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

Class FieldGPSCivilianNavigationMessage<T extends CalculusFieldElement<T>>

java.lang.Object

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

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

org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage<T,GPSCivilianNavigationMessage>

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

Type Parameters:

T - type of the field elements

All Implemented Interfaces:

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

public class FieldGPSCivilianNavigationMessage<T extends CalculusFieldElement<T>>
extends FieldCivilianNavigationMessage<T,GPSCivilianNavigationMessage>

Container for data contained in a GPS navigation message.

Since:

13.0

Author:

Luc Maisonobe

Constructor Summary

Constructors

Constructor

Description

FieldGPSCivilianNavigationMessage(boolean cnv2, 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, T svAccuracy, int svHealth, T iscL1CA, T iscL1CD, T iscL1CP, T iscL2C, T iscL5I5, T iscL5Q5, int uraiEd, int uraiNed0, int uraiNed1, int uraiNed2, int flags)

Creates a new instance.

Method Summary

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

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

getFlags, getIscL1CA, getIscL1CD, getIscL1CP, getIscL2C, getIscL5I5, getIscL5Q5, getSvAccuracy, getSvHealth, getUraiEd, getUraiNed0, getUraiNed1, getUraiNed2, isCivilianMessage, isCnv2

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, 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.propagation.analytical.gnss.data.FieldGNSSClockElements

getAf0, getAf1, getAf2, getTgd, getTimeOfClock

Methods inherited from interface org.orekit.time.FieldTimeStamped

durationFrom, durationFrom, getDate

Constructor Details

FieldGPSCivilianNavigationMessage

public FieldGPSCivilianNavigationMessage(boolean cnv2,
 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,
 T svAccuracy,
 int svHealth,
 T iscL1CA,
 T iscL1CD,
 T iscL1CP,
 T iscL2C,
 T iscL5I5,
 T iscL5Q5,
 int uraiEd,
 int uraiNed0,
 int uraiNed1,
 int uraiNed2,
 int flags)

Creates a new instance.

Parameters:

cnv2 - indicator for CNV2 messages

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

svAccuracy - user SV accuracy (m)

svHealth - satellite health status

iscL1CA - inter signal delay for L1 C/A

iscL1CD - inter signal delay for L1 CD

iscL1CP - inter signal delay for L1 CP

iscL2C - inter signal delay for L2 C

iscL5I5 - inter signal delay for L5I

iscL5Q5 - inter signal delay for L5Q

uraiEd - elevation-dependent user range accuracy

uraiNed0 - term 0 of non-elevation-dependent user range accuracy

uraiNed1 - term 1 of non-elevation-dependent user range accuracy

uraiNed2 - term 2 of non-elevation-dependent user range accuracy

flags - flags

Since:

14.0

Method Details

toNonField

public GPSCivilianNavigationMessage toNonField()

Create a non-field version of the instance.

Specified by:

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

Returns:

non-field version of the instance

toField

public <U extends CalculusFieldElement<U>>
FieldGPSCivilianNavigationMessage<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>,GPSCivilianNavigationMessage>

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