Class NavICAlmanacFactory
java.lang.Object
org.orekit.orbits.AbstractOrbitalParameterFactory<NavICAlmanac>
org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsFactory<NavICAlmanac>
org.orekit.propagation.analytical.gnss.data.NavICAlmanacFactory
- All Implemented Interfaces:
Cloneable,OrbitalParameterFactory<NavICAlmanac>
Factory for
NavICAlmanac.- Since:
- 14.0
- Author:
- Luc Maisonobe
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Field Summary
Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsFactory
ARGUMENT_OF_PERIAPSIS, ECCENTRICITY, FROZEN, INCLINATION, MEAN_ANOMALY, NODE_LONGITUDE, SEMI_MAJOR_AXIS -
Constructor Summary
ConstructorsConstructorDescriptionNavICAlmanacFactory(TimeScales timeScales, SatelliteSystem system, Frame inertial, Frame bodyFixed) Simple constructor. -
Method Summary
Modifier and TypeMethodDescriptionCreate orbital parameters from current drivers values.Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsFactory
buildOrbitalDrivers, createOrbitFromDrivers, getADotDriver, getAf0Driver, getAf1Driver, getAf2Driver, getAngularVelocity, getBodyFixed, getCicDriver, getCisDriver, getCrcDriver, getCrsDriver, getCucDriver, getCusDriver, getDeltaN0DotDriver, getDeltaN0Driver, getIDotDriver, getInertial, getJacobianWrtParameters, getNonKeplerianParametersDrivers, getOmegaDotDriver, getPrn, getSystem, getTgd, getTimeDriver, getTimeOfClock, getTimeOfEphemeris, getTimeScales, getType, jacobianWrtParameters, setDate, setPrn, setTgd, setTimeOfClock, setTimeOfEphemeris, toArrayMethods inherited from class org.orekit.orbits.AbstractOrbitalParameterFactory
clone, getDate, getFrame, getJacobianWrtCartesian, getMu, getOrbitalParametersDrivers, getOrbitType, getPositionAngleType, reset, setFrame, setMu, setPositionAngleType
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Constructor Details
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NavICAlmanacFactory
public NavICAlmanacFactory(TimeScales timeScales, SatelliteSystem system, Frame inertial, Frame bodyFixed) Simple constructor.- Parameters:
timeScales- known time scalessystem- satellite system to use for interpreting week numberinertial- reference inertial framebodyFixed- body fixed frame (will be frozen atdateto build the orbital elements
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Method Details
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createFromDrivers
Create orbital parameters from current drivers values.- Returns:
- created orbital parameters
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