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SUPPORT SITE |
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SUPPORT SITE |
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Path: SC/BasicOrbit
% Converts true anomaly to mean anomaly. -------------------------------------------------------------------------- Form: [meanAnom,eccAnom] = Nu2M( e, nu ) -------------------------------------------------------------------------- ------ Inputs ------ e (1,1) Eccentricity nu (1,:) True anomaly ------- Outputs ------- meanAnom (1,:) Mean anomaly eccAnom (1,:) Eccentric anomaly --------------------------------------------------------------------------
Common: Graphics/Plot2D SC: BasicOrbit/E2M SC: BasicOrbit/Nu2E
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