Path: Orbit/OrbitCoord
% Computes the orbit radius. Type ROrb for a demo -------------------------------------------------------------------------- Form: r = ROrb( e, rp, f ) -------------------------------------------------------------------------- ------ Inputs ------ e (1,1) Eccentricity rp (1,1) Perigee radius f (1,:) True anomaly ------- Outputs ------- r (1,:) Radius -------------------------------------------------------------------------- References: Bate, R. R., Fundamentals of Astrodynamics. pp. 20-40. --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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