Calculates eccentric anomaly given mean anomaly and eccentricity of an elliptical orbit. in matlab

The following Matlab project contains the source code and Matlab examples used for 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).

The source code and files included in this project are listed in the project files section, please make sure whether the listed source code meet your needs there.

Project Files: 

File NameSize
CalcEA.m 939
license.txt 1314

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