Design Analysis of a Hyperbolic Landing Navigation System for Aircraft

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F18%3A00535185" target="_blank" >RIV/60162694:G43__/18:00535185 - isvavai.cz</a>

Výsledek na webu

<a href="http://dx.doi.org/10.1109/EURONAV.2018.8433225" target="_blank" >http://dx.doi.org/10.1109/EURONAV.2018.8433225</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/EURONAV.2018.8433225" target="_blank" >10.1109/EURONAV.2018.8433225</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Design Analysis of a Hyperbolic Landing Navigation System for Aircraft

Popis výsledku v původním jazyce

Radio navigation is widely used nowadays, especially to precisely estimate aircraft position during the approach and landing phase of flight. However, it is challenging to ensure the accuracy of aircraft navigation using a transmission channel that changes rapidly due to noise and interference. To increase the safety and reliability of aircraft in the approach and landing phase, a hyperbolic landing system is proposed as a non-autonomous system. The main goal of this paper is to analyze the mechanism of radio signal propagation between the transmitters and receiver of a novel hyperbolic navigation system that uses the TDOA method. The paper evaluates the effects of the radio channel environment on the proposed system in the landing phase of flight. The theoretical analysis is verified by MATLAB simulations.

Název v anglickém jazyce

Design Analysis of a Hyperbolic Landing Navigation System for Aircraft

Popis výsledku anglicky

Radio navigation is widely used nowadays, especially to precisely estimate aircraft position during the approach and landing phase of flight. However, it is challenging to ensure the accuracy of aircraft navigation using a transmission channel that changes rapidly due to noise and interference. To increase the safety and reliability of aircraft in the approach and landing phase, a hyperbolic landing system is proposed as a non-autonomous system. The main goal of this paper is to analyze the mechanism of radio signal propagation between the transmitters and receiver of a novel hyperbolic navigation system that uses the TDOA method. The paper evaluates the effects of the radio channel environment on the proposed system in the landing phase of flight. The theoretical analysis is verified by MATLAB simulations.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20201 - Electrical and electronic engineering

Projekt

—

Návaznosti

S - Specificky vyzkum na vysokych skolach<br>I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2018

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

2018 European Navigation Conference (ENC)

ISBN

978-1-5386-4962-6

ISSN

—

e-ISSN

—

Počet stran výsledku

6

Strana od-do

148-153

Název nakladatele

IEEE

Místo vydání

Gothenburg, Sweden

Místo konání akce

Gothenburg, Sweden

Datum konání akce

14. 5. 2018

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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