Package | Description |
---|---|
org.orekit.orbits |
This package provides classes to represent orbits.
|
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 |
---|---|
abstract OrbitType |
Orbit.getType()
Get the orbit type.
|
OrbitType |
CircularOrbit.getType()
Get the orbit type.
|
OrbitType |
EquinoctialOrbit.getType()
Get the orbit type.
|
OrbitType |
KeplerianOrbit.getType()
Get the orbit type.
|
OrbitType |
CartesianOrbit.getType()
Get the orbit type.
|
static OrbitType |
OrbitType.valueOf(String name)
Returns the enum constant of this type with the specified name.
|
static OrbitType[] |
OrbitType.values()
Returns an array containing the constants of this enum type, in
the order they are declared.
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Modifier and Type | Method and Description |
---|---|
protected OrbitType |
AbstractIntegratedPropagator.getOrbitType()
Get propagation parameter type.
|
OrbitType |
StateMapper.getOrbitType()
Get propagation parameter type.
|
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.
|
protected void |
AbstractIntegratedPropagator.setOrbitType(OrbitType orbitType)
Set propagation orbit type.
|
Constructor and Description |
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StateMapper(AbsoluteDate referenceDate,
double mu,
OrbitType orbitType,
PositionAngle positionAngleType,
AttitudeProvider attitudeProvider,
Frame frame)
Simple constructor.
|
Modifier and Type | Method and Description |
---|---|
OrbitType |
NumericalPropagator.getOrbitType()
Get propagation parameter type.
|
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.
|
void |
NumericalPropagator.setOrbitType(OrbitType orbitType)
Set propagation orbit type.
|
static double[][] |
NumericalPropagator.tolerances(double dP,
Orbit orbit,
OrbitType type)
Estimate tolerance vectors for integrators.
|
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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