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.
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Meysam Mahooti (2024). Jacchia-Bowman Atmospheric Density Model (https://www.mathworks.com/matlabcentral/fileexchange/56163-jacchia-bowman-atmospheric-density-model), MATLAB Central File Exchange. 检索来源 .
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R2021b
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