Package org.orekit.forces.gravity
Class LenseThirringRelativity
- java.lang.Object
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- org.orekit.forces.AbstractForceModel
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- org.orekit.forces.gravity.LenseThirringRelativity
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- All Implemented Interfaces:
ForceModel
,ParametersDriversProvider
public class LenseThirringRelativity extends AbstractForceModel
Lense-Thirring post-Newtonian correction force due to general relativity.Lense-Thirring term causes a precession of the orbital plane at a rate of the order of 0.8 mas per year (geostationary) to 180 mas per year (low orbit).
- Since:
- 10.3
- Author:
- Bryan Cazabonne
- See Also:
- "Petit, G. and Luzum, B. (eds.), IERS Conventions (2010), Chapter 10, General relativistic models for space-time coordinates and equations of motion (2010)"
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Constructor Summary
Constructors Constructor Description LenseThirringRelativity(double gm, Frame bodyFrame)
Constructor.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description <T extends CalculusFieldElement<T>>
FieldVector3D<T>acceleration(FieldSpacecraftState<T> s, T[] parameters)
Compute acceleration.Vector3D
acceleration(SpacecraftState s, double[] parameters)
Compute acceleration.boolean
dependsOnPositionOnly()
Check if force models depends on position only.Stream<EventDetector>
getEventsDetectors()
Get the discrete events related to the model.<T extends CalculusFieldElement<T>>
Stream<FieldEventDetector<T>>getFieldEventsDetectors(Field<T> field)
Get the discrete events related to the model.List<ParameterDriver>
getParametersDrivers()
Get the drivers for parameters.-
Methods inherited from class org.orekit.forces.AbstractForceModel
complainIfNotSupported, getParameterDriver, isSupported
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Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
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Methods inherited from interface org.orekit.forces.ForceModel
addContribution, addContribution, getParameters, getParameters, init, init
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Constructor Detail
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LenseThirringRelativity
public LenseThirringRelativity(double gm, Frame bodyFrame)
Constructor.- Parameters:
gm
- Earth's gravitational parameter.bodyFrame
- central body frame
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Method Detail
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dependsOnPositionOnly
public boolean dependsOnPositionOnly()
Check if force models depends on position only.- Returns:
- true if force model depends on position only, false if it depends on velocity, either directly or due to a dependency on attitude
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acceleration
public Vector3D acceleration(SpacecraftState s, double[] parameters)
Compute acceleration.- Parameters:
s
- current state information: date, kinematics, attitudeparameters
- values of the force model parameters- Returns:
- acceleration in same frame as state
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acceleration
public <T extends CalculusFieldElement<T>> FieldVector3D<T> acceleration(FieldSpacecraftState<T> s, T[] parameters)
Compute acceleration.- Type Parameters:
T
- type of the elements- Parameters:
s
- current state information: date, kinematics, attitudeparameters
- values of the force model parameters- Returns:
- acceleration in same frame as state
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getEventsDetectors
public Stream<EventDetector> getEventsDetectors()
Get the discrete events related to the model.- Returns:
- stream of events detectors
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getFieldEventsDetectors
public <T extends CalculusFieldElement<T>> Stream<FieldEventDetector<T>> getFieldEventsDetectors(Field<T> field)
Get the discrete events related to the model.- Type Parameters:
T
- extends CalculusFieldElement<T>- Parameters:
field
- field to which the state belongs- Returns:
- stream of events detectors
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getParametersDrivers
public List<ParameterDriver> getParametersDrivers()
Get the drivers for parameters.- Returns:
- drivers for parameters
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