Solve Kepler's Equation for E Matlab script

Version:
File size: 0 KB
File name: solve_Kepler_for_E.m
Last update: 29 Dec 2009
Platform: Windows / Linux / Mac OS / BSD / Solaris
Language: Matlab
Price: Freeware
Company: John Shelton (View more)

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Solve Kepler's Equation for E script details

Solve Kepler's Equation for E script description:

Publisher review:
Solve Kepler's Equation for E calculates Eccentric Anomaly given Mean Anomaly Given mean anomaly and eccentricity of an orbit, eccentric anomaly can be calculated using Kepler's Equation. However, the equation is nonlinear, and an iterative technique must be used.

This program uses a fixed-point iterative technique to output eccentric anomaly to a user defined tolerance, or to a default tolerance of 10^-9 radians.

Solve Kepler's Equation for E is a Matlab script for Astronomy/Aerospace scripts design by John Shelton. It runs on following operating system: Windows / Linux / Mac OS / BSD / Solaris.

Operating system:
Windows / Linux / Mac OS / BSD / Solaris