The Functionality of Satellite Navigation System on a Flight with Acrobatic Elements: Ground and Flight Testing

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21260%2F17%3A00311956" target="_blank" >RIV/68407700:21260/17:00311956 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1109/MILTECHS.2017.7988833" target="_blank" >http://dx.doi.org/10.1109/MILTECHS.2017.7988833</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/MILTECHS.2017.7988833" target="_blank" >10.1109/MILTECHS.2017.7988833</a>

Result language
angličtina
Original language name
The Functionality of Satellite Navigation System on a Flight with Acrobatic Elements: Ground and Flight Testing
Original language description
This paper deals with functionality verification of satellite navigation system GPS-150 before its application for air traffic. The goal of this project was to verify GPS-150 properties with regard to its fundamental functionality – provision of navigation information during flight. Within the research, the main focused was placed on GPS-150 operation during specific flight conditions with acrobatic elements. Another goal of the project was to obtain complementary operational information, which were not included in user’s handbook. For this purpose, ground-based verification methodologies were developed. The project was concluded by flight tests.
Czech name
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Czech description
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Publication year
2017
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Proceedings of the 2017 International Conference on Military Technologies (ICMT)
ISBN
978-1-5386-1988-9
ISSN
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e-ISSN
—
Number of pages
7
Pages from-to
625-631
Publisher name
Ministerstvo obrany, Univerzita obrany
Place of publication
Brno
Event location
Brno
Event date
May 31, 2017
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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