Converting a state vector/orbital elements to a TLE
버전 1.0.1 (323 KB) 작성자:
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.
인용 양식
David Eagle (2025). 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. 검색 날짜: .
MATLAB 릴리스 호환 정보
개발 환경:
R2019b
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도움 준 파일: TLE_convert
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