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 --------------------------------------------------------------------------