Class AbstractNavigationMessage<O extends AbstractNavigationMessage<O>>
- java.lang.Object
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- org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider
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- org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements<O>
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- org.orekit.propagation.analytical.gnss.data.CommonGnssData<O>
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- org.orekit.propagation.analytical.gnss.data.AbstractAlmanac<O>
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- org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage<O>
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- Type Parameters:
O- type of the orbital elements
- All Implemented Interfaces:
GNSSClockElements,NavigationMessage,TimeStamped,ParameterDriversProvider
- Direct Known Subclasses:
BeidouCivilianNavigationMessage,BeidouLegacyNavigationMessage,CivilianNavigationMessage,GalileoNavigationMessage,LegacyNavigationMessage
public abstract class AbstractNavigationMessage<O extends AbstractNavigationMessage<O>> extends AbstractAlmanac<O> implements NavigationMessage
Base class for GNSS navigation messages.- Since:
- 11.0
- Author:
- Bryan Cazabonne
- See Also:
GPSLegacyNavigationMessage,GalileoNavigationMessage,BeidouLegacyNavigationMessage,QZSSLegacyNavigationMessage,NavICLegacyNavigationMessage
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Field Summary
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Fields inherited from class org.orekit.propagation.analytical.gnss.data.CommonGnssData
AF0, AF1, AF2
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Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
ARGUMENT_OF_PERIGEE, ECCENTRICITY, INCLINATION, MEAN_ANOMALY, NODE_LONGITUDE, SEMI_MAJOR_AXIS
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Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider
A_DOT, A_DOT_INDEX, CIC_INDEX, CIS_INDEX, CRC_INDEX, CRS_INDEX, CUC_INDEX, CUS_INDEX, DELTA_N0, DELTA_N0_DOT, DELTA_N0_DOT_INDEX, DELTA_N0_INDEX, I_DOT_INDEX, INCLINATION_COSINE, INCLINATION_RATE, INCLINATION_SINE, LATITUDE_COSINE, LATITUDE_SINE, LONGITUDE_RATE, OMEGA_DOT_INDEX, RADIUS_COSINE, RADIUS_SINE, SIZE, TIME, TIME_INDEX
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Constructor Summary
Constructors Modifier Constructor Description protectedAbstractNavigationMessage(double mu, double angularVelocity, int weeksInCycle, TimeScales timeScales, SatelliteSystem system, String type)Constructor.protectedAbstractNavigationMessage(FieldAbstractNavigationMessage<T,A> original)Constructor from field instance.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description AbsoluteDategetEpochToc()Getter for the time of clock epoch.StringgetNavigationMessageSubType()Get navigation message subtype.StringgetNavigationMessageType()Get navigation message type.doublegetSqrtA()Getter for Square Root of Semi-Major Axis (√m).doublegetTransmissionTime()Getter for transmission time.voidsetEpochToc(AbsoluteDate epochToc)Setter for the time of clock epoch.voidsetSqrtA(double sqrtA)Setter for the Square Root of Semi-Major Axis (√m).voidsetTransmissionTime(double transmissionTime)Setter for transmission time.-
Methods inherited from class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
getPropagator, getPropagator
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.CommonGnssData
getAf0, getAf1, getAf2, getTGD, getToc, setAf0, setAf1, setAf2, setTGD, setToc
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
getDate, getE, getEDriver, getI0, getI0Driver, getM0, getM0Driver, getMeanMotion0, getMu, getOmega0, getOmega0Driver, getPa, getPaDriver, getSma, getSmaDriver, setE, setGnssDate, setI0, setM0, setOmega0, setPa, setSma, toField
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider
copyNonKeplerian, copySelectionSettings, createDriver, getADot, getADotDriver, getAngularVelocity, getCic, getCicDriver, getCis, getCisDriver, getCrc, getCrcDriver, getCrs, getCrsDriver, getCuc, getCucDriver, getCus, getCusDriver, getCycleDuration, getDeltaN0, getDeltaN0Dot, getDeltaN0DotDriver, getDeltaN0Driver, getIDot, getIDotDriver, getOmegaDot, getOmegaDotDriver, getParametersDrivers, getPRN, getSystem, getTime, getTimeDriver, getTimeScales, getWeek, getWeeksInCycle, isCivilianMessage, setADot, setCic, setCis, setCrc, setCrs, setCuc, setCus, setDeltaN0, setDeltaN0Dot, setIDot, setOmegaDot, setPRN, setTime, setWeek
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Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
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Methods inherited from interface org.orekit.utils.ParameterDriversProvider
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
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Methods inherited from interface org.orekit.time.TimeStamped
durationFrom, getDate
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Constructor Detail
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AbstractNavigationMessage
protected AbstractNavigationMessage(double mu, double angularVelocity, int weeksInCycle, TimeScales timeScales, SatelliteSystem system, String type)Constructor.- Parameters:
mu- Earth's universal gravitational parameterangularVelocity- mean angular velocity of the Earth for the GNSS modelweeksInCycle- number of weeks in the GNSS cycletimeScales- known time scalessystem- satellite system to consider for interpreting week number (may be different from real system, for example in Rinex nav, weeks are always according to GPS)type- message type
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AbstractNavigationMessage
protected AbstractNavigationMessage(FieldAbstractNavigationMessage<T,A> original)
Constructor from field instance.- Type Parameters:
T- type of the field elementsA- type of the orbital elements (non-field version)- Parameters:
original- regular field instance
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Method Detail
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getNavigationMessageType
public String getNavigationMessageType()
Get navigation message type.- Specified by:
getNavigationMessageTypein interfaceNavigationMessage- Returns:
- the navigation message type
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getNavigationMessageSubType
public String getNavigationMessageSubType()
Get navigation message subtype.- Specified by:
getNavigationMessageSubTypein interfaceNavigationMessage- Returns:
- the navigation message type
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getSqrtA
public double getSqrtA()
Getter for Square Root of Semi-Major Axis (√m).- Returns:
- Square Root of Semi-Major Axis (√m)
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setSqrtA
public void setSqrtA(double sqrtA)
Setter for the Square Root of Semi-Major Axis (√m).In addition, this method set the value of the Semi-Major Axis.
- Parameters:
sqrtA- the Square Root of Semi-Major Axis (√m)
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getEpochToc
public AbsoluteDate getEpochToc()
Getter for the time of clock epoch.- Returns:
- the time of clock epoch
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setEpochToc
public void setEpochToc(AbsoluteDate epochToc)
Setter for the time of clock epoch.- Parameters:
epochToc- the epoch to set
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getTransmissionTime
public double getTransmissionTime()
Getter for transmission time.- Returns:
- transmission time
- Since:
- 12.0
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setTransmissionTime
public void setTransmissionTime(double transmissionTime)
Setter for transmission time.- Parameters:
transmissionTime- transmission time- Since:
- 12.0
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