Package | Description |
---|---|
org.orekit.propagation.integration |
Utilities for integration-based propagators (both numerical and semi-analytical).
|
org.orekit.propagation.numerical |
Top level package for numerical propagators.
|
org.orekit.propagation.semianalytical.dsst |
This package provides an implementation of the Draper Semi-analytical
Satellite Theory (DSST).
|
Modifier and Type | Method and Description |
---|---|
protected abstract FieldStateMapper<T> |
FieldAbstractIntegratedPropagator.createMapper(FieldAbsoluteDate<T> referenceDate,
T mu,
OrbitType orbitType,
PositionAngleType positionAngleType,
AttitudeProvider attitudeProvider,
Frame frame)
Create a mapper between raw double components and spacecraft state.
|
Constructor and Description |
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FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate,
FieldAbsoluteDate<T> minDate,
FieldAbsoluteDate<T> maxDate,
FieldStateMapper<T> mapper,
PropagationType type,
org.hipparchus.ode.FieldDenseOutputModel<T> model,
FieldArrayDictionary<T> unmanaged,
List<FieldAdditionalStateProvider<T>> providers,
String[] equations,
int[] dimensions)
Creates a new instance of IntegratedEphemeris.
|
Modifier and Type | Method and Description |
---|---|
protected FieldStateMapper<T> |
FieldNumericalPropagator.createMapper(FieldAbsoluteDate<T> referenceDate,
T mu,
OrbitType orbitType,
PositionAngleType positionAngleType,
AttitudeProvider attitudeProvider,
Frame frame)
Create a mapper between raw double components and spacecraft state.
|
Modifier and Type | Method and Description |
---|---|
protected FieldStateMapper<T> |
FieldDSSTPropagator.createMapper(FieldAbsoluteDate<T> referenceDate,
T mu,
OrbitType ignoredOrbitType,
PositionAngleType ignoredPositionAngleType,
AttitudeProvider attitudeProvider,
Frame frame)
Create a mapper between raw double components and spacecraft state.
|
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