Path: Interplanetary/InterplanetaryOrbit
% Apophis 3D optimal trajectory with a linear regulator Starts with plotting the Earth and Apophis orbits. It then uses an optimal regulator to do the transfer with a linearized orbit. ------------------------------------------------------------------------ See also Constant, ApophisOrbit, AdjustMeanAnomaly, RVOrbGen, PlanetPosJPL, NewFig, JD2Date, ECI2Hills, OrbRate, RHSLinOrb, QCR, RK4, TimeHistory ------------------------------------------------------------------------ % -------------------------------------------------------------------------- Copyright (c) 2023.1 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2023.1 --------------------------------------------------------------------------