Отрывок: 0°E, 140.0°E, and 160°E longitudes, respectively. The inclination of the orbit of a BDS MEO is about 55°, and the orbit height is between that of GPS and Galileo satellites. The revolution period is about 773 minutes, leading to 1.86 revolutions per day. The ground track of the satellite repeats every seven days. We can appreciate in the following figure 4. Figure 4. The distribution of “BETS” and the tracks of the sub-satellite points of four GEO, five IGSO and two MEO, BDS Sat...
Полная запись метаданных
Поле DC Значение Язык
dc.contributor.authorCari J. S.ru
dc.contributor.authorBorre K.ru
dc.contributor.authorSamara National Research Universityru
dc.contributor.authorInstitute of ITru
dc.contributor.authorMathematics and Electronicsru
dc.coverage.spatialкосмическое созвездиеru
dc.coverage.spatialприемникru
dc.coverage.spatialMATLABru
dc.coverage.spatialспутниковая видимостьru
dc.coverage.spatialсистема координатru
dc.creatorCari J. S.ru
dc.date.issued2017ru
dc.identifierRU\НТБ СГАУ\ВКР20190402131530ru
dc.identifier.citationCari, J. S. Accuracy investigation of BeiDou outside China : [вып. квалификац. работа по спец. "Прикладные математика и физика"] / Jaime Cari Siles ; supervisor K. Borre ; Samara National Research University, Institute of IT, Mathematics and Electronics, Faculty of Electronics and Instrument Engineering, Inter-University Departme. - Samara, 2017. - on-lineru
dc.description.abstractThe subject of research is we analyze what the current performance of the BDS is outside China. The goal of the research a test the current performance of BDS accuracy worldwide and on Volga region using a standalone case. Using the software program MATLAru
dc.format.extentЭлектрон. дан. (1 файл : 2,1 Мб)ru
dc.titleAccuracy investigation of BeiDou outside Chinaru
dc.typeTextru
dc.subject.rugasnti50.01ru
dc.subject.udc004.9ru
dc.textpart0°E, 140.0°E, and 160°E longitudes, respectively. The inclination of the orbit of a BDS MEO is about 55°, and the orbit height is between that of GPS and Galileo satellites. The revolution period is about 773 minutes, leading to 1.86 revolutions per day. The ground track of the satellite repeats every seven days. We can appreciate in the following figure 4. Figure 4. The distribution of “BETS” and the tracks of the sub-satellite points of four GEO, five IGSO and two MEO, BDS Sat...-
Располагается в коллекциях: Выпускные квалификационные работы

Файлы этого ресурса:
Файл Размер Формат  
Кари_Силес_Хаиме_Accuracy_investigation_BeiDou.pdf2.13 MBAdobe PDFПросмотреть/Открыть  
Показать базовое описание ресурса Просмотр статистики
Поделиться:



Все ресурсы в архиве электронных ресурсов защищены авторским правом, все права сохранены.