Class FieldAbstractPropagator<T extends CalculusFieldElement<T>>
- java.lang.Object
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- org.orekit.propagation.FieldAbstractPropagator<T>
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- Type Parameters:
T
- the type of the field elements
- All Implemented Interfaces:
FieldPropagator<T>
,FieldPVCoordinatesProvider<T>
- Direct Known Subclasses:
FieldAbstractAnalyticalPropagator
,FieldAbstractIntegratedPropagator
public abstract class FieldAbstractPropagator<T extends CalculusFieldElement<T>> extends Object implements FieldPropagator<T>
Common handling ofPropagator
methods for analytical propagators.This abstract class allows to provide easily the full set of
Propagator
methods, including all propagation modes support and discrete events support for any simple propagation method.- Author:
- Luc Maisonobe
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Field Summary
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Fields inherited from interface org.orekit.propagation.FieldPropagator
DEFAULT_MASS
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Constructor Summary
Constructors Modifier Constructor Description protected
FieldAbstractPropagator(Field<T> field)
Build a new instance.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description void
addAdditionalDataProvider(FieldAdditionalDataProvider<?,T> additionalDataProvider)
Add a set of user-specified data to be computed along with the orbit propagation.List<FieldAdditionalDataProvider<?,T>>
getAdditionalDataProviders()
Get an unmodifiable list of providers for additional data.AttitudeProvider
getAttitudeProvider()
Get attitude provider.Field<T>
getField()
Field getter.Frame
getFrame()
Get the frame in which the orbit is propagated.FieldSpacecraftState<T>
getInitialState()
Get the propagator initial state.String[]
getManagedAdditionalData()
Get all the names of all managed data.FieldStepHandlerMultiplexer<T>
getMultiplexer()
Get the multiplexer holding all step handlers.protected FieldAbsoluteDate<T>
getStartDate()
Get the start date.protected void
initializeAdditionalData(FieldAbsoluteDate<T> target)
Initialize the additional data providers at the start of propagation.protected void
initializePropagation()
Initialize propagation.boolean
isAdditionalDataManaged(String name)
Check if an additional data is managed.FieldSpacecraftState<T>
propagate(FieldAbsoluteDate<T> target)
Propagate towards a target date.void
resetInitialState(FieldSpacecraftState<T> state)
Reset the propagator initial state.void
setAttitudeProvider(AttitudeProvider attitudeProvider)
Set attitude provider.protected void
setStartDate(FieldAbsoluteDate<T> startDate)
Set a start date.protected void
stateChanged(FieldSpacecraftState<T> state)
Notify about a state change.FieldSpacecraftState<T>
updateAdditionalData(FieldSpacecraftState<T> original)
Update state by adding all additional data.protected FieldSpacecraftState<T>
updateUnmanagedData(FieldSpacecraftState<T> original)
Update state by adding unmanaged states.-
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.FieldPropagator
addEventDetector, clearEventsDetectors, clearStepHandlers, getEphemerisGenerator, getEventDetectors, getPosition, getPVCoordinates, propagate, setStepHandler, setStepHandler
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Method Detail
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setStartDate
protected void setStartDate(FieldAbsoluteDate<T> startDate)
Set a start date.- Parameters:
startDate
- start date
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getStartDate
protected FieldAbsoluteDate<T> getStartDate()
Get the start date.- Returns:
- start date
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getAttitudeProvider
public AttitudeProvider getAttitudeProvider()
Get attitude provider.- Specified by:
getAttitudeProvider
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Returns:
- attitude provider
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setAttitudeProvider
public void setAttitudeProvider(AttitudeProvider attitudeProvider)
Set attitude provider.- Specified by:
setAttitudeProvider
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Parameters:
attitudeProvider
- attitude provider
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getInitialState
public FieldSpacecraftState<T> getInitialState()
Get the propagator initial state.- Specified by:
getInitialState
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Returns:
- initial state
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getFrame
public Frame getFrame()
Get the frame in which the orbit is propagated.The propagation frame is the definition frame of the initial state, so this method should be called after this state has been set, otherwise it may return null.
- Specified by:
getFrame
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Returns:
- frame in which the orbit is propagated
- See Also:
FieldPropagator.resetInitialState(FieldSpacecraftState)
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resetInitialState
public void resetInitialState(FieldSpacecraftState<T> state)
Reset the propagator initial state.- Specified by:
resetInitialState
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Parameters:
state
- new initial state to consider
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getMultiplexer
public FieldStepHandlerMultiplexer<T> getMultiplexer()
Get the multiplexer holding all step handlers.- Specified by:
getMultiplexer
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Returns:
- multiplexer holding all step handlers
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addAdditionalDataProvider
public void addAdditionalDataProvider(FieldAdditionalDataProvider<?,T> additionalDataProvider)
Add a set of user-specified data to be computed along with the orbit propagation.- Specified by:
addAdditionalDataProvider
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Parameters:
additionalDataProvider
- provider for additional data
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getAdditionalDataProviders
public List<FieldAdditionalDataProvider<?,T>> getAdditionalDataProviders()
Get an unmodifiable list of providers for additional data.- Specified by:
getAdditionalDataProviders
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Returns:
- providers for the additional states
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updateUnmanagedData
protected FieldSpacecraftState<T> updateUnmanagedData(FieldSpacecraftState<T> original)
Update state by adding unmanaged states.- Parameters:
original
- original state- Returns:
- updated state, with unmanaged states included
- See Also:
updateAdditionalData(FieldSpacecraftState)
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updateAdditionalData
public FieldSpacecraftState<T> updateAdditionalData(FieldSpacecraftState<T> original)
Update state by adding all additional data.- Parameters:
original
- original state- Returns:
- updated state, with all additional data included
- See Also:
addAdditionalDataProvider(FieldAdditionalDataProvider)
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initializeAdditionalData
protected void initializeAdditionalData(FieldAbsoluteDate<T> target)
Initialize the additional data providers at the start of propagation.- Parameters:
target
- date of propagation. Not equal toinitialState.getDate()
.- Since:
- 11.2
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isAdditionalDataManaged
public boolean isAdditionalDataManaged(String name)
Check if an additional data is managed.Managed data are the ones for which the propagators know how to compute its evolution. They correspond to additional data for which an
additional data provider
has been registered by calling theaddAdditionalDataProvider
method. If the propagator is anintegrator-based propagator
, the states for which a set ofadditional derivatives provider
has been registered by calling theaddAdditionalDerivativesProvider
method are also counted as managed additional states.Additional data that are present in the
initial state
but have no evolution method registered are not considered as managed data. These unmanaged additional data are not lost during propagation, though. Their value are piecewise constant between state resets that may change them if some event handlerresetState
method is called at an event occurrence and happens to change the unmanaged additional data.- Specified by:
isAdditionalDataManaged
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Parameters:
name
- name of the additional data- Returns:
- true if the additional data is managed
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getManagedAdditionalData
public String[] getManagedAdditionalData()
Get all the names of all managed data.- Specified by:
getManagedAdditionalData
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Returns:
- names of all managed data
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propagate
public FieldSpacecraftState<T> propagate(FieldAbsoluteDate<T> target)
Propagate towards a target date.Simple propagators use only the target date as the specification for computing the propagated state. More feature rich propagators can consider other information and provide different operating modes or G-stop facilities to stop at pinpointed events occurrences. In these cases, the target date is only a hint, not a mandatory objective.
- Specified by:
propagate
in interfaceFieldPropagator<T extends CalculusFieldElement<T>>
- Parameters:
target
- target date towards which orbit state should be propagated- Returns:
- propagated state
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initializePropagation
protected void initializePropagation()
Initialize propagation.- Since:
- 10.1
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stateChanged
protected void stateChanged(FieldSpacecraftState<T> state)
Notify about a state change.- Parameters:
state
- new state
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