PropagatorBuilder
public class NumericalPropagatorBuilder extends AbstractPropagatorBuilder
Constructor | Description |
---|---|
NumericalPropagatorBuilder(Orbit referenceOrbit,
ODEIntegratorBuilder builder,
PositionAngle positionAngle,
double positionScale) |
Build a new instance.
|
Modifier and Type | Method | Description |
---|---|---|
void |
addForceModel(ForceModel model) |
Add a force model to the global perturbation model.
|
NumericalPropagator |
buildPropagator(double[] normalizedParameters) |
Build a propagator.
|
NumericalPropagatorBuilder |
copy() |
Create a copy of a NumericalPropagatorBuilder object.
|
List<ForceModel> |
getAllForceModels() |
Get the list of all force models.
|
AttitudeProvider |
getAttitudeProvider() |
Get the attitudeProvider.
|
ODEIntegratorBuilder |
getIntegratorBuilder() |
Get the integrator builder.
|
double |
getMass() |
Get the mass.
|
void |
setAttitudeProvider(AttitudeProvider attitudeProvider) |
Set the attitude provider.
|
void |
setMass(double mass) |
Set the initial mass.
|
addSupportedParameter, createInitialOrbit, getFrame, getInitialOrbitDate, getMu, getOrbitalParametersDrivers, getOrbitType, getPositionAngle, getPositionScale, getPropagationParametersDrivers, getSelectedNormalizedParameters, resetOrbit, setParameters
public NumericalPropagatorBuilder(Orbit referenceOrbit, ODEIntegratorBuilder builder, PositionAngle positionAngle, double positionScale)
The reference orbit is used as a model to create initial orbit
. It defines the
inertial frame, the central attraction coefficient, and is also used together
with the positionScale
to convert from the normalized
parameters used by the
callers of this builder to the real orbital parameters.
referenceOrbit
- reference orbit from which real orbits will be builtbuilder
- first order integrator builderpositionAngle
- position angle type to usepositionScale
- scaling factor used for orbital parameters normalization
(typically set to the expected standard deviation of the position)public NumericalPropagatorBuilder copy()
public ODEIntegratorBuilder getIntegratorBuilder()
public List<ForceModel> getAllForceModels()
public void addForceModel(ForceModel model)
If this method is not called at all, the integrated orbit will follow a Keplerian evolution only.
model
- perturbing ForceModel
to addpublic double getMass()
public void setMass(double mass)
mass
- the mass (kg)public AttitudeProvider getAttitudeProvider()
public void setAttitudeProvider(AttitudeProvider attitudeProvider)
attitudeProvider
- attitude providerpublic NumericalPropagator buildPropagator(double[] normalizedParameters)
normalizedParameters
- normalized values for the selected parametersCopyright © 2002-2019 CS Systèmes d'information. All rights reserved.