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

机译:基于输入分布的蒙特卡洛模拟的轨迹预测灵敏度分析

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摘要

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.
机译:为了促进空中交通量的增加,当前和将来的空中交通管理决策支持工具需要有效而准确的轨迹预测。由于轨迹预测器的几乎所有输入都固有不确定性,因此准确的预测并不是一件容易的事。在这项研究中,对地面轨迹预测器进行了蒙特卡洛模拟,以估计高达20分钟超前时间的预测不确定性,并评估输入与预测误差之间的相关性。选定的输入是飞机倾斜角,恒定校准的空速和马赫数速度设置,垂直速度,临时水平降落,空气温度,经过率,风和空中交通管制意图。这些输入以分布函数的形式提供,这些函数是从监视数据,天气预报和空中交通管制员的输入等观测数据中获得的。针对重型和中尾流湍流类飞机进行了仿真。结果表明,在提前20分钟的时间内,不考虑离群值时,沿航迹误差可达18 nmi,而高度误差可达约13,000 ft。巡航中的跨航迹误差很大程度上取决于横向由于空中交通管制指令的原因,偏差在10 nmi以内。风的条件,垂直速度,标定的空速,马赫数速度设置和暂时的平稳状态被认为是最有影响力的输入。

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