Package org.orekit.propagation.analytical.gnss.data

Interface SBASOrbitalElements

All Superinterfaces:
TimeStamped
All Known Implementing Classes:
SBASNavigationMessage
public interface SBASOrbitalElements extends TimeStamped
This interface provides the minimal set of orbital elements needed by the SBASPropagator.
Since:
10.1
Author:
Bryan Cazabonne

  • Method Summary

    Modifier and Type
    Method
    Description
    default double
    getAGf0()
    Gets the Zeroth Order Clock Correction.
    default double
    getAGf1()
    Gets the First Order Clock Correction.
    default int
    getIODN()
    Gets the Issue Of Data Navigation (IODN).
    int
    getPRN()
    Gets the PRN number of the SBAS satellite.
    double
    getTime()
    Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
    default double
    getToc()
    Gets the clock correction reference time toc.
    int
    getWeek()
    Gets the Reference Week of the SBAS orbit.
    double
    getX()
    Get the ECEF-X component of satellite coordinates.
    double
    getXDot()
    Get the ECEF-X component of satellite velocity vector.
    double
    getXDotDot()
    Get the ECEF-X component of satellite acceleration vector.
    double
    getY()
    Get the ECEF-Y component of satellite coordinates.
    double
    getYDot()
    Get the ECEF-Y component of satellite velocity vector.
    double
    getYDotDot()
    Get the ECEF-Y component of satellite acceleration vector.
    double
    getZ()
    Get the ECEF-Z component of satellite coordinates.
    double
    getZDot()
    Get the ECEF-Z component of satellite velocity vector.
    double
    getZDotDot()
    Get the ECEF-Z component of satellite acceleration vector.

    Methods inherited from interface org.orekit.time.TimeStamped

    durationFrom, getDate

  • Method Details

    • getPRN

      int getPRN()
      Gets the PRN number of the SBAS satellite.
      Returns:
      the PRN number of the SBAS satellite

    • getWeek

      int getWeek()
      Gets the Reference Week of the SBAS orbit.
      Returns:
      the Reference Week of the SBAS orbit

    • getTime

      double getTime()
      Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
      Returns:
      the Reference Time of the SBAS orbit (s)

    • getX

      double getX()
      Get the ECEF-X component of satellite coordinates.
      Returns:
      the ECEF-X component of satellite coordinates (m)

    • getXDot

      double getXDot()
      Get the ECEF-X component of satellite velocity vector.
      Returns:
      the the ECEF-X component of satellite velocity vector (m/s)

    • getXDotDot

      double getXDotDot()
      Get the ECEF-X component of satellite acceleration vector.
      Returns:
      the GLONASS ECEF-X component of satellite acceleration vector (m/s²)

    • getY

      double getY()
      Get the ECEF-Y component of satellite coordinates.
      Returns:
      the ECEF-Y component of satellite coordinates (m)

    • getYDot

      double getYDot()
      Get the ECEF-Y component of satellite velocity vector.
      Returns:
      the ECEF-Y component of satellite velocity vector (m/s)

    • getYDotDot

      double getYDotDot()
      Get the ECEF-Y component of satellite acceleration vector.
      Returns:
      the ECEF-Y component of satellite acceleration vector (m/s²)

    • getZ

      double getZ()
      Get the ECEF-Z component of satellite coordinates.
      Returns:
      the ECEF-Z component of satellite coordinates (m)

    • getZDot

      double getZDot()
      Get the ECEF-Z component of satellite velocity vector.
      Returns:
      the the ECEF-Z component of satellite velocity vector (m/s)

    • getZDotDot

      double getZDotDot()
      Get the ECEF-Z component of satellite acceleration vector.
      Returns:
      the ECEF-Z component of satellite acceleration vector (m/s²)

    • getIODN

      default int getIODN()
      Gets the Issue Of Data Navigation (IODN).
      Returns:
      the IODN

    • getAGf0

      default double getAGf0()
      Gets the Zeroth Order Clock Correction.
      Returns:
      the Zeroth Order Clock Correction (s)

    • getAGf1

      default double getAGf1()
      Gets the First Order Clock Correction.
      Returns:
      the First Order Clock Correction (s/s)

    • getToc

      default double getToc()
      Gets the clock correction reference time toc.
      Returns:
      the clock correction reference time (s)