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Trajectory Prediction Sensitivity Analysis Using Monte Carlo Simulations

机译:使用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 efficient and accurate trajectory predictors. With uncertainty inherent to almost all inputs of a trajectory predictor, accurate predictions are not a simple task. In this study, Monte Carlo simulations of a trajectory predictor are performed to estimate the prediction uncertainty up to 20 minutes look-ahead time and to assess the correlation between inputs and prediction errors. Selected inputs are aircraft bank angle, constant calibrated airspeed (CAS) 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. Simulations are performed for heavy, medium and light wake turbulence category (WTC) aircraft. Results indicate that at 20 minutes look-ahead time, when outliers are not considered, along-track errors can reach up to 50 nautical miles for heavy and medium WTC and 100 nautical miles for light WTC aircraft. Cross-track errors are mostly within 3 nautical miles for heavy and medium WTC and 8 nautical miles for light WTC. Altitude errors can reach up to 25,000 feet. Wind conditions, vertical speed and CAS/Mach number speed settings are determined to be the most influential inputs.
机译:为了促进空中交通量的增长,当前和将来的空中交通管理决策支持工具需要有效且准确的航迹预测器。由于轨迹预测器的几乎所有输入都具有固有的不确定性,因此准确的预测并不是一项简单的任务。在这项研究中,进行了轨迹预测器的蒙特卡洛模拟,以估计高达20分钟的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(CAS)和马赫数速度设置,垂直速度,临时水平降落,空气温度,失速,风和空中交通管制意图。这些输入以从观测数据获得的分布函数的形式提供。对重型,中型和轻型尾流湍流类别(WTC)飞机进行了仿真。结果表明,在超前时间20分钟时,不考虑离群值时,重型和中型WTC飞机的沿航迹误差可达50海里,而轻型WTC飞机的航迹误差可达100海里。重型和中型WTC的跨航道误差大部分在3海里以内,而轻型WTC的跨航迹误差在8海里以内。高度误差可以达到25,000英尺。风况,垂直速度和CAS / Mach数速度设置被确定为最具影响力的输入。

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