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Path: Orbit/OrbitCoord
% Computes the perigee radius from a. Since version 1. -------------------------------------------------------------------------- Form: rP = A2Perige( a, e ) -------------------------------------------------------------------------- ------ Inputs ------ a Semi major axis e Eccentricity ------- Outputs ------- rP Perigee radius -------------------------------------------------------------------------- References: Bate, R. R., Fundamentals of Astrodynamics. pp. 20-40. --------------------------------------------------------------------------
Common: Graphics/Mesh2 Math: Linear/DupVect
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