modeledpseudorangebase.hpp

一个gps小工具包

/**
 * @file ModeledPseudorangeBase.hpp
 * Abstract base class for modeled pseudoranges
 */

#ifndef GPSTK_MODELEDPSEUDORANGEBASE_HPP
#define GPSTK_MODELEDPSEUDORANGEBASE_HPP

//============================================================================
//
//  This file is part of GPSTk, the GPS Toolkit.
//
//  The GPSTk is free software; you can redistribute it and/or modify
//  it under the terms of the GNU Lesser General Public License as published
//  by the Free Software Foundation; either version 2.1 of the License, or
//  any later version.
//
//  The GPSTk is distributed in the hope that it will be useful,
//  but WITHOUT ANY WARRANTY; without even the implied warranty of
//  MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
//  GNU Lesser General Public License for more details.
//
//  You should have received a copy of the GNU Lesser General Public
//  License along with GPSTk; if not, write to the Free Software Foundation,
//  Inc., 59 Temple Place, Suite 330, Boston, MA  02111-1307  USA
//  
//  Dagoberto Salazar - gAGE. 2006
//
//============================================================================



#include "Xvt.hpp"
#include "Position.hpp"
#include "Matrix.hpp"
#include "Vector.hpp"
#include "RinexObsHeader.hpp"
#include <vector>


namespace gpstk
{
      /** @addtogroup GPSsolutions */
      //@{

      /**
       * This abstract class deals with modeled pseudoranges.
       */
   class ModeledPseudorangeBase
   {
   public:

        /// Implicit constructor
        ModeledPseudorangeBase() : minElev(10.0) {};

        /// Either estimated or "a priori" position of receiver
        Position rxPos;

        /// Estimated geometric ranges from satellites to receiver
        Vector<double> geometricRho;

        /// Satellite clock biases, in meters
        Vector<double> svClockBiases;

        /// Satellite ECEF positions (m) and velocities (m/s) at transmission time
        Vector<Xvt> svXvt;

        /// Epoch when the signal left the satellite (Transmission time)
        Vector<DayTime> svTxTime;

        /// Total Group Delay (TGD) of satellites, in meters
        Vector<double> svTGD;

        /// Relativity corrections of satellites, in meters
        Vector<double> svRelativity;

        /// Ionospheric corrections in each receiver-satellite ray, in meters
        Vector<double> ionoCorrections;

        /// Tropospheric corrections in each receiver-satellite ray, in meters
        Vector<double> tropoCorrections;

        /// Observed (measured) pseudoranges from satellites to receiver
        Vector<double> observedPseudoranges;

        /// Modeled pseudoranges from satellites to receiver
        Vector<double> modeledPseudoranges;

        /// Prefit-residuals: Difference between Pseudoranges and ModeledPseudoranges
        Vector<double> prefitResiduals;

        /// Matrix of Geometry (director cosines from receiver to satellites)
        Matrix<double> geoMatrix;

        /// The elevation cut-off angle for accepted satellites. By default is set to 10 degrees
        double minElev;

        /// Any other biases (in meters) that the user wants to include. Will be substracted from modeled pseudoranges.
        Vector<double> extraBiases;

        /// Boolean telling if there are available computed data for at least 4 satellites
        bool validData;

        /// Vector with the PRN of satellites available for computing.
        Vector<SatID> availableSV;

        /// Vector with the PRN of satellites rejected or not used in computing.
        Vector<SatID> rejectedSV;

        /// Vector with the geodetic elevation of satellites from the receiver point of view.
        Vector<double> elevationSV;

        /// Vector with the geodetic azimuth of satellites from the receiver point of view.
        Vector<double> azimuthSV;

        /// Destructor.
        virtual ~ModeledPseudorangeBase() throw() {};

   protected:
        /// Method to set the initial (a priori) position of receiver.
        virtual int setInitialRxPosition() throw(Exception) = 0;


   }; // class ModeledPseudorangeBase

   //@}

} // namespace

#endif