Trajectory Prediction Sensitivity Analysis Using Monte Carlo Simulations Based on Inputs’ Distributions

Q2 Social Sciences
I. Rudnyk, J. Ellerbroek, J. Hoekstra
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引用次数: 8

Abstract

To facilitate the increasing amount of air traffic, current and future decision support tools for air traffic management require an efficient and accurate trajectory prediction. With uncertainty inherent to almost all inputs of a trajectory predictor, the accurate prediction is not a simple task. In this study, Monte Carlo simulations of a ground-based trajectory predictor are performed to estimate the prediction uncertainty up to 20 min look-ahead time and to assess the correlation between inputs and prediction errors. Selected inputs are aircraft bank angle, constant calibrated airspeed and Mach number speed settings, vertical speed, temporary level-offs, air temperature, lapse rate, wind, and air traffic control intent. These inputs are provided in the form of their distribution functions obtained from observed data such as surveillance data, weather forecasts, and air traffic controllers’ inputs. Simulations are performed for heavy and medium wake turbulence category aircraft. Results indicate that with 20 min look-ahead time, when outliers are not considered, along-track errors can reach up to 18 nmi, whereas altitude errors can reach up to around 13,000 ft. Cross-track errors in cruise highly depend on the lateral deviations due to Air Traffic Control instructions, and, in this study, are within 10 nmi. Wind conditions, vertical speed, calibrated airspeed, Mach number speed setting, and temporary level-offs are determined to be the most influential inputs.
基于输入分布的蒙特卡罗仿真轨迹预测灵敏度分析
为了方便不断增加的空中交通量,当前和未来的空中交通管理决策支持工具需要有效和准确的轨迹预测。由于轨迹预测器的几乎所有输入都带有不确定性,因此准确预测并不是一项简单的任务。在本研究中,进行了地面弹道预测器的蒙特卡罗模拟,以估计预测不确定性,并评估输入与预测误差之间的相关性。选择的输入是飞机倾斜角度,恒定校准空速和马赫数速度设置,垂直速度,临时平降,空气温度,下降率,风和空中交通管制意图。这些输入以分布函数的形式提供,分布函数是从观测数据(如监视数据、天气预报和空中交通管制员的输入)获得的。对重型和中型尾流型飞机进行了仿真。结果表明,在不考虑异常值的情况下,在20分钟的预瞄时间内,沿航迹误差可达18海里,而高度误差可达13000英尺左右。巡航时的跨航迹误差高度依赖于空中交通管制指令引起的横向偏差,在本研究中,误差在10海里以内。风速条件、垂直速度、校准空速、马赫数速度设置和临时平降被确定为最具影响力的输入。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Journal of Air Transportation
Journal of Air Transportation Social Sciences-Safety Research
CiteScore
2.80
自引率
0.00%
发文量
16
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