Interface RadiationSensitive

    • Field Detail

      • GLOBAL_RADIATION_FACTOR

        static final String GLOBAL_RADIATION_FACTOR
        Parameter name for global multiplicative factor.
        Since:
        12.0
        See Also:
        Constant Field Values
      • ABSORPTION_COEFFICIENT

        static final String ABSORPTION_COEFFICIENT
        Parameter name for absorption coefficient.
        See Also:
        Constant Field Values
      • REFLECTION_COEFFICIENT

        static final String REFLECTION_COEFFICIENT
        Parameter name for reflection coefficient.
        See Also:
        Constant Field Values
    • Method Detail

      • getRadiationParametersDrivers

        List<ParameterDriver> getRadiationParametersDrivers()
        Get the drivers for supported parameters.
        Returns:
        parameters drivers
        Since:
        8.0
      • radiationPressureAcceleration

        Vector3D radiationPressureAcceleration​(SpacecraftState state,
                                               Vector3D flux,
                                               double[] parameters)
        Compute the acceleration due to radiation pressure.
        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)
        Since:
        12.0
      • radiationPressureAcceleration

        <T extends CalculusFieldElement<T>> FieldVector3D<T> radiationPressureAcceleration​(FieldSpacecraftState<T> state,
                                                                                           FieldVector3D<T> flux,
                                                                                           T[] parameters)
        Compute the acceleration due to radiation pressure.
        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)
        Since:
        12.0