org.orekit.propagation.analytical.gnss

Interface IRNSSOrbitalElements

All Superinterfaces:

GNSSOrbitalElements, TimeStamped

All Known Implementing Classes:

IRNSSAlmanac

public interface IRNSSOrbitalElements
extends GNSSOrbitalElements

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

Since:

10.1

Author:

Bryan Cazabonne

See Also:

"Indian Regiona Navigation Satellite System, Signal In Space ICD for standard positioning service, version 1.1"

Field Summary

Fields

Modifier and Type	Field and Description
static double	IRNSS_MU WGS 84 value of the Earth's universal gravitational parameter for IRNSS user in m³/s².
static double	IRNSS_PI Value of Pi for conversion from semicircles to radian.
static double	IRNSS_WEEK_IN_SECONDS Duration of the IRNSS week in seconds.
static int	IRNSS_WEEK_NB Number of weeks in the IRNSS cycle.

Method Summary

Modifier and Type	Method and Description
default int	getIODEC() Gets the Issue Of Data Ephemeris and Clock (IODEC).
default double	getTGD() Gets the estimated group delay differential TGD for L5-S correction.

Methods inherited from interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements

getAf0, getAf1, getAf2, getCic, getCis, getCrc, getCrs, getCuc, getCus, getE, getI0, getIDot, getM0, getMeanMotion, getOmega0, getOmegaDot, getPa, getPRN, getSma, getTime, getToc, getWeek

Methods inherited from interface org.orekit.time.TimeStamped

getDate

Field Detail

IRNSS_MU

static final double IRNSS_MU

WGS 84 value of the Earth's universal gravitational parameter for IRNSS user in m³/s².

See Also:

Constant Field Values

IRNSS_PI

static final double IRNSS_PI

Value of Pi for conversion from semicircles to radian.

See Also:

Constant Field Values

IRNSS_WEEK_IN_SECONDS

static final double IRNSS_WEEK_IN_SECONDS

Duration of the IRNSS week in seconds.

See Also:

Constant Field Values

IRNSS_WEEK_NB

static final int IRNSS_WEEK_NB

Number of weeks in the IRNSS cycle.

See Also:

Constant Field Values

Method Detail

getIODEC

default int getIODEC()

Gets the Issue Of Data Ephemeris and Clock (IODEC).

Returns:

the Issue Of Data Ephemeris and Clock (IODEC)

getTGD

default double getTGD()

Gets the estimated group delay differential TGD for L5-S correction.

Returns:

the estimated group delay differential TGD for L5-S correction (s)