完整後設資料紀錄
DC 欄位語言
dc.contributor.authorKong, Qiaolien_US
dc.contributor.authorGuo, Jinyunen_US
dc.contributor.authorHwang, Cheinwayen_US
dc.contributor.authorGao, Fanen_US
dc.contributor.authorLin, Hsinfaen_US
dc.contributor.authorZhao, Chunmeien_US
dc.date.accessioned2015-07-21T08:28:19Z-
dc.date.available2015-07-21T08:28:19Z-
dc.date.issued2014-12-01en_US
dc.identifier.issn2213-5812en_US
dc.identifier.urihttp://dx.doi.org/10.1007/s40328-014-0066-4en_US
dc.identifier.urihttp://hdl.handle.net/11536/124091-
dc.description.abstractHY-2A is the first ocean dynamic environment monitoring satellite of China, and its precise radial orbit is a critical factor to its scientific research application, for example, its orbit can serve as a reference frame for altimeter measurement. In order to realize precise orbit determination, HY-2A is equipped with Doppler orbitography and radiopositioning integrated by satellite (DORIS), retro-reflector array for the satellite laser ranging (SLR) and global positioning system tracking systems. In this study, DORIS Doppler data is used for its good reputation for precise orbit positioning. We described the strategy of orbit determination using dynamic models in detail, and particularly analyzed the relationship between arc length, orbital determination accuracy, and consumed time, and then concluded that 3-day is the optimal arc length. We carried out detail accuracy assessments of external orbit comparison, overlap orbit validation and SLR range validation. Experimental results show that the radial accuracy can reach 0.0154 m for the 3-day arc, and the radial overlap validation accuracy is better than 0.0223 m, and the accuracy of SLR range validation is better than 0.0964 m. Results demonstrate that the DORIS system meets the orbit precision specifications of HY-2A satellite.en_US
dc.language.isoen_USen_US
dc.subjectHY-2Aen_US
dc.subjectPrecise orbit determinationen_US
dc.subjectOrbit assessmenten_US
dc.subjectDORISen_US
dc.titlePrecise orbit determination and accuracy analysis of HY-2A satellite using DORIS Doppler dataen_US
dc.typeArticleen_US
dc.identifier.doi10.1007/s40328-014-0066-4en_US
dc.identifier.journalACTA GEODAETICA ET GEOPHYSICAen_US
dc.citation.volume49en_US
dc.citation.spage455en_US
dc.citation.epage470en_US
dc.contributor.department土木工程學系zh_TW
dc.contributor.departmentDepartment of Civil Engineeringen_US
dc.identifier.wosnumberWOS:000346798500005en_US
dc.citation.woscount1en_US
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