Satellite Orbit Computation

バージョン 1.3.0.0 (745 KB) 作成者: Charles Rino
Modified SGP4 code for GPS interface
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更新 2010/10/18

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A modified version of the SGP4 code used for standard satellite orbit computation using two-line elements (TLE). The modified code outputs satellite positions and velocity in ECF coordinates and universal time from EPOCH. Utilities are provided to calculate point-to-point angle, range rates, TCS positions, constant altitude intercepts and velocities. Outputs are collected in a structure and retained in a *.mat file for subsequent display and Beacon satellite data analysis applications. Documentation and examples are provided. Code uses GPS_CoordinateXform and IGRF utilities available from MATLAB Central.

引用

Charles Rino (2024). Satellite Orbit Computation (https://www.mathworks.com/matlabcentral/fileexchange/28888-satellite-orbit-computation), MATLAB Central File Exchange. 取得済み .

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SGP4/

SatGeom_Example/

utilities/

バージョン 公開済み リリース ノート
1.3.0.0

Corrected error in satGEOM utility. SGP4 is unaffected.
1.2.0.0

Error corrected in function satGEOM. Only affects results that use magnetic field geometry.
1.0.0.0