org.orekit.propagation.analytical.gnss

Interface GNSSOrbitalElements

All Superinterfaces:

TimeStamped

All Known Subinterfaces:

BeidouOrbitalElements, GalileoOrbitalElements, GPSOrbitalElements, IRNSSOrbitalElements, QZSSOrbitalElements

All Known Implementing Classes:

BeidouAlmanac, GalileoAlmanac, GPSAlmanac, IRNSSAlmanac, QZSSAlmanac

public interface GNSSOrbitalElements
extends TimeStamped

This interface provides the minimal set of orbital elements needed by the AbstractGNSSPropagator.

Author:

Pascal Parraud

Method Summary

Modifier and Type	Method and Description
default double	getAf0() Gets the Zeroth Order Clock Correction.
default double	getAf1() Gets the First Order Clock Correction.
default double	getAf2() Gets the Second Order Clock Correction.
double	getCic() Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
double	getCis() Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
double	getCrc() Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
double	getCrs() Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
double	getCuc() Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
double	getCus() Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
double	getE() Gets the Eccentricity.
double	getI0() Gets the Inclination Angle at Reference Time.
double	getIDot() Gets the Rate of Inclination Angle.
double	getM0() Gets the Mean Anomaly at Reference Time.
double	getMeanMotion() Gets the Mean Motion.
double	getOmega0() Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.
double	getOmegaDot() Gets the Rate of Right Ascension.
double	getPa() Gets the Argument of Perigee.
int	getPRN() Gets the PRN number of the GNSS satellite.
double	getSma() Gets the Semi-Major Axis.
double	getTime() Gets the Reference Time of the GNSS orbit as a duration from week start.
default double	getToc() Gets the clock correction reference time toc.
int	getWeek() Gets the Reference Week of the GNSS orbit.

Methods inherited from interface org.orekit.time.TimeStamped

getDate

Method Detail

getPRN

int getPRN()

Gets the PRN number of the GNSS satellite.

Returns:

the PRN number of the GNSS satellite

getWeek

int getWeek()

Gets the Reference Week of the GNSS orbit.

Returns:

the Reference Week of the GNSS orbit within [0, 1024[

getTime

double getTime()

Gets the Reference Time of the GNSS orbit as a duration from week start.

Returns:

the Reference Time of the GNSS orbit (s)

getSma

double getSma()

Gets the Semi-Major Axis.

Returns:

the Semi-Major Axis (m)

getMeanMotion

double getMeanMotion()

Gets the Mean Motion.

Returns:

the Mean Motion (rad/s)

getE

double getE()

Gets the Eccentricity.

Returns:

the Eccentricity

getI0

double getI0()

Gets the Inclination Angle at Reference Time.

Returns:

the Inclination Angle at Reference Time (rad)

getIDot

double getIDot()

Gets the Rate of Inclination Angle.

Returns:

the Rate of Inclination Angle (rad/s)

getOmega0

double getOmega0()

Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.

Returns:

the Longitude of Ascending Node of Orbit Plane at Weekly Epoch (rad)

getOmegaDot

double getOmegaDot()

Gets the Rate of Right Ascension.

Returns:

the Rate of Right Ascension (rad/s)

getPa

double getPa()

Gets the Argument of Perigee.

Returns:

the Argument of Perigee (rad)

getM0

double getM0()

Gets the Mean Anomaly at Reference Time.

Returns:

the Mean Anomaly at Reference Time (rad)

getCuc

double getCuc()

Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.

Returns:

the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude (rad)

getCus

double getCus()

Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.

Returns:

the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude (rad)

getCrc

double getCrc()

Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.

Returns:

the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius (m)

getCrs

double getCrs()

Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.

Returns:

the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius (m)

getCic

double getCic()

Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.

Returns:

the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination (rad)

getCis

double getCis()

Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.

Returns:

the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination (rad)

getAf0

default double getAf0()

Gets the Zeroth Order Clock Correction.

Returns:

the Zeroth Order Clock Correction (s)

Since:

9.3

See Also:

getAf1(), getAf2(), getToc()

getAf1

default double getAf1()

Gets the First Order Clock Correction.

Returns:

the First Order Clock Correction (s/s)

Since:

9.3

See Also:

getAf0(), getAf2(), getToc()

getAf2

default double getAf2()

Gets the Second Order Clock Correction.

Returns:

the Second Order Clock Correction (s/s²)

Since:

9.3

See Also:

getAf0(), getAf1(), getToc()

getToc

default double getToc()

Gets the clock correction reference time toc.

Returns:

the clock correction reference time (s)

Since:

9.3

See Also:

getAf0(), getAf1(), getAf2()