Mevlut Uzun, M. Demirezen, E. Koyuncu, G. Inalhan, Javier Lopez, M. Vilaplana
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State-of-the-art deep learning algorithms are deployed to map baseline estimations for fuel flow and wind to their ground truths. Proper input parameters to have the best estimation results and be compatible with the ground-based flight planning systems are derived through extensive feature engineering. Comparison of the aircraft performance models with real flight data shows that precise estimation of fuel flow with mean absolute errors on a range of %0.1 - %0.7 can be achieved across all the flight modes. Results also show that we can achieve considerable reduction in wind uncertainty both from a mean error and variance sense. For short haul flights, the standard deviations of forecast errors in u and v components are reduced from 6.25 and 8.38 knots to 1.37 and 1.81 knots, respectively. 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引用次数: 1
摘要
本文应用机器学习技术来提高飞行效率。具体来说,我们关注两个不同的问题:飞机性能模型的不确定性和风的不确定性。在这个意义上,本文提出了通过运行数据来改进燃料流量和风估计的基线模型的方法。我们利用baseofaircraft Data (BADA) 4作为飞机性能模型的基准。历史全球预报系统(GFS)的预测被用作风的$u$和$v$分量的基线估计。至于运行数据,使用了窄体和宽体飞机的快速存取记录仪(QAR)轨迹足迹,包括实际记录的发动机燃油流量和测量的风速和风向。采用最先进的深度学习算法,将燃料流量和风的基线估计映射到实际情况。通过大量的特征工程,得到了具有最佳估计结果并与地面飞行规划系统兼容的适当输入参数。飞机性能模型与实际飞行数据的比较表明,在所有飞行模式下都可以精确估计燃油流量,平均绝对误差在%0.1 ~ %0.7之间。结果还表明,我们可以从平均误差和方差意义上大大减少风的不确定性。对于短途航班,u和v分量的预测误差标准差分别从6.25和8.38节减少到1.37和1.81节。长途航班的航速也从11.02和10.89节降至4.88和4.76节。
Deep Learning Techniques for Improving Estimations of Key Parameters for Efficient Flight Planning
This paper applies machine learning techniques to improve flight efficiency. Specifically, we focus on two distinct problems: uncertainties in aircraft performance models and uncertainties in wind. In this sense, this paper proposed methodologies to improve baseline models for fuel flow and wind estimations are via operational data. We utilize Base of Aircraft Data (BADA) 4 as baseline for aircraft performance model. Historical Global Forecast System (GFS) predictions are utilized as baseline estimations for $u$ and $v$ components of wind. As for the operational data, Quick Access Recorder (QAR) trajectory footprints of a narrow body and a wide body aircraft, which include actual recorded fuel flow from engines and measured wind speed and direction, are used. State-of-the-art deep learning algorithms are deployed to map baseline estimations for fuel flow and wind to their ground truths. Proper input parameters to have the best estimation results and be compatible with the ground-based flight planning systems are derived through extensive feature engineering. Comparison of the aircraft performance models with real flight data shows that precise estimation of fuel flow with mean absolute errors on a range of %0.1 - %0.7 can be achieved across all the flight modes. Results also show that we can achieve considerable reduction in wind uncertainty both from a mean error and variance sense. For short haul flights, the standard deviations of forecast errors in u and v components are reduced from 6.25 and 8.38 knots to 1.37 and 1.81 knots, respectively. The same reduction is from 11.02 and 10.89 knots to 4.88 and 4.76 knots in the long haul flights.