Path: Orbit/LowEnergyManeuver
-------------------------------------------------------------------------- Propagate an arbitrary CRTBP with origin at the secondary body backwards -------------------------------------------------------------------------- Form: [yvec, tvec] = PropagateCRTBPBackwards(y,t0,tF,mu); -------------------------------------------------------------------------- ------ Inputs ------ y (6,1) Current state vector [r;v] t0 (1,1) Initial time tF (1,1) Final time (positive) mu (1,1) CRTBP mass parameter ------- Outputs ------- yvec (6,:) State vector tvec (1,:) Time vector --------------------------------------------------------------------------
Orbit: LowEnergyManeuverData/f16pRef Common: Database/Constant Common: Graphics/Plot2D Common: Graphics/TimeLabl
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