GNSSParameters (patrimoine de base SIRIUS 4.16 API)

java.lang.Object
- fr.cnes.sirius.patrius.orbits.pvcoordinates.GNSSParameters

All Implemented Interfaces:

Serializable

Direct Known Subclasses:

AlmanacGNSSParameters, CNAVGNSSParameters, LNAVGNSSParameters
```
public class GNSSParameters
extends Object
implements Serializable
```
This class is a simple container for generic ephemeris description parameters of GNSS satellites (almanac or broadcast model ephemeris).

Author:

fteilhard

See Also:

Serialized Form

Constructor Summary

Constructors
Modifier	Constructor and Description
`protected`	`GNSSParameters(GNSSType gnssType, double refDuration, double m0, double e, double squareRootA, double omega0, double i0, double w0, double rateRa, double af0, double af1, double af2, double deltaN, double iRate, double cuc, double cus, double crc, double crs, double cic, double cis, double aRate, double deltaNRate)` Creates an instance of a generic GNSS Parameter (for GPS or BeiDou only)

Method Summary

All Methods Instance Methods Concrete Methods
Modifier and Type	Method and Description
`double`	`getAf0()`
`double`	`getAf1()`
`double`	`getAf2()`
`double`	`getaRate()`
`double`	`getCic()`
`double`	`getCis()`
`double`	`getCrc()`
`double`	`getCrs()`
`double`	`getCuc()`
`double`	`getCus()`
`double`	`getDeltaN()`
`double`	`getDeltaNRate()`
`double`	`getEccentricity()`
`GNSSType`	`getGnssType()`
`double`	`getI()`
`double`	`getiRate()`
`double`	`getMeanAnomalyInit()`
`double`	`getOmegaInit()`
`double`	`getOmegaRate()`
`double`	`getSqrtA()`
`double`	`gettRef()`
`double`	`getW()`

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

- Constructor Detail
  - GNSSParameters
```
protected GNSSParameters(GNSSType gnssType,
                         double refDuration,
                         double m0,
                         double e,
                         double squareRootA,
                         double omega0,
                         double i0,
                         double w0,
                         double rateRa,
                         double af0,
                         double af1,
                         double af2,
                         double deltaN,
                         double iRate,
                         double cuc,
                         double cus,
                         double crc,
                         double crs,
                         double cic,
                         double cis,
                         double aRate,
                         double deltaNRate)
```
    Creates an instance of a generic GNSS Parameter (for GPS or BeiDou only)
    
    Parameters:
    
    gnssType - the type of satellite (GPS, Galileo or BeiDou)
    
    refDuration - time applicability of the model
    
    m0 - Initial Mean anomaly
    
    e - Eccentricity
    
    squareRootA - Semi major axis square root
    
    omega0 - Initial Right ascencion
    
    i0 - Orbital inclination
    
    w0 - Argument of perigee
    
    rateRa - Rate of right ascension
    
    af0 - Clock correcting parameter af0 (s)
    
    af1 - Clock correcting parameter af1 (s/s)
    
    af2 - Clock correcting parameter af2 (s/s2)
    
    deltaN - Mean motion difference from computed value (rad/s)
    
    iRate - Rate of inclination angle (rad/s)
    
    cuc - Amplitude of the cosine harmonic correction term to the argument of latitude (rad)
    
    cus - Amplitude of the sine harmonic correction term to the argument of latitude (rad)
    
    crc - Amplitude of the cosine harmonic correction term to the orbit radius (m)
    
    crs - Amplitude of the sine harmonic correction term to the orbit radius (m)
    
    cic - Amplitude of the cosine harmonic correction term to the angle of inclination (rad)
    
    cis - Amplitude of the sine harmonic correction term to the angle of inclination (rad)
    
    aRate - Change rate in semi-major axis (m/s)
    
    deltaNRate - Rate of mean motion difference from computed value (rad/s^2)
- Method Detail
  - getGnssType
```
public GNSSType getGnssType()
```
    Returns:
    
    the gnssType
  - getMeanAnomalyInit
```
public double getMeanAnomalyInit()
```
    Returns:
    
    the initial mean anomaly
  - getEccentricity
```
public double getEccentricity()
```
    Returns:
    
    the eccentricity
  - getSqrtA
```
public double getSqrtA()
```
    Returns:
    
    the square root of the semi-major axis
  - getOmegaInit
```
public double getOmegaInit()
```
    Returns:
    
    the initial right ascension of ascending node
  - getI
```
public double getI()
```
    Returns:
    
    the orbital inclination
  - getW
```
public double getW()
```
    Returns:
    
    the Argument of perigee
  - getOmegaRate
```
public double getOmegaRate()
```
    Returns:
    
    the Rate of right ascension
  - gettRef
```
public double gettRef()
```
    Returns:
    
    the number of seconds in the week
  - getAf0
```
public double getAf0()
```
    Returns:
    
    the Clock correcting parameter af0 (s)
  - getAf1
```
public double getAf1()
```
    Returns:
    
    the Clock correcting parameter af1 (s/s)
  - getAf2
```
public double getAf2()
```
    Returns:
    
    the Clock correcting parameter af2 (s/s^2)
  - getDeltaN
```
public double getDeltaN()
```
    Returns:
    
    the Mean motion difference from computed value (rad/s)
  - getiRate
```
public double getiRate()
```
    Returns:
    
    the Rate of inclination angle (rad/s)
  - getCuc
```
public double getCuc()
```
    Returns:
    
    the Amplitude of the cosine harmonic correction term to the argument of latitude (rad)
  - getCus
```
public double getCus()
```
    Returns:
    
    the Amplitude of the sine harmonic correction term to the argument of latitude (rad)
  - getCrc
```
public double getCrc()
```
    Returns:
    
    the Amplitude of the cosine harmonic correction term to the orbit radius (m)
  - getCrs
```
public double getCrs()
```
    Returns:
    
    the Amplitude of the sine harmonic correction term to the orbit radius (m)
  - getCic
```
public double getCic()
```
    Returns:
    
    the Amplitude of the cosine harmonic correction term to the angle of inclination (rad)
  - getCis
```
public double getCis()
```
    Returns:
    
    the Amplitude of the sine harmonic correction term to the angle of inclination (rad)
  - getaRate
```
public double getaRate()
```
    Returns:
    
    the Change rate in semi-major axis (m/s)
  - getDeltaNRate
```
public double getDeltaNRate()
```
    Returns:
    
    the Rate of mean motion difference from computed value (rad/s^2)

Class GNSSParameters

Constructor Summary

Method Summary

Methods inherited from class java.lang.Object

Constructor Detail

GNSSParameters

Method Detail

getGnssType

getMeanAnomalyInit

getEccentricity

getSqrtA

getOmegaInit

getI

getW

getOmegaRate

gettRef

getAf0

getAf1

getAf2

getDeltaN

getiRate

getCuc

getCus

getCrc

getCrs

getCic

getCis

getaRate

getDeltaNRate