📄 ephemerisimprovement.cpp
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#pragma ident "$Id: EphemerisImprovement.cpp 778 2007-09-25 16:14:58Z ocibu $"//============================================================================//// 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// // Copyright 2004, The University of Texas at Austin////============================================================================//============================================================================////This software developed by Applied Research Laboratories at the University of//Texas at Austin, under contract to an agency or agencies within the U.S. //Department of Defense. The U.S. Government retains all rights to use,//duplicate, distribute, disclose, or release this software. ////Pursuant to DoD Directive 523024 //// DISTRIBUTION STATEMENT A: This software has been approved for public // release, distribution is unlimited.////=============================================================================/** * @file EphemerisImprovement.cpp * Implement improvements to the input satellite ephemerides, part of program DDBase. *///------------------------------------------------------------------------------------// system includes#include <list>// GPSTk// DDBase#include "DDBase.hpp"//------------------------------------------------------------------------------------using namespace std;using namespace gpstk;//------------------------------------------------------------------------------------// prototypes -- this module only//------------------------------------------------------------------------------------int EphemerisImprovement(void){try { if(CI.Verbose) oflog << "BEGIN EphemerisImprovement()" << endl; if(dynamic_cast<GPSEphemerisStore*>(pEph)) { GPSEphemerisStore& BCE = dynamic_cast<GPSEphemerisStore&>(*pEph); list<EngEphemeris> EphList; oflog << "XvtStore is broadcast ephemeris" << endl; //BCE.dump(1,oflog); long i, neph = BCE.addToList(EphList); //oflog << "There are " << neph << " ephemerides in the list:" << endl; GSatID sat; map<GSatID,long> IODEmap; map<GSatID,long>::iterator Imapit; list<EngEphemeris>::const_iterator it; // dump the list of ephemerides, and build a map of sat,IODE for(i=0,it=EphList.begin(); it != EphList.end(); it++,i++) { short prn = it->getPRNID(); sat = GSatID(prn,SatID::systemGPS); if(IODEmap.find(sat) == IODEmap.end()) { IODEmap[sat] = -1; } //oflog << " " << setw(2) << i+1 // << " " << sat // << " TOE: " << it->getEphemerisEpoch() // << " TOC: " << it->getEpochTime() // << " HOW: " << it->getTransmitTime() // << " IODE: " << it->getIODE() // << endl; } //for(Imapit=IODEmap.begin(); Imapit != IODEmap.end(); Imapit++) { // oflog << " IODEmap[" << Imapit->first << "] = " << Imapit->second << endl; //} // test change of ephemeris during the time span of the data DayTime tt=FirstEpoch; do { for(Imapit=IODEmap.begin(); Imapit != IODEmap.end(); Imapit++) { sat = Imapit->first; try { //const EngEphemeris& eph = BCE.findNearEphemeris(sat.prn,tt); // findNearEphemeris is obsolete b/c when an ephemeris is updated // early, its fit interval is adjusted to start (usually 16 seconds) // BEFORE that of the ephemeris it is replacing. // This means findEphemeris will now always find the 'best' ephemeris, // whereas findNearEphemeris used to fill that purpose. const EngEphemeris& eph = BCE.findEphemeris(sat,tt); i = eph.getIODE(); if(IODEmap[sat] == -1) { //oflog << "Satellite " << sat // << " starts with ephemeris IODE " << i // << " at epoch " << tt << endl; IODEmap[sat] = i; } if(IODEmap[sat] != i) { oflog << "Satellite " << sat << " changes ephemeris (" << IODEmap[sat] << " -> " << i << ") at epoch " << tt.printf("%Y/%02m/%02d %2H:%02M:%6.3f=%F/%10.3g") << endl; IODEmap[sat] = i; } } catch(InvalidRequest& nef) { continue; } } tt += CI.DataInterval; } while(tt < LastEpoch); } if(dynamic_cast<SP3EphemerisStore*>(pEph)) { SP3EphemerisStore& SP3E = dynamic_cast<SP3EphemerisStore&>(*pEph); oflog << "EphemerisStore is SP3 ephemeris" << endl; } return 0;}catch(Exception& e) { GPSTK_RETHROW(e); }catch(exception& e) { Exception E("std except: "+string(e.what())); GPSTK_THROW(E); }catch(...) { Exception e("Unknown exception"); GPSTK_THROW(e); }} // end EphemerisImprovement()//------------------------------------------------------------------------------------//------------------------------------------------------------------------------------
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