Titlebook: China Satellite Navigation Conference (CSNC) 2013 Proceedings; Precise Orbit Determ Jiadong Sun,Wenhai Jiao,Chuang Shi Conference proceedin

神經(jīng)

China Satellite Navigation Conference (CSNC) 2013 Proceedings978-3-642-37407-4Series ISSN 1876-1100 Series E-ISSN 1876-1119

Eviction

1876-1100 a.Hot topics in Global Navigation Satellite System.Includes .China Satellite Navigation Conference (CSNC) 2013 Proceedings. presents selected research papers from CSNC2013, held on 15-17 May in Wuhan, China. The theme of CSNC2013 is: BeiDou Application: Opportunities and Challenges. These papers dis

講個故事逗他

Mechanisms of Tracer Localizationaper, the continuous constant thrust maneuver model is established. And based on the measurement from C transponder, the COMPASS-GEO orbit determination is analyzed with maneuver arc. It realized the continuous orbit determination and prediction crossing the orbit maneuver.

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Radioactivity and Radioisotopes, This paper presents a method based on the orbital error correction of the wide area differential positioning algorithm. Based on analysis of the GEO satellite orbit maneuver characteristics and other factors that affect positioning accuracy, an improved algorithm is designed, which can enhance the positioning accuracy during orbit maneuver.

Talkative

Application of Thrust Force Model in GEO’s Orbit Determination in Case of Maneuversaper, the continuous constant thrust maneuver model is established. And based on the measurement from C transponder, the COMPASS-GEO orbit determination is analyzed with maneuver arc. It realized the continuous orbit determination and prediction crossing the orbit maneuver.

中世紀(jì)

A Method Based on the Orbital Error Correction of the Wide Area Differential Positioning Algorithm This paper presents a method based on the orbital error correction of the wide area differential positioning algorithm. Based on analysis of the GEO satellite orbit maneuver characteristics and other factors that affect positioning accuracy, an improved algorithm is designed, which can enhance the positioning accuracy during orbit maneuver.

赦免

https://doi.org/10.1007/978-94-011-7094-9ed with the actual Beidou satellites’ on-orbit data. The results showed that the two models which are raised in this paper can improve the accuracy of the Beidou IGSO/MEO orbit determination and prediction.

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