Package org.orekit.forces.radiation
Class PythonRadiationSensitive
- java.lang.Object
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- org.orekit.forces.radiation.PythonRadiationSensitive
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- All Implemented Interfaces:
RadiationSensitive
public class PythonRadiationSensitive extends Object implements RadiationSensitive
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Field Summary
Fields Modifier and Type Field Description protected long
pythonObject
Part of JCC Python interface to object-
Fields inherited from interface org.orekit.forces.radiation.RadiationSensitive
ABSORPTION_COEFFICIENT, GLOBAL_RADIATION_FACTOR, REFLECTION_COEFFICIENT
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Constructor Summary
Constructors Constructor Description PythonRadiationSensitive()
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description void
finalize()
List<ParameterDriver>
getRadiationParametersDrivers()
Get the drivers for supported parameters.void
pythonDecRef()
long
pythonExtension()
void
pythonExtension(long pythonObject)
<T extends CalculusFieldElement<T>>
FieldVector3D<T>radiationPressureAcceleration(FieldSpacecraftState<T> state, FieldVector3D<T> flux, T[] parameters)
Compute the acceleration due to radiation pressure.Vector3D
radiationPressureAcceleration(SpacecraftState state, Vector3D flux, double[] parameters)
Compute the acceleration due to radiation pressure.
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Method Detail
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pythonExtension
public void pythonExtension(long pythonObject)
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pythonExtension
public long pythonExtension()
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finalize
public void finalize() throws Throwable
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pythonDecRef
public void pythonDecRef()
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getRadiationParametersDrivers
public List<ParameterDriver> getRadiationParametersDrivers()
Get the drivers for supported parameters.- Specified by:
getRadiationParametersDrivers
in interfaceRadiationSensitive
- Returns:
- parameters drivers
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radiationPressureAcceleration
public Vector3D radiationPressureAcceleration(SpacecraftState state, Vector3D flux, double[] parameters)
Compute the acceleration due to radiation pressure.- Specified by:
radiationPressureAcceleration
in interfaceRadiationSensitive
- Parameters:
state
- current stateflux
- radiation flux in the same inertial frame as spacecraft orbitparameters
- values of the force model parameters- Returns:
- spacecraft acceleration in the same inertial frame as spacecraft orbit (m/s²)
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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 interfaceRadiationSensitive
- Type Parameters:
T
- extends CalculusFieldElement- Parameters:
state
- current stateflux
- radiation flux in the same inertial frame as spacecraft orbitparameters
- values of the force model parameters- Returns:
- spacecraft acceleration in the same inertial frame as spacecraft orbit (m/s²)
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