Path: SC/BasicOrbit
% Converts true anomaly to eccentric or hyperbolic anomaly. For a demo plot use Nu2E( e ). -------------------------------------------------------------------------- Form: E = Nu2E( e, nu ) -------------------------------------------------------------------------- ------ Inputs ------ e (1,:) or (1,1) Eccentricity nu (1,:) True anomaly ------- Outputs ------- E (1,:) Eccentric or hyperbolic anomaly -------------------------------------------------------------------------- References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988, pp. 57,60. --------------------------------------------------------------------------
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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