| Package | Description |
|---|---|
| org.orekit.propagation.integration | |
| org.orekit.propagation.numerical | |
| 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 StateMapper |
AbstractIntegratedPropagator.createMapper(AbsoluteDate referenceDate,
double mu,
OrbitType orbitType,
PositionAngle positionAngleType,
AttitudeProvider attitudeProvider,
Frame frame)
Create a mapper between raw double components and spacecraft state.
|
| Constructor and Description |
|---|
IntegratedEphemeris(AbsoluteDate startDate,
AbsoluteDate minDate,
AbsoluteDate maxDate,
StateMapper mapper,
boolean meanOrbit,
ContinuousOutputModel model,
Map<String,double[]> unmanaged,
List<AdditionalStateProvider> providers,
String[] equations)
Creates a new instance of IntegratedEphemeris.
|
| Modifier and Type | Method and Description |
|---|---|
protected StateMapper |
NumericalPropagator.createMapper(AbsoluteDate referenceDate,
double mu,
OrbitType orbitType,
PositionAngle positionAngleType,
AttitudeProvider attitudeProvider,
Frame frame)
Create a mapper between raw double components and spacecraft state.
|
| Modifier and Type | Method and Description |
|---|---|
protected StateMapper |
DSSTPropagator.createMapper(AbsoluteDate 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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