Package org.orekit.propagation.conversion

Class TLEPropagatorBuilder

java.lang.Object

org.orekit.propagation.conversion.AbstractPropagatorBuilder

org.orekit.propagation.conversion.TLEPropagatorBuilder

All Implemented Interfaces:

PropagatorBuilder

public class TLEPropagatorBuilder
extends AbstractPropagatorBuilder

Builder for TLEPropagator.

Since:

6.0

Author:

Pascal Parraud

Field Summary

Fields

Modifier and Type	Field	Description
static String	B_STAR	Parameter name for B* coefficient.

Constructor Summary

Constructors

Constructor	Description
TLEPropagatorBuilder(TLE templateTLE, PositionAngle positionAngle, double positionScale)	Build a new instance.

Method Summary

Modifier and Type	Method	Description
Propagator	buildPropagator(double[] normalizedParameters)	Build a propagator.

Methods inherited from class org.orekit.propagation.conversion.AbstractPropagatorBuilder

addSupportedParameter, createInitialOrbit, getFrame, getInitialOrbitDate, getMu, getOrbitalParametersDrivers, getOrbitType, getPositionAngle, getPositionScale, getPropagationParametersDrivers, getSelectedNormalizedParameters, resetOrbit, setParameters

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Field Detail

B_STAR

public static final String B_STAR

Parameter name for B* coefficient.

See Also:

Constant Field Values

Constructor Detail

TLEPropagatorBuilder

public TLEPropagatorBuilder(TLE templateTLE,
                            PositionAngle positionAngle,
                            double positionScale)
                     throws OrekitException

Build a new instance.

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.

Parameters:

templateTLE - reference TLE from which real orbits will be built

positionAngle - position angle type to use

positionScale - scaling factor used for orbital parameters normalization (typically set to the expected standard deviation of the position)

Throws:

OrekitException - if the TEME frame cannot be set

Since:

7.1

Method Detail

buildPropagator

public Propagator buildPropagator(double[] normalizedParameters)
                           throws OrekitException

Build a propagator.

Parameters:

normalizedParameters - normalized values for the selected parameters

Returns:

an initialized propagator

Throws:

OrekitException - if propagator cannot be build