Converting a state vector/orbital elements to a TLE
版本 1.0.1 (323.3 KB) 作者:
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.
引用格式
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. 检索来源 .
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R2019b
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