org.orekit.forces.radiation

Class KnockeRediffusedForceModel

java.lang.Object

org.orekit.forces.radiation.KnockeRediffusedForceModel

All Implemented Interfaces:

ForceModel, EventDetectorsProvider, ParameterDriversProvider

public class KnockeRediffusedForceModel
extends Object
implements ForceModel

The Knocke Earth Albedo and IR emission force model.

This model is based on "EARTH RADIATION PRESSURE EFFECTS ON SATELLITES", 1988, by P. C. Knocke, J. C. Ries, and B. D. Tapley.

This model represents the effects of radiation pressure coming from the Earth. It considers Solar radiation which has been reflected by Earth (albedo) and Earth infrared emissions. The planet is considered as a sphere and is divided into elementary areas. Each elementary area is considered as a plane and emits radiation according to Lambert's law. The flux the satellite receives is then equal to the sum of the elementary fluxes coming from Earth.

The radiative model of the satellite, and its ability to diffuse, reflect or absorb radiation is handled by a radiation sensitive model.

Caution: This model is only suitable for Earth. Using it with another central body is prone to error..

Since:

10.3

Author:

Thomas Paulet

Field Summary

Fields inherited from interface org.orekit.propagation.events.EventDetectorsProvider

DATATION_ACCURACY

Constructor Summary

Constructors

Constructor and Description
KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider sun, RadiationSensitive spacecraft, double equatorialRadius, double angularResolution) Default Constructor.
KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider sun, RadiationSensitive spacecraft, double equatorialRadius, double angularResolution, TimeScale utc) General constructor.

Method Summary

Modifier and Type	Method and Description
<T extends org.hipparchus.CalculusFieldElement<T>> org.hipparchus.geometry.euclidean.threed.FieldVector3D<T>	acceleration(FieldSpacecraftState<T> s, T[] parameters) Compute acceleration.
org.hipparchus.geometry.euclidean.threed.Vector3D	acceleration(SpacecraftState s, double[] parameters) Compute acceleration.
boolean	dependsOnPositionOnly() Check if force models depends on position only.
List<ParameterDriver>	getParametersDrivers() Get the drivers for parameters.

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.forces.ForceModel

addContribution, addContribution, getEventDetectors, getFieldEventDetectors, init, init

Methods inherited from interface org.orekit.utils.ParameterDriversProvider

getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported

Methods inherited from interface org.orekit.propagation.events.EventDetectorsProvider

getEventDetectors, getFieldEventDetectors

Constructor Detail

KnockeRediffusedForceModel

@DefaultDataContext
public KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider sun,
                                                      RadiationSensitive spacecraft,
                                                      double equatorialRadius,
                                                      double angularResolution)

Default Constructor.

This constructor uses the default data context

.

Parameters:

sun - Sun model

spacecraft - the object physical and geometrical information

equatorialRadius - the Earth equatorial radius in m

angularResolution - angular resolution in rad

KnockeRediffusedForceModel

public KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider sun,
                                  RadiationSensitive spacecraft,
                                  double equatorialRadius,
                                  double angularResolution,
                                  TimeScale utc)

General constructor.

Parameters:

sun - Sun model

spacecraft - the object physical and geometrical information

equatorialRadius - the Earth equatorial radius in m

angularResolution - angular resolution in rad

utc - the UTC time scale to define reference epoch

Method Detail

dependsOnPositionOnly

public boolean dependsOnPositionOnly()

Check if force models depends on position only.

Specified by:

dependsOnPositionOnly in interface ForceModel

Returns:

true if force model depends on position only, false if it depends on velocity, either directly or due to a dependency on attitude

acceleration

public org.hipparchus.geometry.euclidean.threed.Vector3D acceleration(SpacecraftState s,
                                                                      double[] parameters)

Compute acceleration.

Specified by:

acceleration in interface ForceModel

Parameters:

s - current state information: date, kinematics, attitude

parameters - values of the force model parameters at state date, only 1 value for each parameterDriver

Returns:

acceleration in same frame as state

acceleration

public <T extends org.hipparchus.CalculusFieldElement<T>> org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> acceleration(FieldSpacecraftState<T> s,
                                                                                                                                 T[] parameters)

Compute acceleration.

Specified by:

acceleration in interface ForceModel

Type Parameters:

T - type of the elements

Parameters:

s - current state information: date, kinematics, attitude

parameters - values of the force model parameters at state date, only 1 value for each parameterDriver

Returns:

acceleration in same frame as state

getParametersDrivers

public List<ParameterDriver> getParametersDrivers()

Get the drivers for parameters.

Specified by:

getParametersDrivers in interface ParameterDriversProvider

Returns:

drivers for parameters