Satellite Efficiency regarding SAA
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).
Zitieren als
Robin Jehn (2024). Satellite Efficiency regarding SAA (https://www.mathworks.com/matlabcentral/fileexchange/70006-satellite-efficiency-regarding-saa), MATLAB Central File Exchange. Abgerufen .
Kompatibilität der MATLAB-Version
Plattform-Kompatibilität
Windows macOS LinuxKategorien
- Industries > Aerospace and Defense > CubeSat and Satellites >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
Tags
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!Live Editor erkunden
Erstellen Sie Skripte mit Code, Ausgabe und formatiertem Text in einem einzigen ausführbaren Dokument.
Functions
satellite orbits 1.0
Version | Veröffentlicht | Versionshinweise | |
---|---|---|---|
1.2.0 | Increased speed and accuracy + J2 pertubation + more functions |
||
1.1.0 | Increased speed and accuracy |
||
1.0.0 |