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Improvement of Trajectory Synthesizer for Efficient Descent Advisor

机译:高效下降顾问的轨迹合成器的改进

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The Efficient Descent Advisor (EDA) is being developed to provide a decision support tool for controllers to help them issue continuous descent trajectories for arrival traffic. This paper investigates methods for improving the accuracy of the trajectory synthesizer, which is the trajectory engine that supports EDA. The study was motivated by the need to harmonize the trajectories generated by the trajectory synthesizer with those generated by on board Flight Management Systems (FMS's), which are used by pilots to execute continuous descents. An analysis of error sources between predicted and actual continuous descent trajectories shows that thrust and descent speed profiles are the most important parameters affecting the accurate prediction of top of descent location and arrival fix cross ing times. While the thrust correction applies to all descents, the descent speed applies to uncontrolled (non-metered) descents. In order to establish the best value for thrust correction for use in the trajectory synthesizer, a limited set of continuous descent trajec tories flown by aircraft during regular revenue flights into the Dallas-Fort Worth Airport were recorded and analyzed. In addition to recorded trajectories, controllers also obtained FMS-calculated top-of-descent ranges, crossing times and speed profiles from pilots when ever possible. In post flight analysis the predicted trajectories generated by the Trajectory Synthesizer were compared to the flight test data. It was generally found that the actual (FMS guided) trajectories were flown at shallower descent angles than the predicted tra jectories and that actual descent speeds often differed significantly from those programmed into the trajectory synthesizer. A descent thrust correction parameter, normalized to air craft weight and dependent on aircraft type and airline/operator is introduced to improve trajectory prediction accuracy. It is shown that this parameter, together with updated speeds obtained from pilots prior to descent, increase the accuracy of trajectory prediction significantly.
机译:正在开发高效下降顾问(EDA),以为管制员提供决策支持工具,以帮助他们为到达交通量发出连续的下降轨迹。本文研究了提高轨迹合成器准确性的方法,该合成器是支持EDA的轨迹引擎。这项研究的动机是需要将轨迹合成器生成的轨迹与机载飞行管理系统(FMS)生成的轨迹进行协调,供飞行员用来执行连续下降。对预测的和实际的连续下降轨迹之间的误差源的分析表明,推力和下降速度曲线是影响精确预测下降位置顶部和到达定点穿越时间的最重要参数。虽然推力校正适用于所有下降,但下降速度适用于不受控制的(非计量)下降。为了确定在轨迹合成器中使用的推力校正的最佳值,记录并分析了飞机在定期飞往达拉斯-沃思堡机场的飞行过程中飞行的一组有限的连续下降轨迹。除了记录的轨迹外,管制员还尽可能从飞行员那里获得FMS计算的下降顶部范围,穿越时间和速度曲线。在飞行后分析中,将轨迹合成器生成的预测轨迹与飞行测试数据进行了比较。通常发现,实际(FMS引导)轨迹的下降角度要比预测轨迹的下降角度浅,并且实际下降速度通常与编程到轨迹合成器中的速度明显不同。引入了下降推力校正参数,将其标准化为飞机重量并取决于飞机类型和航空公司/运营人,以提高轨迹预测的准确性。结果表明,该参数与下降之前从飞行员获得的更新速度一起,显着提高了轨迹预测的准确性。

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