中国航空学报(英文版)2024,Vol.37Issue(9) :347-368.DOI:10.1016/j.cja.2024.05.011

DBN-GABP model for estimation of aircraft wake vortex parameters using Lidar data

Zhiqiang WEI Tong LU Runping GU Fei LIU
中国航空学报(英文版)2024,Vol.37Issue(9) :347-368.DOI:10.1016/j.cja.2024.05.011

DBN-GABP model for estimation of aircraft wake vortex parameters using Lidar data

Zhiqiang WEI 1Tong LU 1Runping GU 1Fei LIU1
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作者信息

  • 1. College of Air Traffic Management,Civil Aviation University of China,Tianjin 300300,China
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Abstract

Aircraft wake turbulence is an inherent outcome of aircraft flight,presenting a substan-tial challenge to air traffic control,aviation safety and operational efficiency.Building upon data obtained from coherent Doppler Lidar detection,and combining Dynamic Bayesian Networks(DBN)with Genetic Algorithm-optimized Backpropagation Neural Networks(GA-BPNN),this paper proposes a model for the inversion of wake vortex parameters.During the wake vortex flow field simulation analysis,the wind and turbulent environment were initially superimposed onto the simulated wake velocity field.Subsequently,Lidar-detected echoes of the velocity field are simulated to obtain a data set similar to the actual situation for model training.In the case study validation,real measured data underwent preprocessing and were then input into the established model.This allowed us to construct the wake vortex characteristic parameter inversion model.The final results demonstrated that our model achieved parameter inversion with only minor errors.In a practical example,our model in this paper significantly reduced the mean square error of the inverted velocity field when compared to the traditional algorithm.This study holds significant promise for real-time monitoring of wake vortices at airports,and is proved a crucial step in developing wake vortex interval standards.

Key words

Air traffic control/Wake vortex flow field sim-ulation/Lidar echo simulation/DBN model/GA-BP model/Wake vortex characteristic parameter inversion model

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基金项目

National Natural Science Foundation of China(U2133210)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDCSCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量3
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