Advanced Search
Volume 38 Issue 10
Oct.  2012
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  38(10): 1369-1374.
Duan Ying, Shen Gong, Zhang Yonggang, et al. Aerodynamic testing simulation facility for high-speed elevator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(05): 444-447. (in Chinese)
Citation: Wang Lei, Su Donglin, Xie Shuguo, et al. Modeling of electromagnetic environment and radiation distribution analysis for aircraft approaching and landing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(10): 1369-1374. (in Chinese)
shu

Modeling of electromagnetic environment and radiation distribution analysis for aircraft approaching and landing

  • School of Electronics and Information Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 14 Oct 2011
  • Publish Date: 30 Oct 2012
    Abstract
  • Electromagnetic field, terrain and obstacle are three vital elements which constitute electromagnetic environment in aerodrome terminal. Because of their inhomogeneity in topology, physics and semanteme, it is difficult to express the characteristic of the electromagnetic environment for aircraft approaching and landing with determined model. Based on the attribute of hierarchy and the coupling interrelation of those three elements, a multi-layer fused electromagnetic environment model frame for aerodrome terminal was put forward. In order to reduce the computation error induced by the non-regulation boundary variation of electromagnetic field, a combination of method of moment(MoM) and ray tracing methods was used to simulate the radiation pattern and wave propagation, and radiation intensity expression and distribution computation flow in approaching and landing area were described. Simulation experiment of the radiation computation in approaching area based on one aerodrome dataset shows the validity of the modeling method.

     

    • FullText(HTML)
    • References(10)
  • [1]
    ICAO.Manual on testing of radio navigation .ICAO Doc 8071,2002
    [2]
    ICAO.Radio navigation aids .ICAO Annex 10,2006
    [3]
    ICAO.Guidelines for electronic terrain,obstacle and aerodrome mapping information .ICAO Doc 9881,2009
    [4]
    黄金明.飞行模拟器近程无线电导航系统建模与仿真[J].计算机仿真,2007,24(2):282-285 Huang Jinming.Modeling and simulation of short-range radio navigation system in flight simulator[J].Computer Simulation,2007,24(2):282-285(in Chinese)
    [5]
    Sandra V Koppen.Airborne RF measurement system (ARMS) and analysis of representative flight RF environment .NASA/TP-2007-214883,2007
    [6]
    Greving G,Biermann W D,Mundt R.Status of advanced scattering distortion system analysis for navaids and radar-examples of A380 and wind turbines // Felix Yanovsky,Proceedings of Microwaves,Radar and Remote Sensing 2008 Symposium.Kyiv,Ukraine:National Aviation University,2008:42-47
    [7]
    Greving G.Hybrid numerical scattering field analysis embedded into simulations of complex radio based systems-examples,capabilities and limitations // Greving G.Proceedings of the 11th International Conference on Electromagnetics in Advanced Applications.New York:IEEE,2009:493-496
    [8]
    刘兴堂,梁炳成.复杂系统建模理论、方法与技术[M].北京:科学出版社,2010:43-51 Liu Xingtang,Liang Bingcheng.The theory,method & technique for complex system modeling[M].Beijing:Science Press,2010:43-51(in Chinese)
    [9]
    Holm P.UTD-diffraction coefficients for higher order wedge diffracted fields[J].IEEE Trans Antennas Propagation,1996:44(6):879-888
    [10]
    Arnaud Dedryvere.A general model for VHF aeronautical multipath propagation channel .ICAO AMCP/WG-D//WP6,1999
    • Relative Articles

  • Relative Articles

    [1]ZHU R N，WANG B，TANG C Y. Improvement of terrain following flight adaptive angle method under small field of view conditions[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：676-682 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0057.
    [2]CAO T T，YANG Y X，YU L F，et al. Whirl flutter on distributed electric propeller aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2627-2635 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0684.
    [3]CAI Jing, NIU Yu-fa, WANG Yan, LI Yue, DAI Xuan. A Simulation analysis of human-machine closed-loop dynamics of aircraft landing and running attitude under cross-rheumatic slip conditions[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0599
    [4]LIU Y J，HAN W，SU X C，et al. Carrier aircraft landing scheduling problem based on improved gray wolf optimization[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（3）：803-813 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0280.
    [5]FENG X R，GAO Z D，WANG J，et al. Research on aircraft landing scheduling problem based on compact subsequence[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2421-2431 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0656.
    [6]ZHAO Hong-jia, ZHANG Duo-na, LU Yuan-yao, DING Wen-rui. Intelligent Recognition of Electromagnetic Signal Modulation with Embedded Domain Knowledge[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0746
    [7]LIN Jiazhe, HE Lei, CHENG Ming, ZHOU Ling, YANG Chunming. Rapid prediction of surface pressure distribution of tactical missile based on point cloud segmentation algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0172
    [8]CHEN N T，MAN Y Z，LI J H. Risk assessment method for civil aircraft approach and landing at high plateau based on QAR data[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：77-85 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0186.
    [9]NI Yu-de, LI Xin-xin, LIU Rui-hua, GUO Jian-li, WANG Yan-yang. Delineation of the Instrument Landing System Localizer Protection Area[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0592
    [10]WANG Xiangzhang, WANG He, XU Bohao. Hard landing risk prediction of civil aircraft based on GBDT-GS method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0443
    [11]CHENG B P，FANG Y W，PENG W S，et al. Comprehensive performance evaluation of swarm intelligence algorithms based on improved radar graph method[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2780-2789 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0726.
    [12]ZHANG Y H，LYU N，MIAO J C，et al. Improved intelligent detection algorithm for SPMA protocol channel state based on recurrent neural network[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：735-744 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0309.
    [13]MA M，YU J，FAN W R. CFRP material detection based on improved joint sparse EIT algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：265-272 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0244.
    [14]YAN Y F，GAN X S，WU Y R，et al. Aircraft landing safety quality analysis based on modified FRAM method[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1964-1973 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0574.
    [15]LI B，WANG C，DING X Y，et al. Surface defect detection algorithm based on improved YOLOv4[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：710-717 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0301.
    [16]SHI X S，LIN Z Y. Fixed-time distributed convex algorithm over second-order multi-agent systems under bounded disturbances[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：2951-2959 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0060.
    [17]TAN Chuan-rui, LI Tang, CHEN Wen-qian, WANG Feng, YANG Dong-kai, WU Shi-yu. Evaluation of TDOA Based Air Target Localization Algorithm Using GNSS-Based Passive Radar[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0685
    [18]CHENG Z Y，YANG Y X，ZHANG X C，et al. Rapid evaluation method for aerodynamic characteristics of distributed electric propulsion aircraft concept scheme[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3047-3058 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0771.
    [19]XU Lijun, LIU Fulu, DING Yiqing, LI Zhengyong, XIE Yuedong. Residual thickness detection of pipeline based on electromagnetic ultrasonic shear wave[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1767-1773. doi: 10.13700/j.bh.1001-5965.2022.0301
    [20]SU Donglin, CUI Shuo, BAI Jiangfei, LI Yaoyao. Fast prediction method for radiated and scattered coupled fields in complex electromagnetic environment[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1553-1560. doi: 10.13700/j.bh.1001-5965.2022.0705
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(1880) PDF downloads(657) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return