Determination of Precise Orbits and Gravity Models Using Simulated ROCSAT-3/COSMIC Tracking Data
碩士 === 國立交通大學 === 土木工程系所 === 92 === In this study, a ’two-step’ approach is used to compute precise orbits and estimate parameters of satellite perturbing forces. The approach is based on satellite equations of motion (EOM) and parameter estimation theory. The perturbing forces under consideration a...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/3h999a |