PropagatorBuilder
public class KeplerianPropagatorBuilder extends AbstractPropagatorBuilder
Constructor | Description |
---|---|
KeplerianPropagatorBuilder(Orbit templateOrbit,
PositionAngle positionAngle,
double positionScale) |
Build a new instance.
|
Modifier and Type | Method | Description |
---|---|---|
Propagator |
buildPropagator(double[] normalizedParameters) |
Build a propagator.
|
addSupportedParameter, createInitialOrbit, getFrame, getInitialOrbitDate, getMu, getOrbitalParametersDrivers, getOrbitType, getPositionAngle, getPositionScale, getPropagationParametersDrivers, getSelectedNormalizedParameters, resetOrbit, setParameters
public KeplerianPropagatorBuilder(Orbit templateOrbit, PositionAngle positionAngle, double positionScale)
The template orbit is used as a model to create initial orbit
. It defines the
inertial frame, the central attraction coefficient, the orbit type, 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.
templateOrbit
- reference orbit from which real orbits will be builtpositionAngle
- position angle type to usepositionScale
- scaling factor used for orbital parameters normalization
(typically set to the expected standard deviation of the position)public Propagator buildPropagator(double[] normalizedParameters)
normalizedParameters
- normalized values for the selected parametersCopyright © 2002-2019 CS Systèmes d'information. All rights reserved.