Path: Interplanetary/InterplanetaryOrbit
% Mars 3D optimal trajectory with a linear regulator Starts with plotting the Earth and Mars orbits. It then uses an optimal regulator to do the transfer with a linearized orbit. This nulls the error but has no limits on acceleration so requires a high delta-V. ------------------------------------------------------------------------ See also Constant, PlanetPosJPL, NewFig, JD2Date, ECI2Hills, OrbRate, RHSLinOrb, QCR, RK4, TimeHistory ------------------------------------------------------------------------ % -------------------------------------------------------------------------- Copyright (c) 2023.1 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2023.1 --------------------------------------------------------------------------
FormationFlying: Coord/GetHillsMats Interplanetary: Ephemeris/PlanetPosJPL Orbit: OrbitCoord/RelativeOrbitState Orbit: RHSOrbit/RHSLinOrb SC: BasicOrbit/FOrbCart SC: BasicOrbit/OrbRate Common: Control/QCR Common: Database/Constant Common: GUIs/TimeDisplay Common: General/DispWithTitle Common: Graphics/NewFig Common: Graphics/Plot3D Common: Graphics/TimeHistory Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/Date2JD Common: Time/JD2Date Math: Integration/RK4 Math: Linear/Mag
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