CalcE.m

Version 1.0.0.0 (1.4 KB) by Richard Rieber
Calculates eccentric anomaly given mean anomaly and eccentricity of an elliptical orbit.
4.0
(1)
4.6K Downloads
Updated 26 Jan 2005

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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 (2024). CalcE.m (https://www.mathworks.com/matlabcentral/fileexchange/6779-calce-m), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R13
Compatible with any release
Platform Compatibility
Windows macOS Linux

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Version Published Release Notes
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.