Estimation of TLE Orbital Parameters of Satellites using Doppler Shift
碩士 === 國立成功大學 === 電機工程學系 === 102 === The Two-Line-Elements (TLE) of satellites contains the orbital parameters used to calculate its position at a determined time based on a referential Earth Centered Inertial (ECI) system. These parameters are given publicly by the North American Aerospace Defense...
Main Authors: | , |
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Other Authors: | |
Format: | Others |
Language: | en_US |
Published: |
2014
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Online Access: | http://ndltd.ncl.edu.tw/handle/95752623020822418592 |