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.

http://celestialandorbitalmechanicswebsite.yolasite.com/

1.5

(2)

다운로드 수: 425

업데이트 날짜: 2022/12/28

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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 (2023). 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. 검색됨 2023/6/6.

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버전	게시됨	릴리스 정보
1.0.1	2022/12/28	Added Scott Campbell's algorithm	다운로드
1.0.0	2021/12/24		다운로드