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Kepler's equation solver

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% Input - Mean anomaly M [rad] , Eccentricity e and Epsilon % Output - eccentric anomaly E [rad]

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Description

% Function solves Kepler's equation M = E-e*sin(E)
% Input - Mean anomaly M [rad] , Eccentricity e and Epsilon
% Output eccentric anomaly E [rad].

Required Products MATLAB
MATLAB release MATLAB 7.10 (R2010a)
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