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SUPPORT SITE |
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SUPPORT SITE |
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Path: SC/BasicOrbit
% Computes the true anomaly from the mean anomaly without wrapping. Between -pi / pi -------------------------------------------------------------------------- Form: nu = M2NuAbs( e, M, tol, nMax ) -------------------------------------------------------------------------- ------ Inputs ------ e Eccentricity M Mean anomaly (rad) tol Tolerance (optional) nMax Maximum number of iterations (optional) ------- Outputs ------- nu True anomaly (rad) --------------------------------------------------------------------------
SC: BasicOrbit/M2Nu
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