Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/25242
Full metadata record
DC FieldValueLanguage
dc.contributor.authorКонин Валерий, Konin Valeriy-
dc.contributor.authorKovalevskiy Eduard-
dc.contributor.authorOlevinska Tetiana-
dc.date.accessioned2017-03-12T14:55:27Z-
dc.date.available2017-03-12T14:55:27Z-
dc.date.issued2013-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/25242-
dc.description.abstractAn algorithm of calculating the guidance parameters for GNSS aircraft landing technology was considered. The simulation and evaluation of calculation parameters error were performed as welluk_UA
dc.description.sponsorshipNational Aviation Universityuk_UA
dc.publisherProceedings of the National Aviation University. – 2013.– N 3 (56).– P. 18 - 21uk_UA
dc.subjectflying machine; guidance parameters; guidance procedure; landing system; modeling; navigation system; trajectoryuk_UA
dc.titleGNSS TECHNOLOGY DETERMINATION OF FLYING MACHINE GUIDANCE PARAMETERSuk_UA
dc.typeArticleuk_UA
dc.subject.udcUDC 629.735.051.83(045)-
Appears in Collections:Наукові статті кафедри аеронавігаційних систем

Files in This Item:
File Description SizeFormat 
Konin.pdfРассмотрен алгоритм расчета параметров наведения для посадки летательного аппарата по технологии GNSS194.18 kBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.