fr.cnes.sirius.patrius.orbits.pvcoordinates

Class AlmanacGNSSParameters

java.lang.Object

fr.cnes.sirius.patrius.orbits.pvcoordinates.GNSSParameters

fr.cnes.sirius.patrius.orbits.pvcoordinates.AlmanacGNSSParameters

All Implemented Interfaces:

Serializable

public class AlmanacGNSSParameters
extends GNSSParameters

This class is a simple container for an almanac ephemeris description parameters of GNSS satellites (GPS, Galileo or BeiDou)

Author:

fteilhard

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description
AlmanacGNSSParameters(GNSSType gnssType, double refDuration, double m0, double e, double squareRootA, double omega0, double i0, double w0, double rateRa, double af0, double af1) Creates an instance of GNSS Parameter for the almanac model (for GPS, Galileo or BeiDou)

Method Summary

Methods inherited from class fr.cnes.sirius.patrius.orbits.pvcoordinates.GNSSParameters

getAf0, getAf1, getAf2, getaRate, getCic, getCis, getCrc, getCrs, getCuc, getCus, getDeltaN, getDeltaNRate, getEccentricity, getGnssType, getI, getiRate, getMeanAnomalyInit, getOmegaInit, getOmegaRate, getSqrtA, gettRef, getW

Methods inherited from class java.lang.Object

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

Constructor Detail

AlmanacGNSSParameters

public AlmanacGNSSParameters(GNSSType gnssType,
                             double refDuration,
                             double m0,
                             double e,
                             double squareRootA,
                             double omega0,
                             double i0,
                             double w0,
                             double rateRa,
                             double af0,
                             double af1)

Creates an instance of GNSS Parameter for the almanac model (for GPS, Galileo or BeiDou)

Parameters:

gnssType - the type of satellite (GPS, Galileo or BeiDou)

refDuration - time applicability of the almanac

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)

Since:

3.1