Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/28263
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dc.contributor.authorКуценко Олександр, Kutsenko Oleksandr-
dc.contributor.authorІльницька Світлана, Ilnytska Svitlana-
dc.contributor.authorКонин Валерий, Konin Valeriy-
dc.date.accessioned2017-05-25T12:59:19Z-
dc.date.available2017-05-25T12:59:19Z-
dc.date.issued2017-05-12-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/28263-
dc.description.abstractThe paper shows the results of simulation of troposphere residual errors in the satellite based aircraft landing system. For such simulation the troposphere MOPS model has been used. The presented simulated troposphere parameters include: dry and wet components of the refraction index and troposphere scale height. Beside of that the simulated residual value of troposphere error for navigation satellites in view of satellite landing system has been presenteduk_UA
dc.publisherProceedings of the 20th Conference for Junior Researchers ‘Science – Future of Lithuania’ TRANSPORT ENGINEERING AND MANAGEMENT, 12 May 2017, Vilnius, Lithuania. - P. 63-68uk_UA
dc.subjectglobal navigation satellite systems (GNSS), landing system, GBAS, troposphere, tropospheric delay, modellinguk_UA
dc.titleTROPOSPHERE PARAMETERS CALCULATION AND RESIDUAL ERROR MODELING FOR GNSS LANDING SYSTEMuk_UA
dc.typeArticleuk_UA
Appears in Collections:Аерокосмічні технології та системи. Матеріали конференцій

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