在接近着陆阶段双曲导航的可能性

Radim Bloudíček, P. Makula, J. Bajer, Miloslav Svarc
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引用次数: 7

摘要

本文旨在分析基于双曲TDOA(到达时差)的飞机导航系统在飞行进近到着陆阶段实现的可能性。为此,目前使用的是传统的系统,如ILS, MLS, GNSS等。对双曲系统的要求是根据实际使用系统的精度来确定的。通过对帕尔杜比采LKPD机场的仿真验证了实现这些要求的可能性。最后一节描述了系统的结构以及提出的编码信号,这是初始实际实验的起点。
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Possibilities of hyperbolic navigation during the approach to landing phase
The paper is aimed at the analysis of possibilities of the implementation of the hyperbolic TDOA (Time Difference Of Arrival) based system intended for aircraft navigation during the approach to landing phase of flight. For this purpose, conventional systems like ILS, MLS, GNSS, etc. are used today. Requirements on hyperbolic system were determined based on accuracy of actually utilized systems. The possibility to achieve these requirements was verified by simulation for LKPD Pardubice airport. The final section describes the configuration of the system together with proposed coded signals, which are starting point for initial real experiments.
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