Package org.orekit.forces.radiation
Interface RadiationSensitive
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- All Known Implementing Classes:
BoxAndSolarArraySpacecraft
,IsotropicRadiationClassicalConvention
,IsotropicRadiationCNES95Convention
,IsotropicRadiationSingleCoefficient
,PythonRadiationSensitive
public interface RadiationSensitive
Interface for spacecraft that are sensitive to radiation pressure forces.- Author:
- Luc Maisonobe, Pascal Parraud
- See Also:
SolarRadiationPressure
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Field Summary
Fields Modifier and Type Field Description static String
ABSORPTION_COEFFICIENT
Parameter name for absorption coefficient.static String
REFLECTION_COEFFICIENT
Parameter name for reflection coefficient.
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Method Summary
All Methods Instance Methods Abstract Methods Modifier and Type Method Description List<ParameterDriver>
getRadiationParametersDrivers()
Get the drivers for supported parameters.Vector3D
radiationPressureAcceleration(AbsoluteDate date, Frame frame, Vector3D position, Rotation rotation, double mass, Vector3D flux, double[] parameters)
Compute the acceleration due to radiation pressure.<T extends CalculusFieldElement<T>>
FieldVector3D<T>radiationPressureAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, FieldVector3D<T> flux, T[] parameters)
Compute the acceleration due to radiation pressure.
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Field Detail
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ABSORPTION_COEFFICIENT
static final String ABSORPTION_COEFFICIENT
Parameter name for absorption coefficient.- See Also:
- Constant Field Values
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REFLECTION_COEFFICIENT
static final String REFLECTION_COEFFICIENT
Parameter name for reflection coefficient.- See Also:
- Constant Field Values
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Method Detail
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getRadiationParametersDrivers
List<ParameterDriver> getRadiationParametersDrivers()
Get the drivers for supported parameters.- Returns:
- parameters drivers
- Since:
- 8.0
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radiationPressureAcceleration
Vector3D radiationPressureAcceleration(AbsoluteDate date, Frame frame, Vector3D position, Rotation rotation, double mass, Vector3D flux, double[] parameters)
Compute the acceleration due to radiation pressure.- Parameters:
date
- current dateframe
- inertial reference frame for state (both orbit and attitude)position
- position of spacecraft in reference framerotation
- orientation (attitude) of the spacecraft with respect to reference framemass
- current massflux
- 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
<T extends CalculusFieldElement<T>> FieldVector3D<T> radiationPressureAcceleration(FieldAbsoluteDate<T> date, Frame frame, FieldVector3D<T> position, FieldRotation<T> rotation, T mass, FieldVector3D<T> flux, T[] parameters)
Compute the acceleration due to radiation pressure.- Type Parameters:
T
- extends CalculusFieldElement- Parameters:
date
- current dateframe
- inertial reference frame for state (both orbit and attitude)position
- position of spacecraft in reference framerotation
- orientation (attitude) of the spacecraft with respect to reference framemass
- current massflux
- 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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