This function is created to convert the classical orbital elements to cartesian position and velocity parameters of any satellite orbit in the geocentric - equatorial reference system.
Comment:
If you need an example code you can send me an e-mail.
Cleared for any question.
인용 양식
Thameur Chebbi (2024). Kepler2Carts (https://www.mathworks.com/matlabcentral/fileexchange/80632-kepler2carts), MATLAB Central File Exchange. 검색됨 .
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Help Center 및 MATLAB Answers에서 Satellite and Orbital Mechanics에 대해 자세히 알아보기
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