Path: Orbit/LowEnergyManeuver
% Calculate from Jacobi constant from a scaled state vector The default three-body problem is the Earth, Moon, and sun. Type CRTBPJacobiConstant for a demo with two identical vectors. -------------------------------------------------------------------------- Form: j = CRTBPJacobiConstant(y,mu) -------------------------------------------------------------------------- ------ Inputs ------ y (6,n) State vector in scaled coordinates [r;v] mu (1,1) CRTBP mass parameter ------- Outputs ------- j (n,1) Jacobi constant --------------------------------------------------------------------------
AC: ACData/ACTConstants Orbit: LowEnergyManeuverData/f16Ref SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/xSplashSmall Common: Database/Constant Common: General/DeleteCell
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