Class FieldBeidouCivilianNavigationMessage<T extends CalculusFieldElement<T>>
- java.lang.Object
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- org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider
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- org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements<T,O>
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- org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData<T,O>
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- org.orekit.propagation.analytical.gnss.data.FieldAbstractAlmanac<T,O>
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- org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage<T,BeidouCivilianNavigationMessage>
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- org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage<T>
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- Type Parameters:
T
- type of the field elements
- All Implemented Interfaces:
FieldGNSSClockElements<T>
,FieldTimeStamped<T>
,ParameterDriversProvider
public class FieldBeidouCivilianNavigationMessage<T extends CalculusFieldElement<T>> extends FieldAbstractNavigationMessage<T,BeidouCivilianNavigationMessage>
Container for data contained in a Beidou civilian navigation message.- Since:
- 13.0
- Author:
- Luc Maisonobe
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Field Summary
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Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider
CIC_INDEX, CIS_INDEX, CRC_INDEX, CRS_INDEX, CUC_INDEX, CUS_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 Constructor Description FieldBeidouCivilianNavigationMessage(Function<V,T> converter, FieldBeidouCivilianNavigationMessage<V> original)
Constructor from different field instance.FieldBeidouCivilianNavigationMessage(Field<T> field, BeidouCivilianNavigationMessage original)
Constructor from non-field instance.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description <U extends CalculusFieldElement<U>,G extends FieldGnssOrbitalElements<U,BeidouCivilianNavigationMessage>>
GchangeField(Function<T,U> converter)
Create another field version of the instance.T
getADot()
Getter for the change rate in semi-major axis.T
getDeltaN0Dot()
Getter for change rate in Δn₀.int
getHealth()
Getter for health.int
getIntegrityFlags()
Getter for B1C integrity flags.int
getIODC()
Getter for the Issue Of Data Clock (IODC).int
getIODE()
Getter for the Issue Of Data Ephemeris (IODE).T
getIscB1CD()
Getter for inter Signal Delay for B1 CD.T
getIscB1CP()
Getter for inter Signal Delay for B1 CP.T
getIscB2AD()
Getter for inter Signal Delay for B2 AD.RadioWave
getRadioWave()
Getter for radio wave.BeidouSatelliteType
getSatelliteType()
Getter for satellite type.int
getSisaiOc1()
Getter for Signal In Space Accuracy Index (clock drift accuracy).int
getSisaiOc2()
Getter for Signal In Space Accuracy Index (clock drift rate accuracy).int
getSisaiOcb()
Getter for Signal In Space Accuracy Index (radial and clock).int
getSisaiOe()
Getter for Signal In Space Accuracy Index (along track and across track).int
getSismai()
Getter for Signal In Space Monitoring Accuracy Index.T
getTgdB1Cp()
Getter for B1/B3 Group Delay Differential (s).T
getTgdB2ap()
Getter for B2 AP Group Delay Differential (s).T
getTgdB2bI()
Getter for B2B_i / B3I Group Delay Differential (s).void
setADot(T value)
Setter for the change rate in semi-major axis.void
setDeltaN0Dot(T deltaN0Dot)
Setter for change rate in Δn₀.void
setHealth(int health)
Setter for health.void
setIntegrityFlags(int integrityFlags)
Setter for B1C integrity flags.void
setIODC(int value)
Setter for the Issue of Data Clock.void
setIODE(int value)
Setter for the Issue of Data Ephemeris.void
setIscB1CD(T delay)
Setter for inter Signal Delay for B1 CD.void
setIscB1CP(T delay)
Setter for inter Signal Delay for B1 CP.void
setIscB2AD(T delay)
Setter for inter Signal Delay for B2 AD.void
setSatelliteType(BeidouSatelliteType satelliteType)
Setter for satellite type.void
setSisaiOc1(int sisaiOc1)
Setter for Signal In Space Accuracy Index (clock drift accuracy).void
setSisaiOc2(int sisaiOc2)
Setter for Signal In Space Accuracy Index (clock drift rate accuracy).void
setSisaiOcb(int sisaiOcb)
Setter for Signal In Space Accuracy Index (radial and clock).void
setSisaiOe(int sisaiOe)
Setter for Signal In Space Accuracy Index (along track and across track).void
setSismai(int sismai)
Setter for Signal In Space Monitoring Accuracy Index.void
setTgdB1Cp(T tgdB1Cp)
Setter for B1/B3 Group Delay Differential (s).void
setTgdB2ap(T tgdB2ap)
Setter for B2 AP Group Delay Differential (s).void
setTgdB2bI(T tgdB2bI)
Setter for B2B_i / B3I Group Delay Differential (s).BeidouCivilianNavigationMessage
toNonField()
Create a non-field version of the instance.-
Methods inherited from class org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage
getDeltaN0, getEpochToc, getSqrtA, getTransmissionTime, setDeltaN0, setEpochToc, setSqrtA, setTransmissionTime
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.FieldAbstractAlmanac
getPropagator, getPropagator, getPropagator
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData
getAf0, getAf1, getAf2, getTGD, getToc, setAf0, setAf1, setAf2, setTGD, setToc
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements
getDate, getE, getI0, getM0, getMeanMotion0, getMu, getOmega0, getPa, getSma, setE, setGnssDate, setI0, setM0, setOmega0, setPa, setSma
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider
copySelectionSettings, createDriver, getAngularVelocity, getCic, getCicDriver, getCis, getCisDriver, getCrc, getCrcDriver, getCrs, getCrsDriver, getCuc, getCucDriver, getCus, getCusDriver, getCycleDuration, getIDot, getIDotDriver, getOmegaDot, getOmegaDotDriver, getParametersDrivers, getPRN, getSystem, getTime, getTimeDriver, getTimeScales, getWeek, getWeeksInCycle, setCic, setCis, setCrc, setCrs, setCuc, setCus, 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.time.FieldTimeStamped
durationFrom, getDate
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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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Constructor Detail
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FieldBeidouCivilianNavigationMessage
public FieldBeidouCivilianNavigationMessage(Field<T> field, BeidouCivilianNavigationMessage original)
Constructor from non-field instance.- Parameters:
field
- field to which elements belongoriginal
- regular non-field instance
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FieldBeidouCivilianNavigationMessage
public FieldBeidouCivilianNavigationMessage(Function<V,T> converter, FieldBeidouCivilianNavigationMessage<V> original)
Constructor from different field instance.- Type Parameters:
V
- type of the old field elements- Parameters:
original
- regular non-field instanceconverter
- for field elements
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Method Detail
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toNonField
public BeidouCivilianNavigationMessage toNonField()
Create a non-field version of the instance.- Specified by:
toNonField
in classFieldGnssOrbitalElements<T extends CalculusFieldElement<T>,BeidouCivilianNavigationMessage>
- Returns:
- non-field version of the instance
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changeField
public <U extends CalculusFieldElement<U>,G extends FieldGnssOrbitalElements<U,BeidouCivilianNavigationMessage>> G changeField(Function<T,U> converter)
Create another field version of the instance.- Specified by:
changeField
in classFieldGnssOrbitalElements<T extends CalculusFieldElement<T>,BeidouCivilianNavigationMessage>
- Type Parameters:
U
- type of the new field elementsG
- type of the orbital elements (field version)- Parameters:
converter
- for field elements- Returns:
- field version of the instance
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getRadioWave
public RadioWave getRadioWave()
Getter for radio wave.- Returns:
- radio wave on which navigation signal is sent
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getADot
public T getADot()
Getter for the change rate in semi-major axis.- Overrides:
getADot
in classFieldGnssOrbitalElements<T extends CalculusFieldElement<T>,BeidouCivilianNavigationMessage>
- Returns:
- the change rate in semi-major axis
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setADot
public void setADot(T value)
Setter for the change rate in semi-major axis.- Parameters:
value
- the change rate in semi-major axis
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getDeltaN0Dot
public T getDeltaN0Dot()
Getter for change rate in Δn₀.- Overrides:
getDeltaN0Dot
in classFieldGnssOrbitalElements<T extends CalculusFieldElement<T>,BeidouCivilianNavigationMessage>
- Returns:
- change rate in Δn₀
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setDeltaN0Dot
public void setDeltaN0Dot(T deltaN0Dot)
Setter for change rate in Δn₀.- Parameters:
deltaN0Dot
- change rate in Δn₀
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getIODE
public int getIODE()
Getter for the Issue Of Data Ephemeris (IODE).- Returns:
- the Issue Of Data Ephemeris (IODE)
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setIODE
public void setIODE(int value)
Setter for the Issue of Data Ephemeris.- Parameters:
value
- the IODE to set
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getIODC
public int getIODC()
Getter for the Issue Of Data Clock (IODC).- Returns:
- the Issue Of Data Clock (IODC)
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setIODC
public void setIODC(int value)
Setter for the Issue of Data Clock.- Parameters:
value
- the IODC to set
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getIscB1CD
public T getIscB1CD()
Getter for inter Signal Delay for B1 CD.- Returns:
- inter signal delay
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setIscB1CD
public void setIscB1CD(T delay)
Setter for inter Signal Delay for B1 CD.- Parameters:
delay
- delay to set
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getIscB2AD
public T getIscB2AD()
Getter for inter Signal Delay for B2 AD.- Returns:
- inter signal delay
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setIscB2AD
public void setIscB2AD(T delay)
Setter for inter Signal Delay for B2 AD.- Parameters:
delay
- delay to set
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getIscB1CP
public T getIscB1CP()
Getter for inter Signal Delay for B1 CP.- Returns:
- inter signal delay
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setIscB1CP
public void setIscB1CP(T delay)
Setter for inter Signal Delay for B1 CP.- Parameters:
delay
- delay to set
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getSisaiOe
public int getSisaiOe()
Getter for Signal In Space Accuracy Index (along track and across track).- Returns:
- Signal In Space Accuracy Index (along track and across track)
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setSisaiOe
public void setSisaiOe(int sisaiOe)
Setter for Signal In Space Accuracy Index (along track and across track).- Parameters:
sisaiOe
- Signal In Space Accuracy Index (along track and across track)
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getSisaiOcb
public int getSisaiOcb()
Getter for Signal In Space Accuracy Index (radial and clock).- Returns:
- Signal In Space Accuracy Index (radial and clock)
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setSisaiOcb
public void setSisaiOcb(int sisaiOcb)
Setter for Signal In Space Accuracy Index (radial and clock).- Parameters:
sisaiOcb
- Signal In Space Accuracy Index (radial and clock)
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getSisaiOc1
public int getSisaiOc1()
Getter for Signal In Space Accuracy Index (clock drift accuracy).- Returns:
- Signal In Space Accuracy Index (clock drift accuracy)
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setSisaiOc1
public void setSisaiOc1(int sisaiOc1)
Setter for Signal In Space Accuracy Index (clock drift accuracy).- Parameters:
sisaiOc1
- Signal In Space Accuracy Index (clock drift accuracy)
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getSisaiOc2
public int getSisaiOc2()
Getter for Signal In Space Accuracy Index (clock drift rate accuracy).- Returns:
- Signal In Space Accuracy Index (clock drift rate accuracy)
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setSisaiOc2
public void setSisaiOc2(int sisaiOc2)
Setter for Signal In Space Accuracy Index (clock drift rate accuracy).- Parameters:
sisaiOc2
- Signal In Space Accuracy Index (clock drift rate accuracy)
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getSismai
public int getSismai()
Getter for Signal In Space Monitoring Accuracy Index.- Returns:
- Signal In Space Monitoring Accuracy Index
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setSismai
public void setSismai(int sismai)
Setter for Signal In Space Monitoring Accuracy Index.- Parameters:
sismai
- Signal In Space Monitoring Accuracy Index
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getHealth
public int getHealth()
Getter for health.- Returns:
- health
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setHealth
public void setHealth(int health)
Setter for health.- Parameters:
health
- health
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getIntegrityFlags
public int getIntegrityFlags()
Getter for B1C integrity flags.- Returns:
- B1C integrity flags
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setIntegrityFlags
public void setIntegrityFlags(int integrityFlags)
Setter for B1C integrity flags.- Parameters:
integrityFlags
- integrity flags
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getTgdB1Cp
public T getTgdB1Cp()
Getter for B1/B3 Group Delay Differential (s).- Returns:
- B1/B3 Group Delay Differential (s)
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setTgdB1Cp
public void setTgdB1Cp(T tgdB1Cp)
Setter for B1/B3 Group Delay Differential (s).- Parameters:
tgdB1Cp
- B1/B3 Group Delay Differential (s)
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getTgdB2ap
public T getTgdB2ap()
Getter for B2 AP Group Delay Differential (s).- Returns:
- B2 AP Group Delay Differential (s)
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setTgdB2ap
public void setTgdB2ap(T tgdB2ap)
Setter for B2 AP Group Delay Differential (s).- Parameters:
tgdB2ap
- B2 AP Group Delay Differential (s)
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getTgdB2bI
public T getTgdB2bI()
Getter for B2B_i / B3I Group Delay Differential (s).- Returns:
- B2B_i / B3I Group Delay Differential (s)
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setTgdB2bI
public void setTgdB2bI(T tgdB2bI)
Setter for B2B_i / B3I Group Delay Differential (s).- Parameters:
tgdB2bI
- B2B_i / B3I Group Delay Differential (s)
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getSatelliteType
public BeidouSatelliteType getSatelliteType()
Getter for satellite type.- Returns:
- satellite type
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setSatelliteType
public void setSatelliteType(BeidouSatelliteType satelliteType)
Setter for satellite type.- Parameters:
satelliteType
- satellite type
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