CalcE.m
Calculates eccentric anomaly given mean anomaly and eccentricity of an elliptical orbit.
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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).
Cite As
Richard Rieber (2026). CalcE.m (https://www.mathworks.com/matlabcentral/fileexchange/6779-calce-m), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.0.0.0 (1.4 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 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. |
