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.
|
Modifier and Type | Method | Description |
---|---|---|
protected abstract FieldStateMapper<T> |
FieldAbstractIntegratedPropagator.createMapper(FieldAbsoluteDate<T> referenceDate,
double mu,
OrbitType orbitType,
PositionAngle positionAngleType,
AttitudeProvider attitudeProvider,
Frame frame) |
Create a mapper between raw double components and spacecraft state.
|
Constructor | Description |
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FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate,
FieldAbsoluteDate<T> minDate,
FieldAbsoluteDate<T> maxDate,
FieldStateMapper<T> mapper,
boolean meanFieldOrbit,
FieldDenseOutputModel<T> model,
Map<String,T[]> unmanaged,
List<FieldAdditionalStateProvider<T>> providers,
String[] equations) |
Creates a new instance of IntegratedEphemeris.
|
Modifier and Type | Method | Description |
---|---|---|
protected FieldStateMapper<T> |
FieldNumericalPropagator.createMapper(FieldAbsoluteDate<T> referenceDate,
double mu,
OrbitType orbitType,
PositionAngle positionAngleType,
AttitudeProvider attitudeProvider,
Frame frame) |
Create a mapper between raw double components and spacecraft state.
|
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