仪表着陆系统下滑信标运行保护区仿真研究

doi:10.16182/j.issn1004731x.joss.23-0133

系统仿真学报 ›› 2024, Vol. 36 ›› Issue (6): 1273-1284.doi: 10.16182/j.issn1004731x.joss.23-0133

仪表着陆系统下滑信标运行保护区仿真研究

李清栋¹^,²(), 叶家全¹^,²(), 许健¹^,²

^1.中国民用航空总局第二研究所民航空管工程技术研究所, 四川成都 610041
^2.民航科技创新示范区导航技术研究实验室, 四川成都 641400

收稿日期:2023-02-14 修回日期:2023-05-05 出版日期:2024-06-28 发布日期:2024-06-19
通讯作者: 叶家全 E-mail:liqingdong@caacsri.com;yejq@caacsri.com
第一作者简介:李清栋(1986-)，男，副研究员，硕士，研究方向为民航导航技术、航空无线电技术等。E-mail：liqingdong@caacsri.com
基金资助:
国家重点研发计划(2017YFB0503402);中国民用航空局安全能力项目(AADSA201S013S)

Research on Operational Protection Area of ILS Glide Slope

Li Qingdong¹^,²(), Ye Jiaquan¹^,²(), Xu Jian¹^,²

^1.Civil Aviation Management Engineering Technology Research Institute, The Second Research Institute of CAAC, Chengdu 610041, China
^2.Navigation Technology Research Laboratory, Civil Aviation Science and Technology Innovation Demonstration Zone, Chengdu 641400, China

Received:2023-02-14 Revised:2023-05-05 Online:2024-06-28 Published:2024-06-19
Contact: Ye Jiaquan E-mail:liqingdong@caacsri.com;yejq@caacsri.com

摘要/Abstract

摘要：

仪表着陆系统下滑信标运行保护区的科学防护，对于确保民用航空导航空间信号质量、保障航空器进近阶段运行安全、提升机场运行效率均具有重要意义。结合下滑信标运行保护区概念的演进，对民用航空国家标准、行业标准，以及国际民用航空公约附件十第I卷要求的下滑信标运行保护区的划设情况进行了对比分析。以特大型航空器A380-800为例，对特定运行类别的下滑信标运行保护区进行了研究，以期作为国际民用航空公约附件十第I卷关于下滑信标保护区相关数据的补充和实际工程论证的示例。给出了针对特定机场实际运行进行下滑信标场地保护的典型研究方法以及下滑信标运行保护区的保护建议，为机场的建设和运行提供参考。

关键词: 仪表着陆系统, 下滑信标, 场地保护区, 运行保护区, 临界区, 敏感区

Abstract:

The scientific protection for the operational protection area of the instrument landing system glide slope is of great significance to ensure the quality of civil aviation navigation space signals, the safety of aircraft approach operations, and the efficiency of airport operations. Combined with the concept evolution of the glide slope operational protection area, a comparative analysis of the delineation of the glide slope operational protection area required by the national civil aviation standards, industry standards, and Annex 10 Volume I of the Convention on International Civil Aviation is carried out. Taking the extra-large aircraft (A380-800) as an example, the glide slope operational protection area of a specific operation category is studied in the form of computer simulation, which maybe a supplement to relevant data on glide slope protection areas in Annex 10 Volume I of the Convention on International Civil Aviation and an example of the actual engineering demonstration. The typical research methods of glide slope site protection for the actual operation of specific airports and protection suggestions for glide slope operational protection area are given as the references for airport construction and operation.

Key words: instrument landing system, glide slope, site protection area, operational protection area, critical area, sensitive area

中图分类号:

TP391.9

李清栋,叶家全,许健 . 仪表着陆系统下滑信标运行保护区仿真研究[J]. 系统仿真学报, 2024, 36(6): 1273-1284.

Li Qingdong,Ye Jiaquan,Xu Jian . Research on Operational Protection Area of ILS Glide Slope[J]. Journal of System Simulation, 2024, 36(6): 1273-1284.

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参考文献 19

1	中国民用航空局: 民用航空通信导航监视台(站)设置场地规范第1部分: 导航: [S]. 北京: 中国民用航空局, 2021: 1-32.
	Civil Aviation Administration of China. Specification for Aeronautical Communication Navigation and Surveillance Station Siting Criteria-part 1: Navigation: [S]. Beijing: Civil Aviation Administration of China, 2021: 1-32.
2	Federal Aviation Administration. Siting Criteria for Instrument Landing Systems: 6750.16E [S]. Washington: Federal Aviation Administration, 2014.
3	赵修斌, 王永生, 姜恒乐. 基于GTD的进近着陆系统多径效应仿真[J]. 系统仿真学报, 2005, 17(8): 1864-1866.
	Zhao Xiubin, Wang Yongsheng, Jiang Hengle. Simulation for Multipath Effect of Approach Landing System Based on GTD[J]. Journal of System Simulation, 2005, 17(8): 1864-1866.
4	Luebbers R, Ungvichian V, Mitchell L. GTD Terrain Reflection Model Applied to ILS Glide Scope[J]. IEEE Transactions on Aerospace and Electronic Systems, 1982, 18(1): 11-20.
5	Weinmann Frank. PO/PTD Ray Tracing for Arbitrary Metallic and Dielectric Objects[C]//2006 First European Conference on Antennas and Propagation. Piscataway, NJ, USA: IEEE, 2006: 1-5.
6	倪育德, 于颖丽, 刘瑞华. 保护区内地形对ILS下滑信标辐射场的影响[J]. 信号处理, 2022, 38(9): 1892-1902.
	Ni Yude, Yu Yingli, Liu Ruihua. Influence of Terrain in Protected Area on Radiation Field of Glide Slope of ILS[J]. Journal of Signal Processing, 2022, 38(9): 1892-1902.
7	姜春英, 康玉祥, 由晓峰, 等. 仪表着陆系统下滑宽度仿真系统研究[J]. 系统仿真学报, 2020, 32(2): 262-268.
	Jiang Chunying, Kang Yuxiang, You Xiaofeng, et al. Research on Glide Width Simulation System of Instrument Landing System[J]. Journal of System Simulation, 2020, 32(2): 262-268.
8	戴传金, 赵修斌, 李颖路. ILS系统复杂场地的数值计算仿真与飞行检验[J]. 航空计算技术, 2006, 36(2): 36-39.
	Dai Chuanjin, Zhao Xiubin, Li Yinglu. Numerical Analysis Simulation and Flight Check on the Difficult Site for ILS[J]. Aeronautical Computing Technique, 2006, 36(2): 36-39.
9	Xu Jian, Ye Jiaquan, Liang Fei, et al. Simulation Analysis and Research on the Influence of Buildings on a Glide Path Antenna[C]//2021 International Conference on Computer Technology and Media Convergence Design (CTMCD). Piscataway, NJ, USA: IEEE, 2021: 63-66.
10	Godfrey J, Hartley H, Moussally G, et al. Terrain Modeling Using the Half-plane Geometry with Applications to ILS Glide Slope Antennas[J]. IEEE Transactions on Antennas and Propagation, 1976, 24(3): 370-378.
11	Ramakrishna S, Sachidananda M. Calculating the Effect of Uneven Terrain on Glide Path Signals[J]. IEEE Transactions on Aerospace and Electronic Systems, 1974, 10(3): 380-384.
12	Iungaitis E M, Voytovich N L, Ershov V A. Influence of Wave Diffraction on the Coastal Airfield Surface on the Glide Path Behavior[C]//2022 16th European Conference on Antennas and Propagation (EuCAP). Piscataway, NJ, USA: IEEE, 2022: 1-5.
13	Yungaitis Ekaterina, Zhdanov Boris, Zotov Andrei, et al. Application of Signals Reflected from an Aircraft for Monitoring an ILS Glide Path Position[C]//2020 7th All-Russian Microwave Conference (RMC). Piscataway, NJ, USA: IEEE, 2020: 291-293.
14	Poljak Dragan, Dorić Vicko, Šušnjara Anna, et al. Deterministic-stochastic Modeling of a Glide Path Antenna System Above a Multilayer[C]//2020 International Symposium on Electromagnetic Compatibility-EMC EUROPE. Piscataway, NJ, USA: IEEE, 2020: 1-5.
15	ICAO. Annex 10 to the Convention on International Civil Aviation, Volume I Aeronautical Telecommunications, Radio Navigation Aids: International Civil Aviation Organization[EB/OL].[2023-01-24]. .
16	李清栋, 李锦耀, 林欢, 等. 基于PO-PTD的航空器对下滑道结构影响的动态研究[J]. 南京航空航天大学学报, 2018, 50(6): 829-833.
	Li Qingdong, Li Jinyao, Lin Huan, et al. Dynamic Research on Glide-slope Approach Based on PO-PTD[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2018, 50(6): 829-833.
17	Knott E F. 雷达散射截面-预估、测量和减缩[M]. 阮颖铮, 陈海译. 北京: 电子工业出版社, 1988: 99-124.
18	蒋相闻, 招启军, 徐国华. 基于面元边缘法的直升机RCS计算与分析[J]. 南京航空航天大学学报, 2011, 43(3): 429-434.
	Jiang Xiangwen, Zhao Qijun, Xu Guohua. Calculation and Analysis of RCS of Helicopter Based on Panel Edge Method[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2011, 43(3): 429-434.
19	Youssef N N. Radar Cross Section of Complex Targets[J]. Proceedings of the IEEE, 1989, 77(5): 722-734.

变量	长度
D	下滑信标天线至跑道着陆端的距离
U/m	60
V	下滑信标天线至跑道中心线的距离
W/m	30
X/m	120
Y	360 m或距离D(以大者为准)
L	900 m或至机场边界或至平滑地面的终止点(以小者为准)

典型参数	参数设置
地形特征	平坦
下滑角/(°)	3
静态多径容差/%	60
动态多径容差/%	80
进近航空器速度/kt	105
基准数据点高(RDH)/m	16.5

分类	物体高度H
地面车辆	H≤6
中型航空器	6<H≤14
大型航空器	14<H≤20
特大型航空器	20<H≤25

仿真参数	参数设置
跑道长度/m	3 800
跑道宽度/m	60
下滑信标后撤距离/m	310
下滑信标横向偏置/m	120
天线类型	捕获效应(M型)
馈电系统	NM7000B
运行类别	CAT Ⅱ/Ⅲ
仿真频率/MHz	330.65
机载接收机类型	典型
仿真算法	物理光学
单次仿真尺度	3 526

色块颜色	对进近航空器的影响(ICAO容限)
绿	<25
浅绿	[25~50)
黄	[50~75)
橘红	75~100
红/深红	大于/远大于100

仪表着陆系统下滑信标运行保护区仿真研究

Research on Operational Protection Area of ILS Glide Slope

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参数		数值
航空器高度		20<H≤25
临界区	X_C	672
临界区	Y_C	34
敏感区	X_s	610
敏感区	Y_s	24