Path: Orbit/OrbitCoord
Convert an Alfriend orbital element set into the standard orbital element set % [a,th,i,q1,q2,W] -> [a,i,W,w,e,M] -------------------------------------------------------------------------- Form: el = Alfriend2El( ela ) -------------------------------------------------------------------------- ------ Inputs ------ ela (:,6) Alfriend orbital element set [a,th,i,q1,q2,W] where: th = true latitude q1 = e*cos(w) q2 = e*sin(w) ------- Outputs ------- el (:,6) Standard orbital element set [a,i,W,w,e,M] --------------------------------------------------------------------------
SC: BasicOrbit/Nu2M
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