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Analysis of Air Traffic Control Command Entries and the Impact on Decision Support Tool Performance

机译:空中交通管制命令条目分析及其对决策支持工具性能的影响

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摘要

In the en route environment, air traffic control is responsible for maintaining separation between aircraft with the assistance of many decision support tools (DSTs), such as Conflict Probe and Trajectory Predictor. Conflict Probe predicts potential airspace conflicts and notifies the controller of the impending separation violation, while Trajectory Predictor predicts more accurate aircraft position. In the Next Generation Air Transportation System (NextGen) environment, it is envisioned that Conflict Probe performance will be improved by adding more accurate aircraft and pilot intent data, better air traffic surveillance, and 4D trajectory-based operations. This paper investigates the effect and sensitivity of a proposed NextGen improvement on the Conflict Probe. A quantitative study is designed to examine integration of the text in the 4th line of the flight data block, which currently serves as an optional note field for air traffic controllers, into the en route DST to create new trajectories. The new, more accurate trajectories are compared against the original baseline trajectories to determine aircraft position accuracy improvements from the Trajectory Predictor, and false alert reductions from the Conflict Probe. The study findings quantitatively demonstrate that heading amendments increase trajectory accuracy by reducing horizontal error as much as 6.21nm, cross track error by 3.65nm, and along track error by 3.64nm on the first day. Speed amendments, noted in 4th line of the flight data block, decrease by 10.3% the overall number of false alerts generated by the Conflict Probe.
机译:在途中环境中,空中交通管制负责在许多决策支持工具(DST)(例如冲突探测和轨迹预测器)的协助下保持飞机之间的间隔。冲突探测器可预测潜在的空域冲突并通知即将发生的分离违规,而轨迹预测器可预测更准确的飞机位置。可以预见,在下一代航空运输系统(NextGen)环境中,将通过添加更准确的飞机和飞行员意图数据,更好的空中交通监视以及基于4D轨迹的操作来提高冲突探测器的性能。本文研究了提议的NextGen改进对冲突探针的影响和敏感性。定量研究旨在检查飞行数据块第4行中的文本(当前用作空中交通管制员的可选注释字段)是否与途中DST集成以创建新轨迹。将新的,更准确的轨迹与原始基线轨迹进行比较,以确定通过“轨迹预测器”提高飞机位置的精度,并通过“冲突探测器”减少误报。研究结果定量地表明,航向修正在第一天通过减少水平误差达6.21nm,交叉轨道误差达3.65nm和沿轨道误差达3.64nm来提高了轨迹精度。飞行数据块第4行中指出的速度修正,使冲突探测器生成的虚假警报总数减少了10.3%。

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