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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:CHEN Xin-long,Yang Di,Zhai Kun.Zenith pass tracing of the inter-satellite linkage antenna[J].Journal of Harbin Institute Of Technology(New Series),2010,17(2):292-296.DOI:10.11916/j.issn.1005-9113.2010.02.027.
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Zenith pass tracing of the inter-satellite linkage antenna
Author NameAffiliation
CHEN Xin-long Dept. of Astronautical Engineering,Harbin Institute of Technology,Harbin 150001,China 
Yang Di Dept. of Astronautical Engineering,Harbin Institute of Technology,Harbin 150001,China 
Zhai Kun Dept. of Astronautical Engineering,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
The inter-satellite linkage antenna of the user satellite uses the Elevation-over-Azimuth type,and the zenith pass problem occurs during tracing TDRS. Firstly,the movement laws of the inter-satellite linkage is introduced for predicting the movement of the user satellite antenna. Then,the potential zenith pass moment is analyzed in detail. Some special orbits for the user satellite that can avoid the blindness zone are obtained. Finally,the zenith pass tracing strategies for the user satellite antenna based on the mechanical tilting are designed by using the trajectory preprocessor. The designs are based on the predicting results of the movement laws of the inter-satellite linkage. The strategies are proved to be reasonable and feasible for solving the zenith pass problem by simulation.
Key words:  TDRS  inter-satellite linkage  trajectory preprocessor  mechanical tilting
DOI：10.11916/j.issn.1005-9113.2010.02.027
Clc Number:TN828.5
Fund:

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