Path: Interplanetary/OrbitOptimization
% Optimal continous thrust transfer to Planet 9 Compute an optimal 3D trajectory to Planet 9's presumed orbit. Size a spacecraft to bring a specific payload there given engine parameters. This demo requires the optimization toolbox. See also: Constant, RVOrbGen, Date2JD, TrajectoryBetweenTwoPlanets, SpacecraftFromAccel % -------------------------------------------------------------------------- Copyright (c) 2021 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2021.1 --------------------------------------------------------------------------
Interplanetary: Visualization/HelioPlot Orbit: Optimization/SpacecraftFromAccel Orbit: Optimization/TrajectoryBetweenTwoPlanets Orbit: OrbitMechanics/RVOrbGen Common: Database/Constant Common: Time/Date2JD
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