Class PythonFieldStateMapper<T extends CalculusFieldElement<T>>
- java.lang.Object
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- org.orekit.propagation.integration.FieldStateMapper<T>
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- org.orekit.propagation.integration.PythonFieldStateMapper<T>
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public class PythonFieldStateMapper<T extends CalculusFieldElement<T>> extends FieldStateMapper<T>
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Constructor Summary
Constructors Constructor Description PythonFieldStateMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)
Simple constructor.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description void
finalize()
Part of JCC Python interface to objectFieldSpacecraftState<T>
mapArrayToState(FieldAbsoluteDate<T> date, T[] y, T[] yDot, PropagationType type)
Map the raw double components to a spacecraft state.void
mapStateToArray(FieldSpacecraftState<T> state, T[] y, T[] yDot)
Map a spacecraft state to raw double components.void
pythonDecRef()
Part of JCC Python interface to objectlong
pythonExtension()
Part of JCC Python interface to objectvoid
pythonExtension(long pythonObject)
Part of JCC Python interface to object-
Methods inherited from class org.orekit.propagation.integration.FieldStateMapper
getAttitudeProvider, getFrame, getMu, getOrbitType, getPositionAngleType, getReferenceDate, mapArrayToState, mapDateToDouble, mapDoubleToDate, mapDoubleToDate, setPositionAngleType
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Constructor Detail
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PythonFieldStateMapper
public PythonFieldStateMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)
Simple constructor.The position parameter type is meaningful only if
propagation orbit type
support it. As an example, it is not meaningful for propagation inCartesian
parameters.- Parameters:
referenceDate
- reference datemu
- central attraction coefficient (m³/s²)orbitType
- orbit type to use for mappingpositionAngleType
- angle type to use for propagationattitudeProvider
- attitude providerframe
- inertial frame
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Method Detail
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pythonExtension
public void pythonExtension(long pythonObject)
Part of JCC Python interface to object
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pythonExtension
public long pythonExtension()
Part of JCC Python interface to object
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finalize
public void finalize() throws Throwable
Part of JCC Python interface to object
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pythonDecRef
public void pythonDecRef()
Part of JCC Python interface to object
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mapArrayToState
public FieldSpacecraftState<T> mapArrayToState(FieldAbsoluteDate<T> date, T[] y, T[] yDot, PropagationType type)
Map the raw double components to a spacecraft state.- Specified by:
mapArrayToState
in classFieldStateMapper<T extends CalculusFieldElement<T>>
- Parameters:
date
- of the state componentsy
- state componentsyDot
- state derivative componentstype
- type of the elements used to build the state (mean or osculating).- Returns:
- spacecraft state
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mapStateToArray
public void mapStateToArray(FieldSpacecraftState<T> state, T[] y, T[] yDot)
Map a spacecraft state to raw double components.- Specified by:
mapStateToArray
in classFieldStateMapper<T extends CalculusFieldElement<T>>
- Parameters:
state
- state to mapy
- placeholder where to put the componentsyDot
- placeholder where to put the components derivatives
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