Planet9:

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
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Children:

Interplanetary: Visualization/HelioPlot
Orbit: Optimization/SpacecraftFromAccel
Orbit: Optimization/TrajectoryBetweenTwoPlanets
Orbit: OrbitMechanics/RVOrbGen
Common: Database/Constant
Common: Time/Date2JD

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