Path: Orbit/Interplanetary
% 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 --------------------------------------------------------------------------
Orbit: Interplanetary/ApophisOrbit Orbit: OrbitCoord/RelativeOrbitState Orbit: OrbitMechanics/RVOrbGen Orbit: RHSOrbit/RHSLinOrb SC: BasicOrbit/AdjustMeanAnomaly SC: BasicOrbit/OrbRate SC: Ephem/PlanetPosJPL Common: Control/QCR Common: Database/Constant Common: GUIs/TimeDisplay Common: General/DispWithTitle Common: Graphics/NewFig Common: Graphics/TimeHistory Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/Date2JD Common: Time/JD2Date Math: Integration/RK4 Math: Linear/Mag
Back to the Orbit Module page