Path: Orbit/OrbitMechanics
% Computes the mean anomaly from the true anomaly without wrapping btwn -pi / pi -------------------------------------------------------------------------- Form: M = Nu2MAbs( e, nu, tol, nMax ); -------------------------------------------------------------------------- ------ Inputs ------ e Eccentricity nu True anomaly (rad) tol Tolerance (optional) nMax Maximum number of iterations (optional) ------- Outputs ------- M Mean anomaly (rad) --------------------------------------------------------------------------
Orbit: OrbitMechanics/Nu2M
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