Path: Orbit/OrbitManeuver
% Orbit separation simulation with discrete delta-Vs Simulates a discrete phasing maneuver in the absolute frame. Includes a simple drag model and point-mass gravity. The simulation runs for twice the desired transfer time. %
AerospaceUtils: AtmosphericCalculations/AtmDens2 AerospaceUtils: Coord/ECIToEF Orbit: OrbitControl/DVTarget Orbit: OrbitCoord/RelativeCoord Orbit: OrbitMechanics/CylOrb Orbit: OrbitMechanics/LambertTOF Orbit: OrbitMechanics/SphOrb Orbit: RHSOrbit/FOrb SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/FOrbCart SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/Period SC: BasicOrbit/RV2El SC: BasicOrbit/RVFromKepler SC: Disturbances/AeroDragForce SC: Disturbances/AeroF Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2Array Common: Time/JD2T Common: Time/T2JD Math: Integration/RK4 Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Linear/Skew Math: Linear/Unit
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