CalcE.m Matlab script

Version:
File size: 0 KB
File name: CalcEA.m
Last update: 24 Oct 2011
Platform: Windows / Linux / BSD / Solaris
Language: Matlab
Price: Freeware
Company: Richard Rieber (View more)

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CalcE.m script details

CalcE.m script description:

Publisher review:
CalcE.m 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). Requirements: · MATLAB Release: R13

CalcE.m is a Matlab script for Astronomy/Aerospace scripts design by Richard Rieber. It runs on following operating system: Windows / Linux / BSD / Solaris.
CalcE.m calculates eccentric anomaly given mean anomaly and eccentricity of an elliptical orbit.

Operating system:
Windows / Linux / BSD / Solaris