Class QZSSAlmanac
java.lang.Object
org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements<QZSSAlmanac>
org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
- All Implemented Interfaces:
OrbitalParameters,GNSSClockElements,TimeStamped
This class holds a QZSS almanac as read from YUMA files.
- Since:
- 10.0
- Author:
- Bryan Cazabonne
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Constructor Summary
ConstructorsConstructorDescriptionQZSSAlmanac(FieldQZSSAlmanac<T> original) Constructor from field instance.QZSSAlmanac(TimeScales timeScales, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, String source, int health) Constructor. -
Method Summary
Modifier and TypeMethodDescriptionbaseFactory(Frame inertial, Frame bodyFixed) Factory for the orbital elements.intGet the Health status.Get the source of this QZSS almanac.<T extends CalculusFieldElement<T>>
FieldQZSSAlmanac<T> toField(FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, DoubleFunction<T> converter) Create another field version of the instance.Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
factory, getADot, getAf0, getAf1, getAf2, getAngularVelocity, getCic, getCis, getCrc, getCrs, getCuc, getCus, getCycleDuration, getDate, getDeltaN0, getDeltaN0Dot, getIDot, getOmegaDot, getOrbit, getPrn, getTgd, getTimeOfClock, getTimeOfEphemeris, getTimeScales, getType, getWeeksInCycle, isCivilianMessage, toFieldMethods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, waitMethods inherited from interface org.orekit.time.TimeStamped
durationFrom
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Constructor Details
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QZSSAlmanac
public QZSSAlmanac(TimeScales timeScales, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, String source, int health) Constructor.- Parameters:
timeScales- known time scalesprn- PRN number of the satellitetoe- tim of ephemeris (must be consistent withorbit)orbit- Keplerian orbit in Earth-frozen frameaDot- change rate in semi-major axis (m/s)deltaN0- delta of satellite mean motiondeltaN0Dot- change rate in Δn₀iDot- inclination rate (rad/s)omegaDot- rate of right ascension (rad/s)cuc- amplitude of the cosine harmonic correction term to the argument of latitudecus- amplitude of the sine harmonic correction term to the argument of latitudecrc- amplitude of the cosine harmonic correction term to the orbit radiuscrs- amplitude of the sine harmonic correction term to the orbit radiuscic- amplitude of the cosine harmonic correction term to the inclinationcis- amplitude of the sine harmonic correction term to the inclinationaf0- zero-th order clock correction (s)af1- first order clock correction (s/s)af2- second order clock correction (s/s²)tgd- group delay differential TGD for L1-L2 correctiontoc- time of clocksource- source of the almanachealth- health status
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QZSSAlmanac
Constructor from field instance.- Type Parameters:
T- type of the field elements- Parameters:
original- regular field instance
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Method Details
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toField
public <T extends CalculusFieldElement<T>> FieldQZSSAlmanac<T> toField(FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, DoubleFunction<T> converter) Create another field version of the instance.- Specified by:
toFieldin classGNSSOrbitalElements<QZSSAlmanac>- Type Parameters:
T- type of the field elements- Parameters:
orbit- orbit in the correct gradient fieldnonKeplerian- non-Keplerian parametersconverter- converter for remaining elements- Returns:
- gradient version of the instance
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getSource
Get the source of this QZSS almanac.- Returns:
- the source of this QZSS almanac
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getHealth
public int getHealth()Get the Health status.- Returns:
- the Health status
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baseFactory
Factory for the orbital elements.- Specified by:
baseFactoryin classGNSSOrbitalElements<QZSSAlmanac>- Parameters:
inertial- reference inertial framebodyFixed- body fixed frame (will be frozen atdateto build the orbital elements- Returns:
- factory for the orbital elements
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