Dynamic modeling of a LEO satellite's motion requires precise computation of atmospheric density for drag effect modeling. Here, Jacchia-Bowman 2006 and 2008 atmospheric models are used to calculate the total mass-desnity of atmosphere. Position of the Sun is computed by JPL Ephemerides (DE440) to improve accuracy of the model.
References:
인용 양식
Meysam Mahooti (2024). Jacchia-Bowman Atmospheric Density Model (https://www.mathworks.com/matlabcentral/fileexchange/56163-jacchia-bowman-atmospheric-density-model), MATLAB Central File Exchange. 검색됨 .
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버전 | 게시됨 | 릴리스 정보 | |
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2.1.2 | It was revised on 2022-12-14. |
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2.1.1 | test_JB2006.m is modified. |
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2.1.0 | JB2006.m and JB2008.m are modified. |
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2.0.0.0 | IERS.m, test_JB2006.m, and test_JB2008.m are modified to decrease CPU time. |
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1.1.0.0 | The image is added.
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1.0.0.0 |