Path: Interplanetary/AsteroidProspector
% Asteroid Prospector Simulation Simulate the Asteroid Prospector mission starting with a spiral out from Earth and performing a rendezvous with Apophis. Try different departure orbits to see the effect on the spiral portion of the orbit. The low-thrust rendezvous corrects each Keplerian orbital element sequentially. See also TransformECIToSEMR, SunEarthMoonSystemConstants, FCRTBPRHS, LowThrustCRTBP_StopFcn, SEMRToSEMI, SEMToSEMND, LowThrustDVToTransfer, LowThrustRendezvousSim
Interplanetary: AsteroidProspector/LowThrustDVToTransfer Interplanetary: AsteroidProspector/LowThrustRendezvousSim Interplanetary: AsteroidProspector/LowThrustTimeToTransfer Interplanetary: Ephemeris/ApophisOrbit Interplanetary: ThreeBody/FCRTBPRHS Interplanetary: ThreeBody/LowThrustCRTBP_StopFcn Orbit: OrbitCoord/SEMIToSEMR Orbit: OrbitCoord/SEMRToSEMI Orbit: OrbitCoord/SEMToSEMND Orbit: OrbitCoord/TransformECIToSEMR Orbit: OrbitData/SunEarthMoonSystemConstants Orbit: OrbitManeuver/LowThrustEscape Orbit: OrbitMechanics/RVOrbGen Orbit: Visualization/PlotSEMTraj SC: BasicOrbit/El2RV SC: BasicOrbit/Period SC: BasicOrbit/RV2El Common: GUIs/Figui Common: GUIs/ODETimeDisplay Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Time/Date2JD Math: Linear/Mag Math: Linear/Unit
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