CommonGnssData (ORbit Extrapolation KIT 11.0 API)

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

Direct Known Subclasses:

AbstractAlmanac, AbstractNavigationMessage
```
public class CommonGnssData
extends Object
```
Container for common GNSS data contained in almanac and navigation messages.

Since:

11.0

Author:

Bryan Cazabonne

Constructor Summary

Constructors
Constructor and Description

CommonGnssData(double mu, double angularVelocity, int weekNumber)
Constructor.

Constructors
Constructor and Description
`CommonGnssData(double mu, double angularVelocity, int weekNumber)` Constructor.

Method Summary

All Methods Instance Methods Concrete Methods
Modifier and Type	Method and Description
`double`	`getAf0()` Getter for the the SV Clock Bias Correction Coefficient.
`double`	`getAf1()` Getter for the SV Clock Drift Correction Coefficient.
`double`	`getAngularVelocity()` Getter for the mean angular velocity of the Earth for the GNSS model.
`double`	`getCycleDuration()` Getter for the duration of the GNSS cycle in seconds.
`AbsoluteDate`	`getDate()` Getter for the ephemeris reference date.
`double`	`getE()` Getter for the eccentricity.
`double`	`getI0()` Getter for the inclination angle at reference time.
`double`	`getM0()` Getter for the mean anomaly at reference time.
`double`	`getMu()` Getter for the Earth's universal gravitational parameter.
`double`	`getOmega0()` Getter for the longitude of ascending node of orbit plane at weekly epoch.
`double`	`getOmegaDot()` Getter for the rate of right ascension.
`double`	`getPa()` Getter for the argument of perigee.
`int`	`getPRN()` Getter for the PRN number of the satellite.
`double`	`getSma()` Getter for the semi-major axis.
`double`	`getTime()` Getter for the reference time of the GNSS orbit as a duration from week start.
`int`	`getWeek()` Getter for the reference week of the GNSS orbit.
`void`	`setAf0(double af0)` Setter for the SV Clock Bias Correction Coefficient (s).
`void`	`setAf1(double af1)` Setter for the SV Clock Drift Correction Coefficient (s/s).
`void`	`setDate(AbsoluteDate date)` Setter for the reference epoch.
`void`	`setE(double e)` Setter the eccentricity.
`void`	`setI0(double i0)` Setter for the Inclination Angle at Reference Time (rad).
`void`	`setM0(double m0)` Setter for the Mean Anomaly at Reference Time (rad).
`void`	`setOmega0(double omega0)` Setter for the Longitude of Ascending Node of Orbit Plane at Weekly Epoch (rad).
`void`	`setOmegaDot(double omegaDot)` Setter for the rate of Rate of Right Ascension (rad/s).
`void`	`setPa(double omega)` Setter fir the Argument of Perigee (rad).
`void`	`setPRN(int number)` Setter for the PRN number of the satellite.
`void`	`setSma(double sma)` Setter for the semi-major axis.
`void`	`setTime(double time)` Setter for the reference time of the orbit as a duration from week start.
`void`	`setWeek(int week)` Setter for the reference week of the orbit.

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

- Constructor Detail
  - CommonGnssData
```
public CommonGnssData(double mu,
                      double angularVelocity,
                      int weekNumber)
```
    Constructor.
    
    Parameters:
    
    mu - Earth's universal gravitational parameter
    
    angularVelocity - mean angular velocity of the Earth for the GNSS model
    
    weekNumber - number of weeks in the GNSS cycle
- Method Detail
  - getMu
```
public double getMu()
```
    Getter for the Earth's universal gravitational parameter.
    
    Returns:
    
    the Earth's universal gravitational parameter
  - getAngularVelocity
```
public double getAngularVelocity()
```
    Getter for the mean angular velocity of the Earth for the GNSS model.
    
    Returns:
    
    the mean angular velocity of the Earth for the GNSS model
  - getCycleDuration
```
public double getCycleDuration()
```
    Getter for the duration of the GNSS cycle in seconds.
    
    Returns:
    
    the duration of the GNSS cycle in seconds
  - getPRN
```
public int getPRN()
```
    Getter for the PRN number of the satellite.
    
    Returns:
    
    the PRN number of the satellite
  - setPRN
```
public void setPRN(int number)
```
    Setter for the PRN number of the satellite.
    
    Parameters:
    
    number - the prn number ot set
  - getWeek
```
public int getWeek()
```
    Getter for the reference week of the GNSS orbit.
    
    Returns:
    
    the reference week of the GNSS orbit
  - setWeek
```
public void setWeek(int week)
```
    Setter for the reference week of the orbit.
    
    Parameters:
    
    week - the week to set
  - getSma
```
public double getSma()
```
    Getter for the semi-major axis.
    
    Returns:
    
    the semi-major axis in meters
  - setSma
```
public void setSma(double sma)
```
    Setter for the semi-major axis.
    
    Parameters:
    
    sma - the semi-major axis (m)
  - getTime
```
public double getTime()
```
    Getter for the reference time of the GNSS orbit as a duration from week start.
    
    Returns:
    
    the reference time in seconds
  - setTime
```
public void setTime(double time)
```
    Setter for the reference time of the orbit as a duration from week start.
    
    Parameters:
    
    time - the time to set
  - getE
```
public double getE()
```
    Getter for the eccentricity.
    
    Returns:
    
    the eccentricity
  - setE
```
public void setE(double e)
```
    Setter the eccentricity.
    
    Parameters:
    
    e - the eccentricity to set
  - getI0
```
public double getI0()
```
    Getter for the inclination angle at reference time.
    
    Returns:
    
    the inclination angle at reference time in radians
  - setI0
```
public void setI0(double i0)
```
    Setter for the Inclination Angle at Reference Time (rad).
    
    Parameters:
    
    i0 - the inclination to set
  - getOmega0
```
public double getOmega0()
```
    Getter for the longitude of ascending node of orbit plane at weekly epoch.
    
    Returns:
    
    the longitude of ascending node of orbit plane at weekly epoch in radians
  - setOmega0
```
public void setOmega0(double omega0)
```
    Setter for the Longitude of Ascending Node of Orbit Plane at Weekly Epoch (rad).
    
    Parameters:
    
    omega0 - the longitude of ascending node to set
  - getOmegaDot
```
public double getOmegaDot()
```
    Getter for the rate of right ascension.
    
    Returns:
    
    the rate of right ascension in rad/s
  - setOmegaDot
```
public void setOmegaDot(double omegaDot)
```
    Setter for the rate of Rate of Right Ascension (rad/s).
    
    Parameters:
    
    omegaDot - the rate of right ascension to set
  - getPa
```
public double getPa()
```
    Getter for the argument of perigee.
    
    Returns:
    
    the argument of perigee in radians
  - setPa
```
public void setPa(double omega)
```
    Setter fir the Argument of Perigee (rad).
    
    Parameters:
    
    omega - the argumet of perigee to set
  - getM0
```
public double getM0()
```
    Getter for the mean anomaly at reference time.
    
    Returns:
    
    the mean anomaly at reference time in radians
  - setM0
```
public void setM0(double m0)
```
    Setter for the Mean Anomaly at Reference Time (rad).
    
    Parameters:
    
    m0 - the mean anomaly to set
  - getAf0
```
public double getAf0()
```
    Getter for the the SV Clock Bias Correction Coefficient.
    
    Returns:
    
    the SV Clock Bias Correction Coefficient (s).
  - setAf0
```
public void setAf0(double af0)
```
    Setter for the SV Clock Bias Correction Coefficient (s).
    
    Parameters:
    
    af0 - the SV Clock Bias Correction Coefficient to set
  - getAf1
```
public double getAf1()
```
    Getter for the SV Clock Drift Correction Coefficient.
    
    Returns:
    
    the SV Clock Drift Correction Coefficient (s/s).
  - setAf1
```
public void setAf1(double af1)
```
    Setter for the SV Clock Drift Correction Coefficient (s/s).
    
    Parameters:
    
    af1 - the SV Clock Drift Correction Coefficient to set
  - getDate
```
public AbsoluteDate getDate()
```
    Getter for the ephemeris reference date.
    
    Returns:
    
    the ephemeris reference date
  - setDate
```
public void setDate(AbsoluteDate date)
```
    Setter for the reference epoch.
    
    Parameters:
    
    date - the epoch to set

Class CommonGnssData

Constructor Summary

Method Summary

Methods inherited from class java.lang.Object

Constructor Detail

CommonGnssData

Method Detail

getMu

getAngularVelocity

getCycleDuration

getPRN

setPRN

getWeek

setWeek

getSma

setSma

getTime

setTime

getE

setE

getI0

setI0

getOmega0

setOmega0

getOmegaDot

setOmegaDot

getPa

setPa

getM0

setM0

getAf0

setAf0

getAf1

setAf1

getDate

setDate