Package org.orekit.forces.gravity
Class SingleBodyRelativeAttraction
- java.lang.Object
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- org.orekit.forces.gravity.AbstractBodyAttraction
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- org.orekit.forces.gravity.SingleBodyRelativeAttraction
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- All Implemented Interfaces:
ForceModel
,EventDetectorsProvider
,ParameterDriversProvider
public class SingleBodyRelativeAttraction extends AbstractBodyAttraction
Body attraction force model computed as relative acceleration towards frame center.- Author:
- Luc Maisonabe, Julio Hernanz
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Field Summary
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Fields inherited from class org.orekit.forces.gravity.AbstractBodyAttraction
ATTRACTION_COEFFICIENT_SUFFIX
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Fields inherited from interface org.orekit.propagation.events.EventDetectorsProvider
DATATION_ACCURACY
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Constructor Summary
Constructors Constructor Description SingleBodyRelativeAttraction(CelestialBody body)
Simple 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.-
Methods inherited from class org.orekit.forces.gravity.AbstractBodyAttraction
dependsOnPositionOnly, getBody, getBodyName, getParametersDrivers
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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.propagation.events.EventDetectorsProvider
getEventDetectors, getFieldEventDetectors
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Methods inherited from interface org.orekit.forces.ForceModel
addContribution, addContribution, dependsOnAttitudeRate, getEventDetectors, getFieldEventDetectors, init, init
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Methods inherited from interface org.orekit.utils.ParameterDriversProvider
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
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Constructor Detail
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SingleBodyRelativeAttraction
public SingleBodyRelativeAttraction(CelestialBody body)
Simple constructor.- Parameters:
body
- the body to consider (ex:CelestialBodies.getSun()
orCelestialBodies.getMoon()
)
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Method Detail
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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 at state date, only 1 value for each parameterDriver- 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 at state date, only 1 value for each parameterDriver- Returns:
- acceleration in same frame as state
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