Package org.orekit.propagation.analytical.gnss.data

Class FieldNavicLegacyNavigationMessage<T extends CalculusFieldElement<T>>

java.lang.Object

org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements<T,NavICLegacyNavigationMessage>

org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage<T,NavICLegacyNavigationMessage>

org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage<T,NavICLegacyNavigationMessage>

org.orekit.propagation.analytical.gnss.data.FieldNavicLegacyNavigationMessage<T>

Type Parameters:

T - type of the field elements

All Implemented Interfaces:

FieldOrbitalParameters<T>, FieldGNSSClockElements<T>, FieldTimeStamped<T>

public class FieldNavicLegacyNavigationMessage<T extends CalculusFieldElement<T>>
extends FieldLegacyNavigationMessage<T,NavICLegacyNavigationMessage>

Container for data contained in an NavIC navigation message.

Since:

13.0

Author:

Luc Maisonobe

Constructor Summary

Constructors

Constructor	Description
FieldNavicLegacyNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int iode, int iodc, T svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags)	Creates a new instance.

Method Summary

Modifier and Type	Method	Description
<U extends CalculusFieldElement<U>> FieldNavicLegacyNavigationMessage<U>	toField(FieldKeplerianOrbit<U> orbit, U[] nonKeplerian, Function<T,U> converter)	Create another field version of the instance.
NavICLegacyNavigationMessage	toNonField()	Create a non-field version of the instance.

Methods inherited from class org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage

getFitInterval, getIODC, getIODE, getL2Codes, getL2PFlags, getSvAccuracy, getSvHealth

Methods inherited from class org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage

getTransmissionTime

Methods inherited from class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements

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, toArray

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.time.FieldTimeStamped

durationFrom, durationFrom

Constructor Details

FieldNavicLegacyNavigationMessage

public FieldNavicLegacyNavigationMessage(double angularVelocity,
 int weeksInCycle,
 TimeScales timeScales,
 String type,
 int prn,
 FieldGNSSDate<T> toe,
 FieldKeplerianOrbit<T> orbit,
 T[] nonKeplerian,
 T tgd,
 FieldGNSSDate<T> toc,
 FieldGNSSDate<T> transmissionTime,
 int iode,
 int iodc,
 T svAccuracy,
 int svHealth,
 int fitInterval,
 int l2Codes,
 int l2PFlags)

Creates a new instance.

Parameters:

angularVelocity - mean angular velocity of the Earth for the GNSS model

weeksInCycle - number of weeks in the GNSS cycle

timeScales - known time scales

type - type (null if not a navigation message)

prn - PRN number of the satellite

toe - time of ephemeris (must be consistent with orbit)

orbit - Keplerian orbit in Earth-frozen frame

nonKeplerian - 15 non-Keplerian parameters (in the order given by NonKeplerianDriversFactory

tgd - group delay differential TGD for L1-L2 correction

toc - time of clock

transmissionTime - transmission time

iode - issue of data, ephemeris

iodc - issue of data, clock

svAccuracy - user SV accuracy (m)

svHealth - satellite health status

fitInterval - fit interval

l2Codes - codes on L2 channel

l2PFlags - L2 P data flags.

Since:

14.0

Method Details

toNonField

public NavICLegacyNavigationMessage toNonField()

Create a non-field version of the instance.

Specified by:

toNonField in class FieldGnssOrbitalElements<T extends CalculusFieldElement<T>,NavICLegacyNavigationMessage>

Returns:

non-field version of the instance

toField

public <U extends CalculusFieldElement<U>>
FieldNavicLegacyNavigationMessage<U> toField(FieldKeplerianOrbit<U> orbit,
 U[] nonKeplerian,
 Function<T,U> converter)

Create another field version of the instance.

Specified by:

toField in class FieldGnssOrbitalElements<T extends CalculusFieldElement<T>,NavICLegacyNavigationMessage>

Type Parameters:

U - type of the new field elements

Parameters:

orbit - orbit in the correct gradient field

nonKeplerian - non-Keplerian parameters

converter - converter for remaining elements

Returns:

field version of the instance