Path: Orbit/LowEnergyManeuver
% Scales CRTBP Jacobi coordinates to km and sec Scales coordinates from Jacobi coordinates of the Circular Restricted Three Body Problem to units of kilometers and seconds -------------------------------------------------------------------------- Form: [stateOut,sec2tu] = CRTBP2kms(stateIn,distanceUnit,muPrimary,muSecondary); -------------------------------------------------------------------------- ------ Inputs ------ stateIn (6,1) Initial state vector distanceUnit (1,1) Distance between Primary and Secondary bodies (km) muPrimary (1,1) Gravitational Parameter of Primary body muSecondary (1,1) Gravitational Parameter of Secondary body ------- Outputs ------- stateOut (1,6) Output state vector sec2tu (1,1) Scaling factor for time --------------------------------------------------------------------------
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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