fr.cnes.sirius.patrius.orbits.pvcoordinates

Class CNAVGNSSParameters

java.lang.Object

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

fr.cnes.sirius.patrius.orbits.pvcoordinates.CNAVGNSSParameters

All Implemented Interfaces:

Serializable

public class CNAVGNSSParameters
extends GNSSParameters

This class is a simple container for a broadcast model CNAV ephemeris description parameters of GNSS satellites (GPS or BeiDou only)

Author:

fteilhard

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description

CNAVGNSSParameters(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 GNSS Parameter for the CNAV broadcast model (for GPS or BeiDou only)

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

CNAVGNSSParameters

public CNAVGNSSParameters(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 GNSS Parameter for the CNAV broadcast model (for GPS or BeiDou only)

Parameters:

gnssType - the type of satellite (GPS or BeiDou only)

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)