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Path: Orbit/OrbitCoord
% Computes the orbit radius. Since version 1. -------------------------------------------------------------------------- Form: r = ROrb( e, rp, f ) -------------------------------------------------------------------------- ------ Inputs ------ e Eccentricity rp Perigee radius f True anomaly ------- Outputs ------- r Radius -------------------------------------------------------------------------- References: Bate, R. R., Fundamentals of Astrodynamics. pp. 20-40. --------------------------------------------------------------------------
Common: Graphics/Plot2D
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