Path: Orbit/OrbitCoord
% Computes the semi-latus rectum. -------------------------------------------------------------------------- Form: p = SLR( e, a ) -------------------------------------------------------------------------- ------ Inputs ------ e (1,:) Eccentricity a (1,:) Semi major axis (or perigee radius for parabola) ------- Outputs ------- p (1,:) Semi-latus rectum -------------------------------------------------------------------------- References: Bates, R.B. Fundamentals of Astrodynamics, pp. 28,34. --------------------------------------------------------------------------
Common: General/DeBlankLT Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Linear/DupVect
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