[1]钟伦珑,张卓轩,樊振东.面向精密进近运行需求的GLS接收机性能评估[J].南京师大学报(自然科学版),2020,43(04):86-94.[doi:10.3969/j.issn.1001-4616.2020.04.013]
　Zhong Lunlong,Zhang Zhuoxuan,Fan Zhendong.Performance uation of GLS Receiver Under Requirementsfor Precision Approach Operation[J].Journal of Nanjing Normal University(Natural Science Edition),2020,43(04):86-94.[doi:10.3969/j.issn.1001-4616.2020.04.013]
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面向精密进近运行需求的GLS接收机性能评估()
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《南京师大学报（自然科学版）》[ISSN:1001-4616/CN:32-1239/N]

卷:
第43卷
期数:
2020年04期
页码:
86-94
栏目:
·智慧应急信息技术·
出版日期:
2020-12-30

文章信息/Info

Title:
Performance uation of GLS Receiver Under Requirementsfor Precision Approach Operation
文章编号:
1001-4616(2020)04-0086-09
作者:
钟伦珑; 张卓轩; 樊振东
中国民航大学,智能信号与图像处理天津市重点实验室,天津 300300
Author(s):
Zhong Lunlong; Zhang Zhuoxuan; Fan Zhendong
Tianjin Key Laboratory for Advanced Signal Processing,Civil Aviation University of China,Tianjin 300300,China
关键词:
卫星着陆系统; 导航接收机; 精密进近; 性能评估
Keywords:
GBAS landing system(GLS); navigation receiver; precision approach; performance uation
分类号:
V241.6 TP391
DOI:
10.3969/j.issn.1001-4616.2020.04.013
文献标志码:
A
摘要:
作为新一代精密进近着陆系统,卫星着陆系统(GLS)有着传统着陆方式无法比拟的优势. 对GLS系统的性能评估有助于分析飞行品质和GLS机载产品适航认证,也可推动我国北斗系统在民航中的应用. 在对GLS机载子系统架构、精密进近运行中性能参数关系与需求的分析基础上,提出了一种GLS接收机的性能评估方案,研究和设计关键所需导航性能参数的评估算法,开发了面向精密进近运行需求的GLS接收机性能评估系统. 使用实际GLS进行着陆的飞机航迹数据的评估结果表明,本文的性能评估方案和系统是切实可行的.
Abstract:
As a new generation of precision approach landing system,GBAS landing system(GLS)has advantages that traditional landing methods cannot match. The performance uation of the GLS system is helpful for analyzing flight quality and airworthiness certification of GLS airborne parts. Moreover,it can promote the application of Beidou system in civil aviation. Through analyzing the architecture of airborne GLS subsystem,as well as the relationship between performance parameters and requirements during precision approach operations,a performance uation scheme for the GLS receiver is proposed. Then,the uation algorithms for key navigation performance parameters are researched and designed. A performance uation system for GLS receiver under requirements for precision approach operation is developed. The uation results of aircraft track data using actual GLS for landing show that the performance uation scheme and system in this paper are feasible.

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备注/Memo

备注/Memo:
收稿日期:2020-07-10.
基金项目:工业和信息化部民机专项科研基金项目(MJ-2017-S-44)、中央高校基本科研业务费项目(3122019050).
通讯作者:钟伦珑,博士,副教授,研究方向:民航智能信息处理与自动化. E-mail:zlunlong@163.com
更新日期/Last Update: 2020-11-15