Converting a state vector/orbital elements to a TLE
Versión 1.0.1 (323 KB) por
David Eagle
MATLAB scripts that can be used to calculate an a Two Line Element (TLE) from a user-provided osculating state vector or orbital elements.
MATLAB script that can be used to calculate an approximate Two Line Element (TLE) set from a user-provided osculating state vector or classical orbital elements. It is valid for spacecraft that can be modeled using the NORAD SGP4 algorithm. Includes PDF users guide.
Citar como
David Eagle (2024). Converting a state vector/orbital elements to a TLE (https://www.mathworks.com/matlabcentral/fileexchange/104065-converting-a-state-vector-orbital-elements-to-a-tle), MATLAB Central File Exchange. Recuperado .
Compatibilidad con la versión de MATLAB
Se creó con
R2019b
Compatible con cualquier versión
Compatibilidad con las plataformas
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