public static class QZSSPropagator.Builder extends Object
It implements the classical builder pattern.
Constructor and Description |
---|
Builder(QZSSOrbitalElements qzssOrbElt)
Initializes the builder.
|
Modifier and Type | Method and Description |
---|---|
QZSSPropagator.Builder |
attitudeProvider(AttitudeProvider userProvider)
Sets the attitude provider.
|
QZSSPropagator |
build()
Finalizes the build.
|
QZSSPropagator.Builder |
ecef(Frame bodyFixed)
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
|
QZSSPropagator.Builder |
eci(Frame inertial)
Sets the Earth Centered Inertial frame used for propagation.
|
QZSSPropagator.Builder |
mass(double userMass)
Sets the mass.
|
public Builder(QZSSOrbitalElements qzssOrbElt)
The QZSS orbital elements is the only requested parameter to build a QZSSPropagator.
The attitude provider is set by default to the
DEFAULT_LAW
.
The mass is set by default to the
DEFAULT_MASS
.
The ECI frame is set by default to the
EME2000 frame
.
The ECEF frame is set by default to the
CIO/2010-based ITRF simple EOP
.
qzssOrbElt
- the QZSS orbital elements to be used by the QZSSpropagator.attitudeProvider(AttitudeProvider provider)
,
mass(double mass)
,
eci(Frame inertial)
,
ecef(Frame bodyFixed)
public QZSSPropagator.Builder attitudeProvider(AttitudeProvider userProvider)
userProvider
- the attitude providerpublic QZSSPropagator.Builder mass(double userMass)
userMass
- the mass (in kg)public QZSSPropagator.Builder eci(Frame inertial)
inertial
- the ECI framepublic QZSSPropagator.Builder ecef(Frame bodyFixed)
bodyFixed
- the ECEF framepublic QZSSPropagator build()
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