public class TLEPropagatorBuilder extends AbstractPropagatorBuilder
Modifier and Type | Field and Description |
---|---|
static String |
B_STAR
Parameter name for B* coefficient.
|
Constructor and Description |
---|
TLEPropagatorBuilder(TLE templateTLE,
PositionAngle positionAngle,
double positionScale)
Build a new instance.
|
Modifier and Type | Method and Description |
---|---|
Propagator |
buildPropagator(double[] normalizedParameters)
Build a propagator.
|
addSupportedParameter, createInitialOrbit, getFrame, getInitialOrbitDate, getOrbitalParametersDrivers, getOrbitType, getPositionAngle, getPropagationParametersDrivers, getSelectedNormalizedParameters, setParameters
public static final String B_STAR
public TLEPropagatorBuilder(TLE templateTLE, PositionAngle positionAngle, double positionScale) throws OrekitException
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)OrekitException
- if the TEME frame cannot be setpublic Propagator buildPropagator(double[] normalizedParameters) throws OrekitException
normalizedParameters
- normalized values for the selected parametersOrekitException
- if propagator cannot be buildCopyright © 2002-2017 CS Systèmes d'information. All rights reserved.