Path: Orbit/LowEnergyManeuver
% Propagate the CRTBP equations of motion for arbitrary mu Finds the state when the trajectory hits the x-axis. Type PropagateCRTBPToXAxis for a demo -------------------------------------------------------------------------- Form: [tF, yF] = PropagateCRTBPToXAxis(y,t0,tol,mu); -------------------------------------------------------------------------- ------ Inputs ------ y (6,1) Current state vector [r;v] t0 (1,1) Initial time tol (1,1) Convergence tolerance mu (1,1) CRTBP mass ratio ------- Outputs ------- tF (1,1) Time at the intersection with the x-axis yF (6,1) State at the intersection with the x-axis --------------------------------------------------------------------------
Orbit: LowEnergyManeuver/PropagateCRTBP Orbit: LowEnergyManeuverData/f16pRef Common: Graphics/NewFig Math: Linear/Mag
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