SIMULATION OF EGNOS SATELLITE NAVIGATION SIGNAL USAGE FOR AIRCRAFT LPV PRECISION INSTRUMENT APPROACH
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F21%3APU147673" target="_blank" >RIV/00216305:26210/21:PU147673 - isvavai.cz</a>
Result on the web
<a href="https://www.scopus.com/record/display.uri?eid=2-s2.0-85118916139&origin=AuthorNamesList&txGid=4a5dc39e2dfda78e8d89caa94cdda2e3&isValidNewDocSearchRedirection=false" target="_blank" >https://www.scopus.com/record/display.uri?eid=2-s2.0-85118916139&origin=AuthorNamesList&txGid=4a5dc39e2dfda78e8d89caa94cdda2e3&isValidNewDocSearchRedirection=false</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.3846/aviation.2021.14554" target="_blank" >10.3846/aviation.2021.14554</a>
Alternative languages
Result language
angličtina
Original language name
SIMULATION OF EGNOS SATELLITE NAVIGATION SIGNAL USAGE FOR AIRCRAFT LPV PRECISION INSTRUMENT APPROACH
Original language description
Satellite navigation has become a very important topic in the air transport industry along with its application in instrument approach procedures. Recently, extracted statistical characteristics of the European Geostationary Navigation Overlay Service (EGNOS) satellite signal have been made available from real measurements in the Czech Republic. The numerical modeling approach is taken for a feasibility study of automatic aircraft control during the Localizer Performance with Vertical Guidance (LPV) precision approach based on such navigation data. The model incorporates Kalman filtering of the stochastic navigation signal, feed-back control of L-410 aircraft dynamics and the calculation of approach progress along the predefined procedure. Evaluation of the performance of the system prototype is performed using the scenarios developed with a strong interest in altitude control. he specific scenario is focused on a curved approach which offers a huge advantage of the approaches based on the Satellite-based Augmentation System (SBAS) compared to ones with the Instrument Landing System (HS). Outputs of simulation executions are statistically analyzed and assessed against predefined navigation performance goals equivalent to ILS categories with a positive outcome.
Czech name
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Czech description
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Classification
Type
J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2021
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
AVIATION
ISSN
1648-7788
e-ISSN
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Volume of the periodical
25
Issue of the periodical within the volume
3
Country of publishing house
LT - LITHUANIA
Number of pages
11
Pages from-to
171-181
UT code for WoS article
000719866900005
EID of the result in the Scopus database
2-s2.0-85118916139