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: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Analysis/SHarm
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