Package | Description |
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org.orekit.propagation |
Propagation
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org.orekit.propagation.integration |
Utilities for integration-based propagators (both numerical and semi-analytical).
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org.orekit.utils |
This package provides useful objects.
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Modifier and Type | Method and Description |
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FieldArrayDictionary<T> |
FieldSpacecraftState.getAdditionalStatesDerivatives()
Get an unmodifiable map of additional states derivatives.
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FieldArrayDictionary<T> |
FieldSpacecraftState.getAdditionalStatesValues()
Get an unmodifiable map of additional states.
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Constructor and Description |
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FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva,
FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit only.
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FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva,
FieldAttitude<T> attitude,
FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit and attitude.
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FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva,
FieldAttitude<T> attitude,
T mass,
FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit, attitude and mass.
|
FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva,
FieldAttitude<T> attitude,
T mass,
FieldArrayDictionary<T> additional,
FieldArrayDictionary<T> additionalDot)
Build a spacecraft state from orbit, attitude and mass.
|
FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva,
FieldAttitude<T> attitude,
T mass,
FieldArrayDictionary<T> additional,
FieldArrayDictionary<T> additionalDot)
Build a spacecraft state from orbit, attitude and mass.
|
FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva,
T mass,
FieldArrayDictionary<T> additional)
Create a new instance from orbit and mass.
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FieldSpacecraftState(FieldOrbit<T> orbit,
FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit and additional states.
|
FieldSpacecraftState(FieldOrbit<T> orbit,
FieldAttitude<T> attitude,
FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit attitude and additional states.
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FieldSpacecraftState(FieldOrbit<T> orbit,
FieldAttitude<T> attitude,
T mass,
FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit, attitude, mass and additional states.
|
FieldSpacecraftState(FieldOrbit<T> orbit,
FieldAttitude<T> attitude,
T mass,
FieldArrayDictionary<T> additional,
FieldArrayDictionary<T> additionalDot)
Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
|
FieldSpacecraftState(FieldOrbit<T> orbit,
FieldAttitude<T> attitude,
T mass,
FieldArrayDictionary<T> additional,
FieldArrayDictionary<T> additionalDot)
Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
|
FieldSpacecraftState(FieldOrbit<T> orbit,
T mass,
FieldArrayDictionary<T> additional)
Create a new instance from orbit, mass and additional states.
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Constructor and Description |
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FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate,
FieldAbsoluteDate<T> minDate,
FieldAbsoluteDate<T> maxDate,
FieldStateMapper<T> mapper,
PropagationType type,
FieldDenseOutputModel<T> model,
FieldArrayDictionary<T> unmanaged,
List<FieldAdditionalStateProvider<T>> providers,
String[] equations)
|
FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate,
FieldAbsoluteDate<T> minDate,
FieldAbsoluteDate<T> maxDate,
FieldStateMapper<T> mapper,
PropagationType type,
FieldDenseOutputModel<T> model,
FieldArrayDictionary<T> unmanaged,
List<FieldAdditionalStateProvider<T>> providers,
String[] equations,
int[] dimensions)
Creates a new instance of IntegratedEphemeris.
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Modifier and Type | Method and Description |
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FieldArrayDictionary<T> |
FieldArrayDictionary.unmodifiableView()
Get an unmodifiable view of the dictionary.
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Modifier and Type | Method and Description |
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void |
FieldArrayDictionary.putAll(FieldArrayDictionary<T> dictionary)
Put all the entries from another dictionary.
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Constructor and Description |
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FieldArrayDictionary(FieldArrayDictionary<T> dictionary)
Constructor from another dictionary.
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