期刊文献+

基于时空特征融合的飞机尾涡识别 被引量:2

Aircraft Wake Vortex Identification Based on Spatiotemporal Feature Fusion
下载PDF
导出
摘要 为了实现动态尾流缩减技术,减少进近阶段前机尾流对后机飞行安全的影响。依据相干激光雷达(coherent Doppler lidar,CDL)扫描风场循环周期性特点,提出一种基于时空特征融合的飞机尾涡识别模型。首先,CDL扫描生成的径向速度风场转换成序列输入和块输入。然后,双向长短时记忆(bidirectional long short-term memory,Bi-LSTM)网络用于提取序列输入的时间域特征,卷积神经网络(convolutional neural network,CNN)网络用于提取径向速度风场块输入的空间域特征。最后,将融合的时间域和空间域特征输入全连接层分类器,得到最终分类识别结果。实验团队在深圳宝安机场附近采集风场,并构建尾流数据集来验证所提得融合模型。结果表明:基于CNN和Bi-LSTM时空特征融合模型具有较好的分类性能,在尾涡识别上的准确率、召回率、F_(1)分数分别达到97.13%、97.50%、97.03%,且相比单一模型是一种更有效的识别方式,能够获得实时高效尾流预警。 In order to realize the dynamic wake reduction technology,the influence of the wake of the front aircraft on the flight safety of the rear aircraft during the approach phase is reduced.According to the periodic characteristics of coherent Doppler lidar(CDL)scanning wind field,an aircraft wake vortex identification model based on fusion of spatiotemporal features was proposed.First,the radial velocity wind field generated by the CDL scan was converted into sequence input and patch input.Then,a bidirectional long short-term memory(Bi-LSTM)network was used to extract the temporal features of the sequence input,and a convolutional neural network(CNN)network was used to extract the radial velocity wind field block input spatial characteristics.Finally,the fused temporal and spatial features were input into the fully connected layer classifier to obtain the final classification and recognition result.The experimental team collected wind fields near Shenzhen Bao an Airport,and constructed a wake data set to verify the proposed fusion model.The results show that the spatiotemporal feature mixture model based on CNN and Bi-LSTM has better classification performance,and it can be used in wake vortex recognition.The accuracy rate,recall rate,and F_(1) score reached 97.13%,97.50%,and 97.03%respectively,and compared with a single model,it is a more effective identification method and can obtain real-time and efficient wake early warning.
作者 潘卫军 冷元飞 吴天祎 PAN Wei-jun;LENG Yuan-fei;WU Tian-yi(China College of Air Traffic Management,Civil Aviation Flight University of China,Guanghan 618307,China)
出处 《科学技术与工程》 北大核心 2022年第31期14044-14049,共6页 Science Technology and Engineering
基金 国家自然科学基金(U1733203) 民航专业项目(TM2019-16-1/3) 四川省科技计划(2021YFS0319) 中央引导地方科技发展项目(2020ZYD094)。
关键词 尾涡识别 双向长短时记忆网络 卷积神经网络 目标识别 相干激光雷达 wake vortex identification Bi-LSTM CNN target identification coherent lidar
  • 相关文献

参考文献5

二级参考文献46

  • 1卜擎燕,熊宁宁,邹建东,蒋萌,刘芳,Anna Zhao-Wong.ICH国际医学用语词典(MedDRA):药事管理的标准医学术语集[J].中国临床药理学与治疗学,2007,12(5):586-590. 被引量:38
  • 2VICROY D D,VIJGEN P M,REIMER H M,et al.Recent NASA wake-vortex flight tests,flow-physics database and wake-development analysis[C] ∥AIAA.World Aviation Congress and Exposition.Anaheim:AIAA,1998:1-14.
  • 3LIOT D.Wake vortex encounter model implementation and validation in the online(piloted)flight simulation environ-ment[R].Toulouse:WAVENC Technical Note TN-19,AM Airbus,2000.
  • 4DE BRUIN A C,SPEIJKER L J P,MOET H,et al.S-wake:assessment of wake vortex safety[R].Amsterdam:National Aerospace Laboratory NLR,2003.
  • 5LUCKNER R,HHNE G,FUHRMANN M.Hazard crite-ria for wake vortex encounters during approach[J].Aero-space Science and Technology,2004,8(8):673-687.
  • 6BRANDON J M,JORDAN F L,STUEVER R A,et al.Application of wind tunnel free-flight technique for wake vor-tex encounters[R].Washington DC:NASA,1997.
  • 7PADFIELD G D,MANIMALA B,TURNER G P.A severity analysis for rotorcraft encounters with vortex wakes[J].Journal of the American Helicopter Society,2004,49(4):445-456.
  • 8LAWRENCE B,PADFIELD G D.Wake vortex encounter severity for rotorcraft in approach and landing[R].Florence:31st European Rotorcraft Forum,2005.
  • 9POIREL D,PRICE S J.Bifurcation characteristics of a two-dimensional structurally non-linear airfoil in turbulent flow[J].Nonlinear Dynamics,2007,48(4):423-435.
  • 10BROWN A.The impact upon aircraft airworthiness design from encounters with discrete vortices[C] ∥AIAA.44th AIAA Aerospace Sciences Meeting and Exhibit.Reno:AIAA,2006:1-19.

共引文献79

同被引文献24

引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部