PropagatorBuilder
public class TLEPropagatorBuilder extends AbstractPropagatorBuilder
Modifier and Type | Field | Description |
---|---|---|
static String |
B_STAR |
Parameter name for B* coefficient.
|
Constructor | Description |
---|---|
TLEPropagatorBuilder(TLE templateTLE,
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 static final String B_STAR
public TLEPropagatorBuilder(TLE templateTLE, PositionAngle positionAngle, double positionScale)
The template TLE is used as a model to create initial orbit
. It defines the
inertial frame, the central attraction coefficient, orbit type, satellite number,
classification, .... 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.
templateTLE
- reference TLE 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.