Path: Interplanetary/InterplanetaryOrbit
% Apophis 3D Lambert transfer delta-V analysis Starts with plotting the Earth and Apophis orbits. It thens uses PlanetTransferLambert to find the minimum delta-V for impulsive burns. This can be used to help design the low-thrust trajectory. The low-thrust problem is a rendezvous problem. See PorkChopTOFKepler to generate pork chop plots for Earth/Apophis missions. See also: Constant, ApophisOrbit, Date2JD, AdjustMeanAnomaly, RVOrbGen, PlanetPosJPL, NewFig, JD2Date, PlanetTransferLambert, Mag, Plot2D, AddFillToPlots, Figui % -------------------------------------------------------------------------- Copyright (c) 2023.1 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2023.1 --------------------------------------------------------------------------
Interplanetary: Ephemeris/ApophisOrbit Interplanetary: Ephemeris/PlanetPosJPL Interplanetary: InterplanetaryOrbit/PlanetTransferLambert Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/AdjustMeanAnomaly Common: Database/Constant Common: GUIs/Figui Common: Graphics/AddFillToPlots Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/Date2JD Common: Time/JD2Date
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