java.lang.Object
- org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider

All Implemented Interfaces:

ParameterDriversProvider

Direct Known Subclasses:

FieldGnssOrbitalElements, GNSSOrbitalElements
```
public abstract class GNSSOrbitalElementsDriversProvider
extends Object
implements ParameterDriversProvider
```
This class manages the non-keplerian parameter drivers for GNSSOrbitalElements and FieldGnssOrbitalElements.
In both primitive double and field classes, only the non-Keplerian parameters are returned in the getParametersDrivers() method, the Keplerian orbital parameters must be accessed independently. These groups ensure proper separate computation of state transition matrix and Jacobian matrix by GNSSPropagator and FieldGnssPropagator.

Since:

13.0

Author:

Luc Maisonobe

Field Summary

Fields
Modifier and Type	Field	Description
`static String`	`A_DOT`	Name for change rate in semi-major axis parameter.
`static int`	`A_DOT_INDEX`	Index of change rate in semi-major axis parameter in the list returned by `getParametersDrivers()`.
`static int`	`CIC_INDEX`	Index of cosine on inclination in the list returned by `getParametersDrivers()`.
`static int`	`CIS_INDEX`	Index of sine on inclination in the list returned by `getParametersDrivers()`.
`static int`	`CRC_INDEX`	Index of cosine on radius in the list returned by `getParametersDrivers()`.
`static int`	`CRS_INDEX`	Index of sine on radius in the list returned by `getParametersDrivers()`.
`static int`	`CUC_INDEX`	Index of cosine on latitude argument in the list returned by `getParametersDrivers()`.
`static int`	`CUS_INDEX`	Index of sine on latitude argument in the list returned by `getParametersDrivers()`.
`static String`	`DELTA_N0`	Name for delta of satellite mean motion.
`static String`	`DELTA_N0_DOT`	Name for change rate in Δn₀.
`static int`	`DELTA_N0_DOT_INDEX`	Index of change rate in Δn₀ in the list returned by `getParametersDrivers()`.
`static int`	`DELTA_N0_INDEX`	Index of delta of satellite mean motion in the list returned by `getParametersDrivers()`.
`static int`	`I_DOT_INDEX`	Index of inclination rate in the list returned by `getParametersDrivers()`.
`static String`	`INCLINATION_COSINE`	Name for cosine of inclination harmonic parameter.
`static String`	`INCLINATION_RATE`	Name for inclination rate parameter.
`static String`	`INCLINATION_SINE`	Name for sine of inclination harmonic parameter.
`static String`	`LATITUDE_COSINE`	Name for cosine of latitude argument harmonic parameter.
`static String`	`LATITUDE_SINE`	Name for sine of latitude argument harmonic parameter.
`static String`	`LONGITUDE_RATE`	Name for longitude rate parameter.
`static int`	`OMEGA_DOT_INDEX`	Index of longitude rate in the list returned by `getParametersDrivers()`.
`static String`	`RADIUS_COSINE`	Name for cosine of orbit radius harmonic parameter.
`static String`	`RADIUS_SINE`	Name for sine of orbit radius harmonic parameter.
`static int`	`SIZE`	Size of parameters array.
`static String`	`TIME`	Name for time parameter.
`static int`	`TIME_INDEX`	Index of time in the list returned by `getParametersDrivers()`.

Constructor Summary

Constructors
Modifier	Constructor	Description
`protected`	`GNSSOrbitalElementsDriversProvider(double angularVelocity, int weeksInCycle, TimeScales timeScales, SatelliteSystem system)`	Constructor.

Method Summary

All Methods Static Methods Instance Methods Abstract Methods Concrete Methods
Modifier and Type	Method	Description
`protected void`	`copyNonKeplerian(GNSSOrbitalElementsDriversProvider original)`	Copy non-Keplerian elements.
`protected void`	`copySelectionSettings(GNSSOrbitalElementsDriversProvider original)`	Copy drivers selection settings from another instance.
`protected static ParameterDriver`	`createDriver(String name, int scalePower)`	Create parameter driver.
`double`	`getADot()`	Get change rate in semi-major axis.
`ParameterDriver`	`getADotDriver()`	Get driver for the change rate in semi-major axis.
`double`	`getAngularVelocity()`	Get the mean angular velocity of the Earth of the GNSS model.
`double`	`getCic()`	Get amplitude of the cosine harmonic correction term to the angle of inclination.
`ParameterDriver`	`getCicDriver()`	Get the driver for the amplitude of the cosine harmonic correction term to the angle of inclination.
`double`	`getCis()`	Get amplitude of the sine harmonic correction term to the angle of inclination.
`ParameterDriver`	`getCisDriver()`	Get the driver for the amplitude of the sine harmonic correction term to the angle of inclination.
`double`	`getCrc()`	Get amplitude of the cosine harmonic correction term to the orbit radius.
`ParameterDriver`	`getCrcDriver()`	Get the driver for the amplitude of the cosine harmonic correction term to the orbit radius.
`double`	`getCrs()`	Get amplitude of the sine harmonic correction term to the orbit radius.
`ParameterDriver`	`getCrsDriver()`	Get the driver for the amplitude of the sine harmonic correction term to the orbit radius.
`double`	`getCuc()`	Get amplitude of the cosine harmonic correction term to the argument of latitude.
`ParameterDriver`	`getCucDriver()`	Get the driver for the amplitude of the cosine harmonic correction term to the argument of latitude.
`double`	`getCus()`	Get amplitude of the sine harmonic correction term to the argument of latitude.
`ParameterDriver`	`getCusDriver()`	Get the driver for the amplitude of the sine harmonic correction term to the argument of latitude.
`double`	`getCycleDuration()`	Get for the duration of the GNSS cycle in seconds.
`double`	`getDeltaN0()`	Get the delta of satellite mean motion.
`double`	`getDeltaN0Dot()`	Get the change rate in Δn₀.
`ParameterDriver`	`getDeltaN0DotDriver()`	Get the driver for change rate in Δn₀.
`ParameterDriver`	`getDeltaN0Driver()`	Get the driver for delta of satellite mean motion.
`double`	`getIDot()`	Get rate of inclination angle.
`ParameterDriver`	`getIDotDriver()`	Get the driver for the rate of inclination angle.
`double`	`getOmegaDot()`	Get rate of right ascension.
`ParameterDriver`	`getOmegaDotDriver()`	Get the driver for the rate of right ascension.
`List<ParameterDriver>`	`getParametersDrivers()`	Get the drivers for parameters.
`int`	`getPRN()`	Get the PRN number of the satellite.
`SatelliteSystem`	`getSystem()`	Get satellite system.
`double`	`getTime()`	Get reference time of the GNSS orbit as a duration from week start.
`ParameterDriver`	`getTimeDriver()`	Get the driver for reference time of the GNSS orbit as a duration from week start.
`TimeScales`	`getTimeScales()`	Get known time scales.
`int`	`getWeek()`	Get the reference week of the orbit.
`int`	`getWeeksInCycle()`	Get for the duration of the GNSS cycle in weeks.
`boolean`	`isCivilianMessage()`	Check if elements correspond to a civilian message.
`void`	`setADot(double aDot)`	Set change rate in semi-major axis.
`void`	`setCic(double cic)`	Set amplitude of the cosine harmonic correction term to the angle of inclination.
`void`	`setCis(double cis)`	Set amplitude of the sine harmonic correction term to the angle of inclination.
`void`	`setCrc(double crc)`	Set amplitude of the cosine harmonic correction term to the orbit radius.
`void`	`setCrs(double crs)`	Set amplitude of the sine harmonic correction term to the orbit radius.
`void`	`setCuc(double cuc)`	Set amplitude of the cosine harmonic correction term to the argument of latitude.
`void`	`setCus(double cus)`	Set amplitude of the sine harmonic correction term to the argument of latitude.
`void`	`setDeltaN0(double deltaN0)`	Set the delta of satellite mean motion.
`void`	`setDeltaN0Dot(double deltaN0Dot)`	Set the change rate in Δn₀.
`protected abstract void`	`setGnssDate(GNSSDate gnssDate)`	Set GNSS date.
`void`	`setIDot(double iDot)`	Set the driver for the rate of inclination angle.
`void`	`setOmegaDot(double dom)`	Set rate of right ascension.
`void`	`setPRN(int number)`	Set the PRN number of the satellite.
`void`	`setTime(double time)`	Set reference time of the GNSS orbit as a duration from week start.
`void`	`setWeek(int week)`	Set the reference week of the orbit.

Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.utils.ParameterDriversProvider
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported

- Field Detail
  - TIME
```
public static final String TIME
```
    Name for time parameter.
    
    See Also:
    
    Constant Field Values
  - A_DOT
```
public static final String A_DOT
```
    Name for change rate in semi-major axis parameter.
    
    Since:
    
    14.0
    
    See Also:
    
    Constant Field Values
  - DELTA_N0
```
public static final String DELTA_N0
```
    Name for delta of satellite mean motion.
    
    Since:
    
    14.0
    
    See Also:
    
    Constant Field Values
  - DELTA_N0_DOT
```
public static final String DELTA_N0_DOT
```
    Name for change rate in Δn₀.
    
    Since:
    
    14.0
    
    See Also:
    
    Constant Field Values
  - INCLINATION_RATE
```
public static final String INCLINATION_RATE
```
    Name for inclination rate parameter.
    
    See Also:
    
    Constant Field Values
  - LONGITUDE_RATE
```
public static final String LONGITUDE_RATE
```
    Name for longitude rate parameter.
    
    See Also:
    
    Constant Field Values
  - LATITUDE_COSINE
```
public static final String LATITUDE_COSINE
```
    Name for cosine of latitude argument harmonic parameter.
    
    See Also:
    
    Constant Field Values
  - LATITUDE_SINE
```
public static final String LATITUDE_SINE
```
    Name for sine of latitude argument harmonic parameter.
    
    See Also:
    
    Constant Field Values
  - RADIUS_COSINE
```
public static final String RADIUS_COSINE
```
    Name for cosine of orbit radius harmonic parameter.
    
    See Also:
    
    Constant Field Values
  - RADIUS_SINE
```
public static final String RADIUS_SINE
```
    Name for sine of orbit radius harmonic parameter.
    
    See Also:
    
    Constant Field Values
  - INCLINATION_COSINE
```
public static final String INCLINATION_COSINE
```
    Name for cosine of inclination harmonic parameter.
    
    See Also:
    
    Constant Field Values
  - INCLINATION_SINE
```
public static final String INCLINATION_SINE
```
    Name for sine of inclination harmonic parameter.
    
    See Also:
    
    Constant Field Values
  - TIME_INDEX
```
public static final int TIME_INDEX
```
    Index of time in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - A_DOT_INDEX
```
public static final int A_DOT_INDEX
```
    Index of change rate in semi-major axis parameter in the list returned by getParametersDrivers().
    
    Since:
    
    14.0
    
    See Also:
    
    Constant Field Values
  - DELTA_N0_INDEX
```
public static final int DELTA_N0_INDEX
```
    Index of delta of satellite mean motion in the list returned by getParametersDrivers().
    
    Since:
    
    14.0
    
    See Also:
    
    Constant Field Values
  - DELTA_N0_DOT_INDEX
```
public static final int DELTA_N0_DOT_INDEX
```
    Index of change rate in Δn₀ in the list returned by getParametersDrivers().
    
    Since:
    
    14.0
    
    See Also:
    
    Constant Field Values
  - I_DOT_INDEX
```
public static final int I_DOT_INDEX
```
    Index of inclination rate in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - OMEGA_DOT_INDEX
```
public static final int OMEGA_DOT_INDEX
```
    Index of longitude rate in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - CUC_INDEX
```
public static final int CUC_INDEX
```
    Index of cosine on latitude argument in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - CUS_INDEX
```
public static final int CUS_INDEX
```
    Index of sine on latitude argument in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - CRC_INDEX
```
public static final int CRC_INDEX
```
    Index of cosine on radius in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - CRS_INDEX
```
public static final int CRS_INDEX
```
    Index of sine on radius in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - CIC_INDEX
```
public static final int CIC_INDEX
```
    Index of cosine on inclination in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - CIS_INDEX
```
public static final int CIS_INDEX
```
    Index of sine on inclination in the list returned by getParametersDrivers().
    
    See Also:
    
    Constant Field Values
  - SIZE
```
public static final int SIZE
```
    Size of parameters array.
    
    See Also:
    
    Constant Field Values
- Constructor Detail
  - GNSSOrbitalElementsDriversProvider
```
protected GNSSOrbitalElementsDriversProvider(double angularVelocity,
                                             int weeksInCycle,
                                             TimeScales timeScales,
                                             SatelliteSystem system)
```
    Constructor.
    
    Parameters:
    
    angularVelocity - mean angular velocity of the Earth for the GNSS model
    
    weeksInCycle - number of weeks in the GNSS cycle
    
    timeScales - known time scales
    
    system - 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)
- Method Detail
  - copySelectionSettings
```
protected void copySelectionSettings(GNSSOrbitalElementsDriversProvider original)
```
    Copy drivers selection settings from another instance.
    
    Parameters:
    
    original - original instance providing selection settings
  - setGnssDate
```
protected abstract void setGnssDate(GNSSDate gnssDate)
```
    Set GNSS date.
    
    Parameters:
    
    gnssDate - GNSS date
  - createDriver
```
protected static ParameterDriver createDriver(String name,
                                              int scalePower)
```
    Create parameter driver.
    
    Parameters:
    
    name - name of the driver
    
    scalePower - power of two of the scale parameter
    
    Returns:
    
    build driver
  - getSystem
```
public SatelliteSystem getSystem()
```
    Get satellite system.
    
    Returns:
    
    satellite system
  - getTimeScales
```
public TimeScales getTimeScales()
```
    Get known time scales.
    
    Returns:
    
    known time scales
  - getParametersDrivers
```
public List<ParameterDriver> getParametersDrivers()
```
    Get the drivers for parameters.
    Only the 12 non-Keplerian evolution parameters are listed here, i.e. getTimeDriver() (at index TIME_INDEX), getADotDriver() (at index A_DOT_INDEX), getDeltaN0Driver() (at index DELTA_N0_INDEX), getDeltaN0DotDriver() (at index DELTA_N0_DOT_INDEX), getIDotDriver() (at index I_DOT_INDEX), getOmegaDotDriver() (at index OMEGA_DOT_INDEX), getCucDriver() (at index CUC_INDEX), getCusDriver() (at index CUS_INDEX), getCrcDriver() (at index CRC_INDEX), getCrsDriver() (at index CRS_INDEX), getCicDriver() (at index CIC_INDEX), and getCisDriver() (at index CIS_INDEX)
    
    The Keplerian orbital parameters drivers are not included.
    
    Specified by:
    
    getParametersDrivers in interface ParameterDriversProvider
    
    Returns:
    
    drivers for parameters
  - copyNonKeplerian
```
protected void copyNonKeplerian(GNSSOrbitalElementsDriversProvider original)
```
    Copy non-Keplerian elements.
    
    Parameters:
    
    original - original instance to copy from
    
    Since:
    
    14.0
  - getAngularVelocity
```
public double getAngularVelocity()
```
    Get the mean angular velocity of the Earth of the GNSS model.
    
    Returns:
    
    mean angular velocity of the Earth of the GNSS model
  - getWeeksInCycle
```
public int getWeeksInCycle()
```
    Get for the duration of the GNSS cycle in weeks.
    
    Returns:
    
    the duration of the GNSS cycle in weeks
  - getCycleDuration
```
public double getCycleDuration()
```
    Get for the duration of the GNSS cycle in seconds.
    
    Returns:
    
    the duration of the GNSS cycle in seconds
  - getPRN
```
public int getPRN()
```
    Get the PRN number of the satellite.
    
    Returns:
    
    PRN number of the satellite
  - setPRN
```
public void setPRN(int number)
```
    Set the PRN number of the satellite.
    
    Parameters:
    
    number - the prn number ot set
  - getWeek
```
public int getWeek()
```
    Get the reference week of the orbit.
    
    Returns:
    
    reference week of the orbit
  - setWeek
```
public void setWeek(int week)
```
    Set the reference week of the orbit.
    
    Parameters:
    
    week - the week to set
  - getTimeDriver
```
public ParameterDriver getTimeDriver()
```
    Get the driver for reference time of the GNSS orbit as a duration from week start.
    
    Returns:
    
    driver for the reference time of the GNSS orbit (s)
  - getTime
```
public double getTime()
```
    Get reference time of the GNSS orbit as a duration from week start.
    
    Returns:
    
    reference time of the GNSS orbit (s)
  - setTime
```
public void setTime(double time)
```
    Set reference time of the GNSS orbit as a duration from week start.
    
    Parameters:
    
    time - reference time of the GNSS orbit (s)
  - isCivilianMessage
```
public boolean isCivilianMessage()
```
    Check if elements correspond to a civilian message.
    
    Returns:
    
    true if elements correspond to a civilian message
    
    Since:
    
    14.0
  - getADotDriver
```
public ParameterDriver getADotDriver()
```
    Get driver for the change rate in semi-major axis.
    
    Returns:
    
    driver for the change rate in semi-major axis
    
    Since:
    
    14.0
  - getADot
```
public double getADot()
```
    Get change rate in semi-major axis.
    
    Returns:
    
    the change rate in semi-major axis
    
    Since:
    
    14.0
  - setADot
```
public void setADot(double aDot)
```
    Set change rate in semi-major axis.
    
    Parameters:
    
    aDot - change rate in semi-major axis
    
    Since:
    
    14.0
  - getDeltaN0Driver
```
public ParameterDriver getDeltaN0Driver()
```
    Get the driver for delta of satellite mean motion.
    
    Returns:
    
    driver for delta of satellite mean motion
    
    Since:
    
    14.0
  - getDeltaN0
```
public double getDeltaN0()
```
    Get the delta of satellite mean motion.
    
    Returns:
    
    the delta of satellite mean motion
    
    Since:
    
    14.0
  - setDeltaN0
```
public void setDeltaN0(double deltaN0)
```
    Set the delta of satellite mean motion.
    
    Parameters:
    
    deltaN0 - the value to set
    
    Since:
    
    14.0
  - getDeltaN0DotDriver
```
public ParameterDriver getDeltaN0DotDriver()
```
    Get the driver for change rate in Δn₀.
    
    Returns:
    
    driver for change rate in Δn₀
    
    Since:
    
    14.0
  - getDeltaN0Dot
```
public double getDeltaN0Dot()
```
    Get the change rate in Δn₀.
    
    Returns:
    
    change rate in Δn₀
    
    Since:
    
    14.0
  - setDeltaN0Dot
```
public void setDeltaN0Dot(double deltaN0Dot)
```
    Set the change rate in Δn₀.
    
    Parameters:
    
    deltaN0Dot - change rate in Δn₀
    
    Since:
    
    14.0
  - getIDotDriver
```
public ParameterDriver getIDotDriver()
```
    Get the driver for the rate of inclination angle.
    
    Returns:
    
    driver for the rate of inclination angle (rad/s)
  - getIDot
```
public double getIDot()
```
    Get rate of inclination angle.
    
    Returns:
    
    rate of inclination angle (rad/s)
  - setIDot
```
public void setIDot(double iDot)
```
    Set the driver for the rate of inclination angle.
    
    Parameters:
    
    iDot - rate of inclination angle (rad/s)
  - getOmegaDotDriver
```
public ParameterDriver getOmegaDotDriver()
```
    Get the driver for the rate of right ascension.
    
    Returns:
    
    driver for the rate of right ascension (rad/s)
  - getOmegaDot
```
public double getOmegaDot()
```
    Get rate of right ascension.
    
    Returns:
    
    rate of right ascension (rad/s)
  - setOmegaDot
```
public void setOmegaDot(double dom)
```
    Set rate of right ascension.
    
    Parameters:
    
    dom - rate of right ascension (rad/s)
  - getCucDriver
```
public ParameterDriver getCucDriver()
```
    Get the driver for the amplitude of the cosine harmonic correction term to the argument of latitude.
    
    Returns:
    
    driver for the amplitude of the cosine harmonic correction term to the argument of latitude (rad)
  - getCuc
```
public double getCuc()
```
    Get amplitude of the cosine harmonic correction term to the argument of latitude.
    
    Returns:
    
    amplitude of the cosine harmonic correction term to the argument of latitude (rad)
  - setCuc
```
public void setCuc(double cuc)
```
    Set amplitude of the cosine harmonic correction term to the argument of latitude.
    
    Parameters:
    
    cuc - amplitude of the cosine harmonic correction term to the argument of latitude (rad)
  - getCusDriver
```
public ParameterDriver getCusDriver()
```
    Get the driver for the amplitude of the sine harmonic correction term to the argument of latitude.
    
    Returns:
    
    driver for the amplitude of the sine harmonic correction term to the argument of latitude (rad)
  - getCus
```
public double getCus()
```
    Get amplitude of the sine harmonic correction term to the argument of latitude.
    
    Returns:
    
    amplitude of the sine harmonic correction term to the argument of latitude (rad)
  - setCus
```
public void setCus(double cus)
```
    Set amplitude of the sine harmonic correction term to the argument of latitude.
    
    Parameters:
    
    cus - amplitude of the sine harmonic correction term to the argument of latitude (rad)
  - getCrcDriver
```
public ParameterDriver getCrcDriver()
```
    Get the driver for the amplitude of the cosine harmonic correction term to the orbit radius.
    
    Returns:
    
    driver for the amplitude of the cosine harmonic correction term to the orbit radius (m)
  - getCrc
```
public double getCrc()
```
    Get amplitude of the cosine harmonic correction term to the orbit radius.
    
    Returns:
    
    amplitude of the cosine harmonic correction term to the orbit radius (m)
  - setCrc
```
public void setCrc(double crc)
```
    Set amplitude of the cosine harmonic correction term to the orbit radius.
    
    Parameters:
    
    crc - amplitude of the cosine harmonic correction term to the orbit radius (m)
  - getCrsDriver
```
public ParameterDriver getCrsDriver()
```
    Get the driver for the amplitude of the sine harmonic correction term to the orbit radius.
    
    Returns:
    
    driver for the amplitude of the sine harmonic correction term to the orbit radius (m)
  - getCrs
```
public double getCrs()
```
    Get amplitude of the sine harmonic correction term to the orbit radius.
    
    Returns:
    
    amplitude of the sine harmonic correction term to the orbit radius (m)
  - setCrs
```
public void setCrs(double crs)
```
    Set amplitude of the sine harmonic correction term to the orbit radius.
    
    Parameters:
    
    crs - amplitude of the sine harmonic correction term to the orbit radius (m)
  - getCicDriver
```
public ParameterDriver getCicDriver()
```
    Get the driver for the amplitude of the cosine harmonic correction term to the angle of inclination.
    
    Returns:
    
    driver for the amplitude of the cosine harmonic correction term to the angle of inclination (rad)
  - getCic
```
public double getCic()
```
    Get amplitude of the cosine harmonic correction term to the angle of inclination.
    
    Returns:
    
    amplitude of the cosine harmonic correction term to the angle of inclination (rad)
  - setCic
```
public void setCic(double cic)
```
    Set amplitude of the cosine harmonic correction term to the angle of inclination.
    
    Parameters:
    
    cic - amplitude of the cosine harmonic correction term to the angle of inclination (rad)
  - getCisDriver
```
public ParameterDriver getCisDriver()
```
    Get the driver for the amplitude of the sine harmonic correction term to the angle of inclination.
    
    Returns:
    
    driver for the amplitude of the sine harmonic correction term to the angle of inclination (rad)
  - getCis
```
public double getCis()
```
    Get amplitude of the sine harmonic correction term to the angle of inclination.
    
    Returns:
    
    amplitude of the sine harmonic correction term to the angle of inclination (rad)
  - setCis
```
public void setCis(double cis)
```
    Set amplitude of the sine harmonic correction term to the angle of inclination.
    
    Parameters:
    
    cis - amplitude of the sine harmonic correction term to the angle of inclination (rad)

Class GNSSOrbitalElementsDriversProvider

Field Summary

Constructor Summary

Method Summary

Methods inherited from class java.lang.Object

Methods inherited from interface org.orekit.utils.ParameterDriversProvider

Field Detail

TIME

A_DOT

DELTA_N0

DELTA_N0_DOT

INCLINATION_RATE

LONGITUDE_RATE

LATITUDE_COSINE

LATITUDE_SINE

RADIUS_COSINE

RADIUS_SINE

INCLINATION_COSINE

INCLINATION_SINE

TIME_INDEX

A_DOT_INDEX

DELTA_N0_INDEX

DELTA_N0_DOT_INDEX

I_DOT_INDEX

OMEGA_DOT_INDEX

CUC_INDEX

CUS_INDEX

CRC_INDEX

CRS_INDEX

CIC_INDEX

CIS_INDEX

SIZE

Constructor Detail

GNSSOrbitalElementsDriversProvider

Method Detail

copySelectionSettings

setGnssDate

createDriver

getSystem

getTimeScales

getParametersDrivers

copyNonKeplerian

getAngularVelocity

getWeeksInCycle

getCycleDuration

getPRN

setPRN

getWeek

setWeek

getTimeDriver

getTime

setTime

isCivilianMessage

getADotDriver

getADot

setADot

getDeltaN0Driver

getDeltaN0

setDeltaN0

getDeltaN0DotDriver

getDeltaN0Dot

setDeltaN0Dot

getIDotDriver

getIDot

setIDot

getOmegaDotDriver

getOmegaDot

setOmegaDot

getCucDriver

getCuc

setCuc

getCusDriver

getCus

setCus

getCrcDriver

getCrc

setCrc

getCrsDriver

getCrs

setCrs