首页|期刊导航|南京航空航天大学学报(英文版)|高保真进近偏差重构:融合快速存取记录器飞行数据与仪表着陆系统电磁信号物理特性

高保真进近偏差重构:融合快速存取记录器飞行数据与仪表着陆系统电磁信号物理特性OA

High-Fidelity Reconstruction of Approach Deviations:Integrating QAR Flight Data with ILS Electromagnetic Signal Physics

中文摘要英文摘要

精准检测进近阶段的飞行轨迹偏差对于识别运行风险和提升航空安全至关重要.但由于缺乏高保真的物理参考模型,现有监测方法在区分环境信号畸变与飞行员操作误差时往往面临巨大挑战.为突破此类局限性,本研究通过将飞行快速存取记录器(Quick access recorder,QAR)数据与严密的导航物理建模相融合,建立了一个涵盖所需导航性能(Required navigation performance,RNP)与仪表着陆系统(Instrument landing system,ILS)进近的综合仿真框架.具体而言,以临汾尧都机场为主要研究对象,构建了一个特定的"数字孪生"模型.首先结合墨卡托投影和气压垂直导航逻辑进行了三维轨迹重建,随后利用天线阵列和镜像理论对ILS信号开展电磁仿真,以准确模拟多径效应.实证检验表明,该模型能够准确复现干涉条纹和次级下滑道波瓣等关键信号特征.在此高保真物理环境的基础上,通过定量回归分析确立了由物理模型推导出的理论调制度差(Difference in depth of modulation,DDM)与飞行员观测到的仪表刻度偏差(Distance off track,DOT)之间存在显著的线性相关性,从而为解释驾驶舱指示数据提供了经过严格验证的校准方程.最终通过对特定垂直偏差异常事件的深度调查,证实了该框架的实用价值:成功追溯了从信号失真到不安全着陆(如高度超限和拉平压缩)之间的因果关系链.本文为持续的飞行品质监控提供了一种稳健的、数据驱动的方法,并为识别导航事故的根本原因提供了科学依据.

Precise detection of flight path deviations during the approach phase is critical for identifying operational risks and enhancing aviation safety.However,existing monitoring methods often face significant challenges in distinguishing between environmental signal distortions and operational handling errors due to the lack of high-fidelity physical reference models.To address these limitations,this study establishes an integrated simulation framework for required navigation performance(RNP)and instrument landing system(ILS)approaches by synthesizing quick access recorder(QAR)data with rigorous navigation modeling.A site-specific"digital twin"of Linfen Yaodu Airport is constructed,incorporating 3D trajectory reconstruction based on Mercator projection and Baro-VNAV logic,alongside an electromagnetic simulation of ILS signals utilizing antenna array and image theory to model multipath effects.Empirical validation demonstrates that the model accurately reproduces critical signal characteristics,including interference fringes and secondary glide slope lobes.Furthermore,quantitative regression analysis establishes a definitive linear correlation(R2>0.98)between the theoretical difference in depth of modulation(DDM)and the pilot-observed distance off track(DOT),providing a verified calibration equation for interpreting cockpit indications.The practical utility of the framework is substantiated through the investigation of a specific vertical deviation anomaly,where the model successfully traces the causal chain from signal distortion to unsafe landing parameters such as threshold height exceedance and flare compression.This research offers a robust,data-driven methodology for continuous flight quality monitoring and provides a scientific foundation for identifying the root causes of navigation incidents.

刘济明;高振兴;李玥

南京航空航天大学民航学院,南京 211106,中国南京航空航天大学通用航空与飞行学院,南京 211106,中国南京航空航天大学通用航空与飞行学院,南京 211106,中国

航空航天

飞行偏差检测飞行品质监控RNP进近程序仪表着陆系统

flight deviation detectionflight quality monitoringRNP approach procedureinstrument landing system(ILS)

《南京航空航天大学学报(英文版)》 2026 (2)

187-202,16

This work was supported by the Na-tional Natural Science Foundations of China(Nos.U2333202,52272351)and the Civil Aviation Capacity Build-ing Fund Project(No.ASSA2024/121).

10.16356/j.1005-1120.2026.02.003

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