Class IsotropicRadiationSingleCoefficient

    • Constructor Detail

      • IsotropicRadiationSingleCoefficient

        public IsotropicRadiationSingleCoefficient​(double crossSection,
                                                   double cr)
        Constructor with reflection coefficient min/max set to ±∞.
        Parameters:
        crossSection - Surface (m²)
        cr - reflection coefficient
      • IsotropicRadiationSingleCoefficient

        public IsotropicRadiationSingleCoefficient​(double crossSection,
                                                   double cr,
                                                   double crMin,
                                                   double crMax)
        Constructor with reflection coefficient min/max set by user.
        Parameters:
        crossSection - Surface (m²)
        cr - reflection coefficient
        crMin - Minimum value of reflection coefficient
        crMax - Maximum value of reflection coefficient
    • Method Detail

      • radiationPressureAcceleration

        public Vector3D radiationPressureAcceleration​(SpacecraftState state,
                                                      Vector3D flux,
                                                      double[] parameters)
        Compute the acceleration due to radiation pressure.
        Specified by:
        radiationPressureAcceleration in interface RadiationSensitive
        Parameters:
        state - current state
        flux - radiation flux in the same inertial frame as spacecraft orbit
        parameters - values of the force model parameters
        Returns:
        spacecraft acceleration in the same inertial frame as spacecraft orbit (m/s²)
      • radiationPressureAcceleration

        public <T extends CalculusFieldElement<T>> FieldVector3D<T> radiationPressureAcceleration​(FieldSpacecraftState<T> state,
                                                                                                  FieldVector3D<T> flux,
                                                                                                  T[] parameters)
        Compute the acceleration due to radiation pressure.
        Specified by:
        radiationPressureAcceleration in interface RadiationSensitive
        Type Parameters:
        T - extends CalculusFieldElement
        Parameters:
        state - current state
        flux - radiation flux in the same inertial frame as spacecraft orbit
        parameters - values of the force model parameters
        Returns:
        spacecraft acceleration in the same inertial frame as spacecraft orbit (m/s²)