public class GLONASSAlmanac extends Object implements GLONASSOrbitalElements
GLONASS_MU, GLONASS_PI| Constructor and Description |
|---|
GLONASSAlmanac(int channel,
int health,
int day,
int month,
int year,
double ta,
double lambda,
double deltaI,
double pa,
double ecc,
double deltaT,
double deltaTDot,
double tGlo2UTC,
double tGPS2Glo,
double tGlo)
Constructor.
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| Modifier and Type | Method and Description |
|---|---|
AbsoluteDate |
getDate()
Get the date.
|
double |
getDeltaI()
Get the correction to the mean value of inlination.
|
double |
getDeltaT()
Get the correction to the mean value of Draconian period.
|
double |
getDeltaTDot()
Get the rate of change of Draconian period.
|
double |
getE()
Get the Eccentricity.
|
int |
getFrequencyChannel()
Get the frequency channel.
|
double |
getGlo2UTC()
Get the correction from GLONASS to UTC.
|
double |
getGloOffset()
Get the correction of time relative to GLONASS system time.
|
double |
getGPS2Glo()
Get the correction to GPS time relative GLONASS.
|
int |
getHealth()
Get the Health status.
|
double |
getLambda()
Get the longitude of ascending node of orbit.
|
int |
getN4()
Get the number of the current four year interval.
|
int |
getNa()
Get the number of the current day in a four year interval.
|
double |
getPa()
Get the Argument of Perigee.
|
double |
getTime()
Get the Reference Time.
|
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, waitgetGammaN, getIOD, getTN, getX, getXDot, getXDotDot, getY, getYDot, getYDotDot, getZ, getZDot, getZDotDotpublic GLONASSAlmanac(int channel,
int health,
int day,
int month,
int year,
double ta,
double lambda,
double deltaI,
double pa,
double ecc,
double deltaT,
double deltaTDot,
double tGlo2UTC,
double tGPS2Glo,
double tGlo)
channel - the frequency channel from -7 to 6)health - the Health statusday - the day of Almanacmonth - the month of Almanacyear - the year of Almanacta - the reference time of the almanac (s)lambda - the Greenwich longitude of ascending node of orbit (rad)deltaI - the correction to the mean value of inclination (rad)pa - the argument of perigee (rad)ecc - the eccentricitydeltaT - the correction to the mean value of Draconian period (s)deltaTDot - the rate of change of orbital periodtGlo2UTC - the correction from GLONASS to UTC (s)tGPS2Glo - the correction to GPS time relative GLONASS (s)tGlo - the correction of time relative to GLONASS system time (s)public AbsoluteDate getDate()
TimeStampedgetDate in interface TimeStampedpublic double getTime()
GLONASSOrbitalElementsgetTime in interface GLONASSOrbitalElementspublic double getLambda()
GLONASSOrbitalElementsgetLambda in interface GLONASSOrbitalElementspublic double getE()
GLONASSOrbitalElementsgetE in interface GLONASSOrbitalElementspublic double getPa()
GLONASSOrbitalElementsgetPa in interface GLONASSOrbitalElementspublic double getDeltaI()
GLONASSOrbitalElementsgetDeltaI in interface GLONASSOrbitalElementspublic double getDeltaT()
GLONASSOrbitalElementsgetDeltaT in interface GLONASSOrbitalElementspublic double getDeltaTDot()
GLONASSOrbitalElementsgetDeltaTDot in interface GLONASSOrbitalElementspublic int getHealth()
public int getFrequencyChannel()
public double getGlo2UTC()
public double getGPS2Glo()
public double getGloOffset()
public int getNa()
GLONASSOrbitalElementsgetNa in interface GLONASSOrbitalElementspublic int getN4()
GLONASSOrbitalElementsgetN4 in interface GLONASSOrbitalElementsCopyright © 2002-2019 CS Systèmes d'information. All rights reserved.