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

Interface SBASOrbitalElements

    • Method Summary

      All Methods Instance Methods Abstract Methods Default Methods 
      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.

    • Method Detail

      • 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)