CalcE.m
Versión 1.0.0.0 (1,4 KB) por
Richard Rieber
Calculates eccentric anomaly given mean anomaly and eccentricity of an elliptical orbit.
Since the eccentric anomaly cannot be directly calculated from certain given values, this function performs a simple Newton-Raphson iteration to solve for the eccentric anomaly within a given tolerance (default 10^-8 radians).
Citar como
Richard Rieber (2024). CalcE.m (https://www.mathworks.com/matlabcentral/fileexchange/6779-calce-m), MATLAB Central File Exchange. Recuperado .
Compatibilidad con la versión de MATLAB
Se creó con
R13
Compatible con cualquier versión
Compatibilidad con las plataformas
Windows macOS LinuxCategorías
- Aerospace > Aerospace Blockset > Guidance, Navigation, and Control (GNC) >
- Industries > Aerospace and Defense > CubeSat and Satellites >
- Aerospace > Aerospace Blockset > Reference Applications >
Más información sobre Guidance, Navigation, and Control (GNC) en Help Center y MATLAB Answers.
Etiquetas
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!Descubra Live Editor
Cree scripts con código, salida y texto formateado en un documento ejecutable.
Versión | Publicado | Notas de la versión | |
---|---|---|---|
1.0.0.0 | Didn't notice that MatLab already had a function entitled calce.m, so the file has been renamed to CalcEA.m. |