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Path: Orbit/OrbitCoord
% Computes true anomaly from a series expansion Since version 1. -------------------------------------------------------------------------- Form: nu = M2NuS( e, M ) -------------------------------------------------------------------------- ------ Inputs ------ e Eccentricity M (1,:) Mean anomaly (rad) ------- Outputs ------- nu True anomaly --------------------------------------------------------------------------
Common: Graphics/Plot2D Math: Analysis/SHarm
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