Path: Orbit/OrbitManeuver
% Computes the velocity and inclination errors for a delta V burn Since version 1. -------------------------------------------------------------------------- Form: [v, dec, dV, dI] = DVDisp( i, vA, vT, decErr, vErr, nPlot ) -------------------------------------------------------------------------- ------ Inputs ------ i Target change in inclination (deg) vA Apogee velocity vT Target velocity decErr Declination fractional error range (0.1 = 10%) vErr Velocity fractional error range nPlot Number of plot points ------- Outputs ------- v Ideal delta-v dec Ideal declination (deg) dV Velocity Error dI Inclination Error --------------------------------------------------------------------------
Common: General/DeBlankLT Common: Graphics/NewFig Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS
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