使用集成元估计器的数据驱动飞机轨迹预测

A. M. Hernández, Enrique J. Casado Magaña, A. Berná
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引用次数: 8

摘要

飞机轨迹预测是当今空中交通管理和管制环境中开发和实施新概念和工具的核心任务。传统上,这个问题是通过使用复杂的基于模型的方法来解决的,这种方法不考虑对飞机轨迹的实际演变有很大影响的战术情况。目前,重点已经转向数据驱动方法的应用,由于使用记录轨迹信息训练的学习算法,可以采用这些因素。在本文中,飞机轨迹预测问题被表述为一个回归问题,通过最先进的集成机器学习技术来解决。所选择的算法已经使用来自实际监测记录数据的重建轨迹数据集进行了训练。一旦经过训练,计算轨迹预测,它们只会得到航班起飞前可用的信息(即提交的飞行计划和天气预报)。然后,比较了不同集合元估计器家族发布的预测,以衡量其作为数据驱动轨迹预测器的适用性和准确性。主要结果表明,本文中提出的数据驱动预测器有可能在指定的轨迹点估计参数,如估计到达时间,平均误差约为10秒,这对于ATM目的来说是非凡的结果,飞机质量平均范围约为75公斤,因此可能实现非常精确的未来环境影响评估。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Data-driven Aircraft Trajectory Predictions using Ensemble Meta-Estimators
Aircraft trajectory prediction is nowadays a core task in the development and implementation of new concepts and tools within the Air Traffic Management and Control environment. Traditionally, this problem has been tackled by the usage of sophisticated model-based approaches that do not consider tactical situations that greatly influence the actual evolution of the aircraft's trajectory. Currently, the focus has shifted towards the application of data-driven methods, which enable the adoption of these factors thanks to learning algorithms trained with recorded trajectory information. In this paper, the aircraft trajectory prediction problem is formulated as a regression problem to be solved by state-of-the-art ensemble machine learning techniques. The selected algorithms have been trained using reconstructed trajectory datasets derived from actual surveillance recorded data. Once trained, to compute a trajectory prediction, they are fed only by information available prior to the flight departure (i.e. filed Flight Plans and weather forecasts). Then, the predictions issued by the different families of ensemble meta-estimators are compared to weigh their suitability and accuracy as data-driven trajectory predictors. The main results show that the data-driven predictors presented in this paper are potentially able to estimate parameters at a designated trajectory points such as the Estimated Time of Arrival within an average error of ≈ 10 sec, which represents extraordinary results for ATM purposes, and the aircraft mass within an average range of ≈75 kg, thus possibly enabling very highly accurate future environmental impact assessments.
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