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...
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Поле DC | Значение | Язык |
---|---|---|
dc.contributor.author | Cari J. S. | ru |
dc.contributor.author | Borre K. | ru |
dc.contributor.author | Samara National Research University | ru |
dc.contributor.author | Institute of IT | ru |
dc.contributor.author | Mathematics and Electronics | ru |
dc.coverage.spatial | космическое созвездие | ru |
dc.coverage.spatial | приемник | ru |
dc.coverage.spatial | MATLAB | ru |
dc.coverage.spatial | спутниковая видимость | ru |
dc.coverage.spatial | система координат | ru |
dc.creator | Cari J. S. | ru |
dc.date.issued | 2017 | ru |
dc.identifier | RU\НТБ СГАУ\ВКР20190402131530 | ru |
dc.identifier.citation | Cari, 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-line | ru |
dc.description.abstract | The 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 MATLA | ru |
dc.format.extent | Электрон. дан. (1 файл : 2,1 Мб) | ru |
dc.title | Accuracy investigation of BeiDou outside China | ru |
dc.type | Text | ru |
dc.subject.rugasnti | 50.01 | ru |
dc.subject.udc | 004.9 | ru |
dc.textpart | 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... | - |
Располагается в коллекциях: | Выпускные квалификационные работы |
Файлы этого ресурса:
Файл | Размер | Формат | |
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Кари_Силес_Хаиме_Accuracy_investigation_BeiDou.pdf | 2.13 MB | Adobe PDF | Просмотреть/Открыть |
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