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云雾中飞机尾流的环量估计 被引量:3

Circulation Estimation of Wake Vortex in Cloudy and Mist Conditions
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摘要 结合典型的稳定段尾流空气动力学模型和电磁散射模型,仿真分析了尾流的毫米波雷达多普勒特性;进而利用网格映射的方法,提出了一种基于双部毫米波雷达探测的尾流速度场反演和环量估计技术。结果表明,双部多普勒雷达可有效估计垂直于航向截面上的尾流二维速度场特征,据此可以得到航空安全领域非常关注的尾流环量特征。 The millimeter radar doppler characteristics of the wake vortex is simulated and analyzed on the combination of typical wake vortex aerodynamics model and electromagnetic scattering model. And then, using a grid mapping method. A technology is proposed to estimate the velocity and circulation of wake vortex based on two millimeter radars. Results show that the 2D velocity ( on the cross section) of wake vortex, as well as its circulation for aviation security, can be well estimated from the Doppler spectrums of two radars.
出处 《现代雷达》 CSCD 北大核心 2015年第6期10-15,共6页 Modern Radar
关键词 飞机尾流 云雾 雷达 多普勒 环量估计 wake vortex cloud and mist radar Doppler circulation estimation
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参考文献19

  • 1Liu C. Wake vortex encounter analysis with different wakevortex models using vortex-lattice method[ D]. Netherlands :Delft University of Technology, 2007.
  • 2Veillette P R. Data show that U. S. wake-turbulence accidentsare most frequent at low altitude and during approach and land-ing[J]. Flight Safety Digest, 2002, 21 (3-4) : 1-47.
  • 3Garnet M, Altman A. Identification of any aircraft by its u-nique turbulent wake signature [ J ]. Journal of Aircraft,2009, 46(1) : 263-268.
  • 4徐肖豪,赵鸿盛,王振宇.尾流间隔缩减技术综述[J].航空学报,2010,31(4):655-662. 被引量:31
  • 5International Civil Aviation Organization. Rules of the air[S]. 10th ed. Montreal : International Civil Aviation Or-ganization ,2004.
  • 6吕建飞.航空公司飞行机组排班问题研究[J].西安航空学院学报,2015,33(1):33-37. 被引量:4
  • 7Lunsford C,Johnson E. Crosswind-based wake avoidancesystem approved by the FAA for operational use [ C ]//Wake Net-Europe Workshop. Paris, France: STAC, 2013.
  • 8Barbaresco F. European FP7 UFO project “ ultra-fast-windsensors” forwake-votex hazardshazards mitigation [ C ]//Wake Net-EuropeWorkshop. Paris, France: STAC, 2013.
  • 9Frehlich R, Sharman R. Maximum likelihood estimates ofvortex parameters from simulated coherent Doppler lidar da-ta [ J ]. Journal of Atmospheric and Oceanic Technology,2005(22) ; 117-130.
  • 10Hannon S M, Thomson J A. Aircraft wake vortex detectionand measurement with pulsed solid-state coherent laser ra-dar[ J]. Journal of Modem Optics, 1994(41 ) : 21-75.

二级参考文献37

  • 1Annex 2. Rules of the air[S]. Montreal: International Civil Aviation Organization, 2004.
  • 2Frech M. VORTEX-TDM -a parameterized wake vortex transport model and its meteorological input data base [R]. DFS, 2001.
  • 3Spitzer E A, Rudis R P, Hallock J N, et al. Windline for parallel runway operations at San Francisco airport[C]// XXV Assembly of the European Geophysical Society. Nice, France: European Geophysical Society, 2000.
  • 4Gurke T, Lafferton H. The development of the wake vortex warning system for Frankfurt airport: theory and implementation[J]. Air Traffic Control Quarterly, 1997, 5 (1) : 3 -29.
  • 5Ahlbrecht M, Gurke T. The progressive algorithm of the wake vortex warning system[R]. IABG Report 1029/01, 1994.
  • 6Roux L C, Corjon A. Wake vortex advisory system implementation at Orly airport for departing aircraft [J]. Air Traffic Control Quarterly, 1997, 5 (1): 31-48.
  • 7Corjon A, Poinsot T. Vortex model to define safe aircraft separations distances[J]. Journal of Aircraft, 1996, 33 (3) : 547-553.
  • 8Corjon A, Zheng Z C. Model of the behavior of aircraft wake vortices experiencing crosswind near the ground[R]. AIAA-1996-2516, 1996.
  • 9Lissman P S, Crow S C. Aircraft wake vortex descent and decay under real atmospheric effects[R]. FAA-RD-73-120 DOT, 1973.
  • 10Burnham D C, Hallock J N. Ground based measurements of the wake vortex characteristics of a B -747 aircraft in various conflgurations[R]. FAA- RD-78-146, 1978.

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