CDO Sensitivity Analysis for Robust Trajectory Planning under Uncertain Weather Prediction

Shumpei Kamo, J. Rosenow, H. Fricke
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引用次数: 4

Abstract

When planning and predicting a flight trajectory, uncertainties are inherent both in the current values of various influencing factors and in their evolution. These uncertainties can turn initially “optimized” trajectories into impossible or at least less attractive solutions later when it is executed. In order to support a more robust trajectory planning for Continuous Descent Operations (CDO), this paper investigates how variations of those influencing factors impact the trajectory optimization fidelity. For this purpose, a set of optimal trajectories are generated for each of the variations and their sensitivities are analyzed. The trajectory optimization is formalized as a multi-phase optimal control problem and is numerically solved with the Legendre-Gauss Pseudospectral Method (LGPM). An iterative process is proposed to determine the required number of collocation points to grant a pre-set level of convergence. Case studies are carried out for International Standard Atmosphere (ISA) baseline conditions as well as for wind and temperature variations as relevant representatives of the weather prediction uncertainties. The numerical simulation results show shifts from the reference trajectory depending on wind and temperature variation. Uncertain wind speed caused a larger solution space and more variation in fuel burn than temperature errors. The designed solution spaces, especially the earliest and latest ToD locations, give pilots and air traffic controllers a good reference where their aircraft is expected to match best CDO goals under the individually prevailing uncertainties. We believe that such additional flight envelope information should complement current vertical path displays in glass cockpits to foster robust flight planning and execution.
不确定天气下鲁棒轨迹规划的CDO灵敏度分析
在规划和预测飞行轨迹时,各种影响因素的当前值及其演变都具有固有的不确定性。这些不确定性可能会使最初的“优化”轨迹在执行后变得不可能或至少不那么吸引人。为了支持连续下降操作(CDO)更稳健的轨迹规划,本文研究了这些影响因素的变化对轨迹优化保真度的影响。为此,为每个变量生成了一组最优轨迹,并分析了它们的灵敏度。将弹道优化问题形式化为多相最优控制问题,采用legende - gauss伪谱法(LGPM)对其进行数值求解。提出了一个迭代过程来确定所需的并置点数量,以保证预先设定的收敛水平。个案研究是针对国际标准大气(ISA)的基线条件,以及风和温度的变化,作为天气预报不确定性的相关代表。数值模拟结果表明,参考轨迹随风和温度的变化而变化。与温度误差相比,不确定的风速导致更大的解空间和更大的燃料燃烧变化。设计的解决方案空间,特别是最早和最新的ToD位置,为飞行员和空中交通管制员提供了一个很好的参考,在单个普遍存在的不确定性下,他们的飞机期望达到最佳CDO目标。我们认为,这种额外的飞行包线信息应该补充目前在玻璃驾驶舱的垂直路径显示,以促进强大的飞行计划和执行。
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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