Input any Longitude Latitude and Altitude into SAA and it will return 1 for operational and 0 for not operational due to a radiation higher than 0.8 protons/cm^2/s. An edited version of the orbit propagator TwoBody from Satellite Orbits: Models, Methods and Applications (v1.0.0), which now includes J2 pertubation and better performance, is used.
See files for documentation.
True anomaly and excentricity is always assumed to be 0 (If you want to change that go to position_vector.m and change the input arguments and values forwarded to TwoBody).
인용 양식
Robin Jehn (2024). Satellite Efficiency regarding SAA (https://www.mathworks.com/matlabcentral/fileexchange/70006-satellite-efficiency-regarding-saa), MATLAB Central File Exchange. 검색됨 .
MATLAB 릴리스 호환 정보
플랫폼 호환성
Windows macOS Linux카테고리
- Industries > Aerospace and Defense > CubeSat and Satellites >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
태그
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!