DocumentCode :
523306
Title :
Perturbation effects on the solar synchronous satellite
Author :
Qiu, Yi ; Wang, Ya
Author_Institution :
National Satellite Meteorological Center of China Meteorological Administration
fYear :
2009
fDate :
7-9 Dec. 2009
Firstpage :
769
Lastpage :
772
Abstract :
Due to the self-rotation, the earth becomes ellipsoid and the equator upheaves. Satellites will be affected by the perturbation when it rotates around the earth. In May, 27 of 2008, China launched the second generation solar synchronous meteorological satellite named FY-3. By analyzing the subpoint tracks of several recurrence intervals during the year, it is find that the perturbation affects greatly on FY-3 and the corresponding observation performance. This paper takes the actual data of subpoint track from FY-3 and gives a detailed analysis about the perturbation effects on the solar synchronous meteorological satellite.
Keywords :
Obit Drift; Perturbation Effect; Recurrence Intervals; Solar Synchronous Satellite;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Wireless Mobile and Computing (CCWMC 2009), IET International Communication Conference on
Conference_Location :
Shanghai, China
Type :
conf
Filename :
5521897
Link To Document :
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