Path: SC/BasicOrbit
% Computes the true anomaly from the eccentric or hyperbolic anomaly. Since version 1. -------------------------------------------------------------------------- Form: nu = E2Nu( e, E ) -------------------------------------------------------------------------- ------ Inputs ------ e (1,:) Eccentricity E (1,:) Eccentric or Hyperbolic anomaly ------- Outputs ------- nu (1,:) True anomaly -------------------------------------------------------------------------- References: Bate, R. R., Fundamentals of Astrodynamics. pp. 20-40. --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect
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