Models

机译:使用因果机学习模型对跑道占用时间降落参数的因果影响

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Limited runway capacity is a common problem faced by most airports worldwide. The two important factors that affect runway throughput are the wake-vortex separation and Runway Occupancy Time (ROT). Therefore, to improve runway throughput, Wake Turbulence Re-categorisation program (RECAT) was introduced to reduce the minimum separation distance required between successive aircraft on final approach. As a result, the constraining impact of ROT on runway throughput has now become significant. The objective of this paper is to identify data-driven intervention to reduce the ROT of landing aircraft. Specifically, we propose a data-driven approach to estimate the causal effect of landing parameters on ROT. We propose categorisation of each landing parameter into groups using Gaussian process models and employ Generalised Random Forest (GRF) to estimate the average treatment effect and the standard deviation of each landing parameters. Experimental results show that a few procedural changes to current landing procedure may reduce ROT. The results establish that slowing down the aircraft speed in the final approach phase leads to shorter ROT. In the final approach phase, ROTs of aircraft which are at least 10 knots slower than the average aircraft speed are on an average 2.63 seconds shorter. Furthermore, aircraft that are at least 10 knots faster than the average aircraft have on average 4 seconds longer ROTs. The second finding of this work is that flexible glide-slope angles should be introduced for the different aircraft types to achieve better ROT performance. Therefore, our findings also validate the industry need for Ground-Based Augmented System landing system which provides landing guidance with flexible glide-slopes.
机译:有限的跑道容量是全球大多数机场面临的常见问题。影响跑道吞吐量的两个重要因素是唤醒 - 涡旋分离和跑道入住时间(腐烂)。因此,为了提高跑道吞吐量,引入了唤醒湍流重新分类程序(RECAT),以减少连续飞机在最终方法之间所需的最小分离距离。结果,腐烂对跑道吞吐量的约束影响现在变得显着。本文的目的是识别数据驱动的干预以减少着陆飞机的腐烂。具体地,我们提出了一种数据驱动的方法来估计着陆参数对腐烂的因果效应。我们向使用高斯工艺模型进行分类,并采用广泛的随机森林(GRF)来估计每个着陆参数的平均治疗效果和标准偏差。实验结果表明,目前着陆程序的一些程序变化可能会减少腐烂。结果建立了最终方法中的飞机速度放缓,导致腐烂更短。在最终的方法中,飞机的痕迹比平均飞机速度慢的至少10节较短,平均为2.63秒。此外,比平均飞机至少为10节的飞机平均越长,越来越长。第二种发现这项工作是柔性滑坡角度应引入不同的飞机类型以实现更好的腐烂性能。因此,我们的调查结果还验证了行业的基于地面增强系统着陆系统,该系统提供了柔性滑坡的着陆引导。

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