Path: Orbit/OrbitCoord
% Computes the orbit position vector in the perifocal plane. Since version 1. -------------------------------------------------------------------------- Form: r = RPQ( e, rP, nu ) -------------------------------------------------------------------------- ------ Inputs ------ e Eccentricity rP Perigee radius nu True anomaly (rad) ------- Outputs ------- r [xP;xQ;0] -------------------------------------------------------------------------- References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988, p. 63. --------------------------------------------------------------------------
Orbit: OrbitCoord/ROrb 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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