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
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