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Path: Orbit/OrbitCoord
% Computes the eccentricity from apogee and perigee radii Since version 1. -------------------------------------------------------------------------- Form: e = RARP2E( rA, rP ) -------------------------------------------------------------------------- ------ Inputs ------ rA (1,m) Apogee radius rP (1,n) Perigee radius ------- Outputs ------- e (m,n) eccentricity --------------------------------------------------------------------------
Common: Graphics/Mesh2 Math: Linear/DupVect
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