Path: Interplanetary/InterplanetaryOrbit
% Compute a transfer from earth orbit to the asteroid Apophis. This uses LambertOpt to search for an optimal start and transfer time given the initial positions of the bodies. See also Constant, LambertOpt, DVTransfer, PlotLambertTransfer %
Orbit: OrbitControl/LambertOpt Orbit: RHSOrbit/FOrb Orbit: Visualization/PlotLambertTransfer Common: Database/Constant Math: Integration/RK45
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