/[PAMELA software]/DarthVader/OrbitalInfo/src/OrbitalInfoCore.cpp

Diff of /DarthVader/OrbitalInfo/src/OrbitalInfoCore.cpp

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-revision 1.44 by mocchiut,
Fri Jan 29 17:27:57 2010 UTC
+revision 1.72 by mocchiut,
Tue Apr 15 15:48:17 2014 UTC
 Line 9
  // ROOT headers
  //
  //#include <TCanvas.h>
- //#include <TH2F.h> //for test only. Vitaly.
+ #include <TH2F.h> //for test only. Vitaly.
+ #include <TVector3.h>
  //#include <TF1.h>
  #include <TTree.h>
-Line 47
+Line 48
  #include <OrbitalInfoCore.h>
  #include <InclinationInfo.h>
+ //
+ // Tracker and ToF classes headers and definitions
+ //
+ #include <ToFLevel2.h>
+ #include <TrkLevel2.h>
  using namespace std;
-Line 65 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 71 
 int OrbitalInfoCore(UInt_t run, TFile *f
    stringstream myquery;
    myquery.str("");
    myquery << "SET time_zone='+0:00'";
-   dbc->Query(myquery.str().c_str());
+   delete dbc->Query(myquery.str().c_str());
    //
    TString processFolder = Form("OrbitalInfoFolder_%u",run);
    //
-Line 121 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 127 
 int OrbitalInfoCore(UInt_t run, TFile *f
    TTree *OrbitalInfotrclone = 0;
    Bool_t reproc = false;
    Bool_t reprocall = false;
+   Bool_t igrfloaded = false;
    UInt_t nobefrun = 0;
    UInt_t noaftrun = 0;
    UInt_t numbofrun = 0;
-Line 128 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 135 
 int OrbitalInfoCore(UInt_t run, TFile *f
    TString fname;
    UInt_t totfileentries = 0;
    UInt_t idRun = 0;
+   UInt_t anni5 = 60 * 60 * 24 * 365 * 5 ;//1576800
    //
    // My variables. Vitaly.
    //
-Line 180 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 188 
 int OrbitalInfoCore(UInt_t run, TFile *f
    //
    // IGRF stuff
    //
-   Float_t dimo = 0.0; // dipole moment (computed from dat files)
+   Double_t dimo = 0.0; // dipole moment (computed from dat files) // EM GCC 4.7
    Float_t bnorth, beast, bdown, babs;
    Float_t xl; // L value
    Float_t icode; // code value for L accuracy (see fortran code)
-Line 223 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 231 
 int OrbitalInfoCore(UInt_t run, TFile *f
    //
    //Quaternions classes
    //
-   Quaternions *L_QQ_Q_l_lower = new Quaternions();
+   Quaternions *L_QQ_Q_l_lower = 0;
-   InclinationInfo *RYPang_lower = new InclinationInfo();
+   InclinationInfo *RYPang_lower = 0;
-   Quaternions *L_QQ_Q_l_upper = new Quaternions();
+   Quaternions *L_QQ_Q_l_upper = 0;
-   InclinationInfo *RYPang_upper = new InclinationInfo();
+   InclinationInfo *RYPang_upper = 0;
    cEci eCi;
    // Initialize fortran routines!!!
+   Int_t ltp1 = 0;
    Int_t ltp2 = 0;
    Int_t ltp3 = 0;
-   Int_t uno = 1;
+   //  Int_t uno = 1;
-   const char *niente = " ";
+   //  const char *niente = " ";
+   GL_PARAM *glparam0 = new GL_PARAM();
    GL_PARAM *glparam = new GL_PARAM();
    GL_PARAM *glparam2 = new GL_PARAM();
+   GL_PARAM *glparam3 = new GL_PARAM();
    //
    // Orientation variables. Vitaly
-Line 244 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 255 
 int OrbitalInfoCore(UInt_t run, TFile *f
    UInt_t evfrom = 0;
    UInt_t jumped = 0;
    Int_t itr = -1;
-   Double_t A1;
+   //  Double_t A1;
-   Double_t A2;
+   //  Double_t A2;
-   Double_t A3;
+   //  Double_t A3;
    Double_t Px = 0;
    Double_t Py = 0;
    Double_t Pz = 0;
    TTree *ttof = 0;
    ToFLevel2 *tof = new ToFLevel2();
+   TTree *ttrke = 0;
+   TrkLevel2 *trke = new TrkLevel2();
    OrientationInfo *PO = new OrientationInfo();
    Int_t nz = 6;
    Float_t zin[6];
    Int_t nevtofl2 = 0;
+   Int_t nevtrkl2 = 0;
    if ( verbose ) cout<<"Reading quaternions external file"<<endl;
    cout.setf(ios::fixed,ios::floatfield);
    /******Reading recovered quaternions...*********/
-   //cout<<"START reading recovered quaternions..."<<endl;
    vector<Double_t> recqtime;
    vector<Float_t> recq0;
    vector<Float_t> recq1;
    vector<Float_t> recq2;
    vector<Float_t> recq3;
    Float_t Norm = 1;
-   Int_t parerror=glparam->Query_GL_PARAM(1,303,dbc); // parameters stored in DB in GL_PRAM table
+   Int_t parerror=glparam0->Query_GL_PARAM(1,303,dbc); // parameters stored in DB in GL_PRAM table
+   if ( verbose ) cout<<parerror<<"\t"<<(char*)(glparam0->PATH+glparam0->NAME).Data()<<endl;
+   ifstream in((char*)(glparam0->PATH+glparam0->NAME).Data(),ios::in);
    if ( parerror<0 ) {
      code = parerror;
-     goto closeandexit;
+     //goto closeandexit;
-   };
+   }
-   ifstream in((glparam->PATH+glparam->NAME).Data(),ios::in);
-   //cout<<"ifstream loaded..."<<endl;
    while(!in.eof()){
      recqtime.resize(recqtime.size()+1);
      Int_t sizee = recqtime.size();
-Line 286 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 299 
 int OrbitalInfoCore(UInt_t run, TFile *f
      in>>recq2[sizee-1];
      in>>recq3[sizee-1];
      in>>Norm;
-     //cout<<recqtime[sizee]<<endl;
    }
+   in.close();
    if ( verbose ) cout<<"We have read recovered data"<<endl;
+   if (debug) cout << "size of recovered quaterions data set is " << recqtime.size() << endl;
+   vector<UInt_t> RTtime1;
+   vector<UInt_t> RTtime2;
+   vector<Double_t> RTbank1;
+   vector<Double_t> RTbank2;
+   vector<Int_t> RTazim;
+   vector<Int_t> RTdir1;
+   vector<Int_t> RTdir2;
+   vector<Int_t> RTerrq;
+ // 10RED CHECK
+ //  TH2F* DIFFX = new TH2F("diffx","",100,0,100,90,0,90);
+ //  TH2F* DIFFY = new TH2F("diffy","",100,0,100,90,0,90);
+ //  TH2F* DIFFZ = new TH2F("diffz","",100,0,100,90,0,90);
+   ofstream mc;
+   TString gr = "methodscomparison_";
+   gr+=run;
+   gr+=".txt";
+   mc.open(gr);
+   mc.setf(ios::fixed,ios::floatfield);
+ // 10RED CHECK END
+   if ( verbose ) cout<<"read Rotation Table"<<endl;
+   Int_t parerror2=glparam0->Query_GL_PARAM(1,305,dbc);
+   ifstream an((char*)(glparam0->PATH+glparam0->NAME).Data(),ios::in);
+   if ( verbose ) cout<<parerror2<<"\t"<<(char*)(glparam0->PATH+glparam0->NAME).Data()<<endl;
+ //  if ( parerror2<0 ) {
+ //    code = parerror;
+     //goto closeandexit;
+ //  }
+ //ifstream an("/data03/Malakhov/pam9Malakhov/installed10/calib/orb-param/RDBCC.txt",ios::in);
+   while(!an.eof()){
+     RTtime1.resize(RTtime1.size()+1);
+     Int_t sizee = RTtime1.size();
+     RTbank1.resize(sizee+1);
+     RTazim.resize(sizee+1);
+     RTdir1.resize(sizee+1);
+     RTerrq.resize(sizee+1);
+     an>>RTtime1[sizee-1];
+     an>>RTbank1[sizee-1];
+     an>>RTazim[sizee-1];
+     an>>RTdir1[sizee-1];
+     an>>RTerrq[sizee-1];
+     if(sizee>1) {
+       RTtime2.resize(sizee+1);
+       RTbank2.resize(sizee+1);
+       RTdir2.resize(sizee+1);
+       RTtime2[sizee-2]=RTtime1[sizee-1];
+       RTbank2[sizee-2]=RTbank1[sizee-1];
+       RTdir2[sizee-2]=RTdir1[sizee-1];
+     }
+   }
+   an.close();
+   //cout<<"put some number here"<<endl;
+   //Int_t yupi;
+   //cin>>yupi;
+   if ( verbose ) cout<<"We have read Rotation Table"<<endl;
+     //Geomagnetic coordinates calculations staff
+   GMtype_CoordGeodetic location;
+   //  GMtype_CoordDipole GMlocation;
+   GMtype_Ellipsoid Ellip;
+   GMtype_Data G0, G1, H1;
+   //  { // this braces is necessary to avoid jump to label 'closeandexit'  error   // but it is wrong since the variable "igpath" will not exist outside. To overcome the "jump to label 'closeandexit'  error" it is necessary to set the "igpath" before line 276
+   //    TString igpath="/data03/Malakhov/pam9Malakhov/installed10/calib/orb-param/";
+   //  }
+   //  GM_ScanIGRF(glparam->PATH, &G0, &G1, &H1);
+   GM_ScanIGRF(dbc, &G0, &G1, &H1);
+   //cout << G0.element[0] << "\t" << G1.element[0] << "\t" << H1.element[0] << endl;
+   //cout << G0.element[5] << "\t" << G1.element[5] << "\t" << H1.element[5] << endl;
+   GM_SetEllipsoid(&Ellip);
+   // IGRF stuff moved inside run loop!
-   parerror=glparam->Query_GL_PARAM(1,301,dbc); // parameters stored in DB in GL_PRAM table
-   if ( parerror<0 ) {
-     code = parerror;
-     goto closeandexit;
-   };
-   ltp2 = (Int_t)(glparam->PATH+glparam->NAME).Length();
-   if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam->PATH+glparam->NAME).Data());
-   //
-   parerror=glparam2->Query_GL_PARAM(1,302,dbc); // parameters stored in DB in GL_PRAM table
-   if ( parerror<0 ) {
-     code = parerror;
-     goto closeandexit;
-   };
-   ltp3 = (Int_t)(glparam2->PATH+glparam2->NAME).Length();
-   if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam2->PATH+glparam2->NAME).Data());
-   //
-   initize_((char *)niente,&uno,(char *)(glparam->PATH+glparam->NAME).Data(),&ltp2,(char *)(glparam2->PATH+glparam2->NAME).Data(),&ltp3);
-   //
-   // End IGRF stuff//
-   //
    for (Int_t ip=0;ip<nz;ip++){
      zin[ip] = tof->GetZTOF(tof->GetToFPlaneID(ip));
    };
-Line 324 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 399 
 int OrbitalInfoCore(UInt_t run, TFile *f
        if ( verbose ) printf(" OrbitalInfo - ERROR: no tof tree\n");
        code = -900;
        goto closeandexit;
-     };
+     }
      ttof->SetBranchAddress("ToFLevel2",&tof);
      nevtofl2 = ttof->GetEntries();
-   };
+     ttrke = (TTree*)file->Get("Tracker");
+     if ( !ttrke ) {
+       if ( verbose ) printf(" OrbitalInfo - ERROR: no trk tree\n");
+       code = -903;
+       goto closeandexit;
+     }
+     ttrke->SetBranchAddress("TrkLevel2",&trke);
+     nevtrkl2 = ttrke->GetEntries();
+   }
    //
    // Let's start!
    //
-Line 416 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 500 
 int OrbitalInfoCore(UInt_t run, TFile *f
        //
        reprocall = true;
        //
-       if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing all runs\n");
+       if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing all runs\n Deleting old tree...\n");
        //
      } else {
        //
-Line 434 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 518 
 int OrbitalInfoCore(UInt_t run, TFile *f
        tempOrbitalInfo = OrbitalInfotrclone->CloneTree(-1,"fast");
        tempOrbitalInfo->SetName("OrbitalInfo-old");
        tempfile->Write();
+       tempOrbitalInfo->Delete();
        tempfile->Close();
      }
      //
      // Delete the old tree from old file and memory
      //
+     OrbitalInfotrclone->Clear();
      OrbitalInfotrclone->Delete("all");
      //
      if (verbose) printf(" ...done!\n");
-Line 484 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 570 
 int OrbitalInfoCore(UInt_t run, TFile *f
          //
        };
        if (verbose) printf(" Finished successful copying!\n");
      };
    };
    //
    //
-Line 495 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 581 
 int OrbitalInfoCore(UInt_t run, TFile *f
    // Loop over the run to be processed
    //
    for (UInt_t irun=0; irun < numbofrun; irun++){
+     L_QQ_Q_l_lower = new Quaternions();
+     RYPang_lower = new InclinationInfo();
+     L_QQ_Q_l_upper = new Quaternions();
+     RYPang_upper = new InclinationInfo();
      //
      // retrieve the first run ID to be processed using the RunInfo list
      //
-Line 557 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 649 
 int OrbitalInfoCore(UInt_t run, TFile *f
      //
      //    if ( !totevent ) goto closeandexit;
      // Open Level0 file
+     if ( l0File ) l0File->Close();
      l0File = new TFile(fname.Data());
      if ( !l0File ) {
        if ( debug ) printf(" OrbitalInfo - ERROR: problems opening Level0 file\n");
-Line 595 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 688 
 int OrbitalInfoCore(UInt_t run, TFile *f
        code = -12;
        goto closeandexit;
      };
+     //
+     // open IGRF files and do it only once if we are processing a full level2 file
+     //
+     if ( !igrfloaded ){
+       if ( l0head->GetEntry(runinfo->EV_FROM) > 0 ){
+         igrfloaded = true;
+         //
+         // absolute time of first event of the run (it should not matter a lot)
+         //
+         ph = eh->GetPscuHeader();
+         atime = dbtime->DBabsTime(ph->GetOrbitalTime());
+         parerror=glparam->Query_GL_PARAM(atime-anni5,301,dbc); // parameters stored in DB in GL_PRAM table
+         if ( parerror<0 ) {
+           code = parerror;
+           goto closeandexit;
+         }
+         ltp1 = (Int_t)(glparam->PATH+glparam->NAME).Length();
+         if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam->PATH+glparam->NAME).Data());
+         //
+         parerror=glparam2->Query_GL_PARAM(atime,301,dbc); // parameters stored in DB in GL_PRAM table
+         if ( parerror<0 ) {
+           code = parerror;
+           goto closeandexit;
+         }
+         ltp2 = (Int_t)(glparam2->PATH+glparam2->NAME).Length();
+         if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam2->PATH+glparam2->NAME).Data());
+         //
+         parerror=glparam3->Query_GL_PARAM(atime,302,dbc); // parameters stored in DB in GL_PRAM table
+         if ( parerror<0 ) {
+           code = parerror;
+           goto closeandexit;
+         }
+         ltp3 = (Int_t)(glparam3->PATH+glparam3->NAME).Length();
+         if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam3->PATH+glparam3->NAME).Data());
+         //
+         initize_((char *)(glparam->PATH+glparam->NAME).Data(),&ltp1,(char *)(glparam2->PATH+glparam2->NAME).Data(),&ltp2,(char *)(glparam3->PATH+glparam3->NAME).Data(),&ltp3);
+         //
+         if (debug) cout<<"initize: "<<(char *)(glparam->PATH+glparam->NAME).Data()<<"\t"<<(char *)(glparam2->PATH+glparam2->NAME).Data()<<"\t"<<(char *)(glparam3->PATH+glparam3->NAME).Data()<<endl;
+       }
+     }
+     //
+     // End IGRF stuff//
+     //
      //
      //     TTree *tp = (TTree*)l0File->Get("RunHeader");
      //     tp->SetBranchAddress("Header", &eH);
-Line 717 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 857 
 int OrbitalInfoCore(UInt_t run, TFile *f
  //    UInt_t mctren = 0;
  //    UInt_t mcreen = 0;
-     UInt_t numrec = 0;
+ //    UInt_t numrec = 0;
      //
-     Double_t upperqtime = 0;
+     //    Double_t upperqtime = 0;
      Double_t lowerqtime = 0;
- //    Double_t incli = 0;
+     //    Double_t incli = 0;
- //    oi = 0;
+     //    oi = 0;
- //    UInt_t ooi = 0;
+     //    UInt_t ooi = 0;
      //
      // init quaternions information from mcmd-packets
      //
      Bool_t isf = true;
- //    Int_t fgh = 0;
+     //    Int_t fgh = 0;
      vector<Float_t> q0;
      vector<Float_t> q1;
-Line 743 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 883 
 int OrbitalInfoCore(UInt_t run, TFile *f
      Int_t nt = 0;
-     //init sine-function interpolation
-     //cout<<"Sine coeficient initialisation..."<<endl;
-     vector<Sine> q0sine;
-     vector<Sine> q1sine;
-     vector<Sine> q2sine;
-     vector<Sine> q3sine;
-     vector<Sine> Yawsine;
-     /*TH2F* q0testing = new TH2F();
-       TH2F* q1testing = new TH2F();
-       TH2F* q2testing = new TH2F();
-       TH2F* q3testing = new TH2F();
-       TH2F* Pitchtesting = new TH2F();
-     */
      UInt_t must = 0;
      //
-Line 803 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 928 
 int OrbitalInfoCore(UInt_t run, TFile *f
            if ( verbose ) printf(" OrbitalInfo - ERROR: no tof events with entry = %i in Level2 file\n",itr);
            if ( debug ) printf(" nobefrun %u re %u evfrom %u jumped %u reprocall %i \n",nobefrun,re,evfrom,jumped,reprocall);
            l0File->Close();
-           code = -901;
+           code = -904;
            goto closeandexit;
          };
          //
          tof->Clear();
          //
-         if ( ttof->GetEntry(itr) <= 0 ) throw -36;
+         if ( ttof->GetEntry(itr) <= 0 ){
+          if ( verbose ) printf(" problems with tof tree entries... entry = %i in Level2 file\n",itr);
+          if ( verbose ) printf(" nobefrun %u re %u evfrom %u jumped %u reprocall %i \n",nobefrun,re,evfrom,jumped,reprocall);
+          throw -36;
+         }
          //
-       };
+       }
+       //
+       // retrieve tracker informations
+       //
+       if ( !standalone ){
+         if ( itr > nevtrkl2 ){
+           if ( verbose ) printf(" OrbitalInfo - ERROR: no trk events with entry = %i in Level2 file\n",itr);
+           if ( debug ) printf(" nobefrun %u re %u evfrom %u jumped %u reprocall %i \n",nobefrun,re,evfrom,jumped,reprocall);
+           l0File->Close();
+           code = -905;
+           goto closeandexit;
+         };
+         //
+         trke->Clear();
+         //
+         if ( ttrke->GetEntry(itr) <= 0 ) throw -36;
+         //
+       }
        //
        procev++;
        //
-Line 823 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 971 
 int OrbitalInfoCore(UInt_t run, TFile *f
        OrbitalInfoTrkVar *t_orb = new OrbitalInfoTrkVar();
        if( !(orbitalinfo->OrbitalInfoTrk) ) orbitalinfo->OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2);
        TClonesArray &tor = *orbitalinfo->OrbitalInfoTrk;
+       // Geomagnetic coordinates calculation variables
+       GMtype_CoordSpherical CoordSpherical, DipoleSpherical;
+       GMtype_CoordCartesian CoordCartesian, DipoleCartesian;
+       GMtype_Model Model;
+       GMtype_Pole Pole;
        //
        // Fill OBT, pkt_num and absTime
        //
-Line 852 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1007 
 int OrbitalInfoCore(UInt_t run, TFile *f
              + (month*31.+ (float) day)/365.
              + (hour*3600.+min*60.+(float)sec)/(24.*3600.*365.);
            //
            if ( debug ) printf(" %i compute magnetic dipole moment get dipole moment for year\n",procev);
+           if ( debug ) printf(" %i jyear %f dimo %f \n",procev,jyear,dimo);
            feldcof_(&jyear, &dimo); // get dipole moment for year
            if ( debug ) printf(" %i compute magnetic dipole moment end\n",procev);
+           GM_TimeAdjustCoefs(year, jyear, G0, G1, H1, &Model);
+           GM_PoleLocation(Model, &Pole);
          } else {
            code = -56;
            goto closeandexit;
-Line 864 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1024 
 int OrbitalInfoCore(UInt_t run, TFile *f
        //
        cOrbit orbits(*gltle->GetTle());
        //
-       if ( debug ) printf(" I am Here \n");
-       //
        // synchronize with quaternions data
        //
        if ( isf && neventsm>0 ){
-Line 873 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1031 
 int OrbitalInfoCore(UInt_t run, TFile *f
          // First event
          //
          isf = false;
-         upperqtime = atime;
+         //      upperqtime = atime;
          lowerqtime = runinfo->RUNHEADER_TIME;
          for ( ik = 0; ik < neventsm; ik++){  //number of macrocommad packets
            if ( ch->GetEntry(ik) <= 0 ) throw -36;
            tmpSize = mcmdev->Records->GetEntries();
-           numrec = tmpSize;
+           //      numrec = tmpSize;
+           if ( debug ) cout << "packet number " << ik <<"\tnumber of subpackets is " << tmpSize << endl;
            for (Int_t j3 = 0;j3<tmpSize;j3++){  //number of subpackets
-             if ( debug ) printf(" ik %i j3 %i eh eh eh \n",ik,j3);
              mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(j3);
              if ( mcmdrc ){ // missing inclination bug [8RED 090116]
+               if ( debug ) printf(" pluto \n");
                if ((int)mcmdrc->ID1 == 226 && mcmdrc->Mcmd_Block_crc_ok == 1){ //Check that it is Inclination Packet
-                 L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
+                L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
                  for (UInt_t ui = 0; ui < 6; ui++){
                    if (ui>0){
                      if (L_QQ_Q_l_upper->time[ui]>L_QQ_Q_l_upper->time[0]){
+                       if ( debug ) printf(" here1 %i \n",ui);
                        Double_t u_time = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));
                        Int_t recSize = recqtime.size();
-                       for(Int_t mu = nt;mu<recSize;mu++){
+                       if(lowerqtime > recqtime[recSize-1]){
-                         if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){
+                          // to avoid interpolation between bad quaternions arrays
-                           nt=mu;
+                          if(sqrt(pow(L_QQ_Q_l_upper->quat[ui][0],2)+pow(L_QQ_Q_l_upper->quat[ui][1],2)+pow(L_QQ_Q_l_upper->quat[ui][2],2)+pow(L_QQ_Q_l_upper->quat[ui][3],2))>0.99999){
-                           Int_t sizeqmcmd = qtime.size();
-                           inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
-                           qtime[sizeqmcmd]=recqtime[mu];
-                           q0[sizeqmcmd]=recq0[mu];
-                           q1[sizeqmcmd]=recq1[mu];
-                           q2[sizeqmcmd]=recq2[mu];
-                           q3[sizeqmcmd]=recq3[mu];
-                           qmode[sizeqmcmd]=-10;
-                           orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi);
-                           RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,recq0[mu],recq1[mu],recq2[mu],recq3[mu]);
-                           qRoll[sizeqmcmd]=RYPang_upper->Kren;
-                           qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
-                           qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
-                         }
-                         if(recqtime[mu]>=u_time){
                            Int_t sizeqmcmd = qtime.size();
                            inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
                            qtime[sizeqmcmd]=u_time;
-Line 922 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1067 
 int OrbitalInfoCore(UInt_t run, TFile *f
                            qRoll[sizeqmcmd]=RYPang_upper->Kren;
                            qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
                            qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
-                           break;
+                          }
+                       }
+                       for(Int_t mu = nt;mu<recSize;mu++){
+                         if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){
+                           if(sqrt(pow(recq0[mu],2)+pow(recq1[mu],2)+pow(recq2[mu],2)+pow(recq3[mu],2))>0.99999){
+                             nt=mu;
+                             Int_t sizeqmcmd = qtime.size();
+                             inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
+                             qtime[sizeqmcmd]=recqtime[mu];
+                             q0[sizeqmcmd]=recq0[mu];
+                             q1[sizeqmcmd]=recq1[mu];
+                             q2[sizeqmcmd]=recq2[mu];
+                             q3[sizeqmcmd]=recq3[mu];
+                             qmode[sizeqmcmd]=-10;
+                             orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi);
+                             RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,recq0[mu],recq1[mu],recq2[mu],recq3[mu]);
+                             qRoll[sizeqmcmd]=RYPang_upper->Kren;
+                             qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
+                             qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
+                           }
+                         }
+                         if(recqtime[mu]>=u_time){
+                           if(sqrt(pow(L_QQ_Q_l_upper->quat[ui][0],2)+pow(L_QQ_Q_l_upper->quat[ui][1],2)+pow(L_QQ_Q_l_upper->quat[ui][2],2)+pow(L_QQ_Q_l_upper->quat[ui][3],2))>0.99999){
+                             Int_t sizeqmcmd = qtime.size();
+                             inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
+                             qtime[sizeqmcmd]=u_time;
+                             q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][0];
+                             q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][1];
+                             q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][2];
+                             q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][3];
+                             qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui);
+                             lowerqtime = u_time;
+                             orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi);
+                             RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,L_QQ_Q_l_upper->quat[ui][0],L_QQ_Q_l_upper->quat[ui][1],L_QQ_Q_l_upper->quat[ui][2],L_QQ_Q_l_upper->quat[ui][3]);
+                             qRoll[sizeqmcmd]=RYPang_upper->Kren;
+                             qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
+                             qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
+                             break;
+                           }
                          }
                        }
                      }
                    }else{
+                     if ( debug ) printf(" here2 %i \n",ui);
                      Double_t u_time = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
                      if(lowerqtime>u_time)nt=0;
                      Int_t recSize = recqtime.size();
-                     for(Int_t mu = nt;mu<recSize;mu++){
+                     if(lowerqtime > recqtime[recSize-1]){
-                       if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){
+                       if(sqrt(pow(L_QQ_Q_l_upper->quat[ui][0],2)+pow(L_QQ_Q_l_upper->quat[ui][1],2)+pow(L_QQ_Q_l_upper->quat[ui][2],2)+pow(L_QQ_Q_l_upper->quat[ui][3],2))>0.99999){
-                         nt=mu;
-                         Int_t sizeqmcmd = qtime.size();
-                         inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
-                         qtime[sizeqmcmd]=recqtime[mu];
-                         q0[sizeqmcmd]=recq0[mu];
-                         q1[sizeqmcmd]=recq1[mu];
-                         q2[sizeqmcmd]=recq2[mu];
-                         q3[sizeqmcmd]=recq3[mu];
-                         qmode[sizeqmcmd]=-10;
-                         orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi);
-                         RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,recq0[mu],recq1[mu],recq2[mu],recq3[mu]);
-                         qRoll[sizeqmcmd]=RYPang_upper->Kren;
-                         qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
-                         qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
-                       }
-                       if(recqtime[mu]>=u_time){
                          Int_t sizeqmcmd = qtime.size();
                          inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
                          qtime[sizeqmcmd]=u_time;
-Line 962 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1130 
 int OrbitalInfoCore(UInt_t run, TFile *f
                          qRoll[sizeqmcmd]=RYPang_upper->Kren;
                          qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
                          qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
-                         CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
+                       }
-                         break;
+                     }
+                     for(Int_t mu = nt;mu<recSize;mu++){
+                       if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){
+                          if(sqrt(pow(recq0[mu],2)+pow(recq1[mu],2)+pow(recq2[mu],2)+pow(recq3[mu],2))>0.99999){
+                            nt=mu;
+                            Int_t sizeqmcmd = qtime.size();
+                            inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
+                            qtime[sizeqmcmd]=recqtime[mu];
+                            q0[sizeqmcmd]=recq0[mu];
+                            q1[sizeqmcmd]=recq1[mu];
+                            q2[sizeqmcmd]=recq2[mu];
+                            q3[sizeqmcmd]=recq3[mu];
+                            qmode[sizeqmcmd]=-10;
+                            orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi);
+                            RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,recq0[mu],recq1[mu],recq2[mu],recq3[mu]);
+                            qRoll[sizeqmcmd]=RYPang_upper->Kren;
+                            qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
+                            qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
+                          }
+                       }
+                       if(recqtime[mu]>=u_time){
+                          if(sqrt(pow(L_QQ_Q_l_upper->quat[0][0],2)+pow(L_QQ_Q_l_upper->quat[0][1],2)+pow(L_QQ_Q_l_upper->quat[0][2],2)+pow(L_QQ_Q_l_upper->quat[0][3],2))>0.99999){
+                            Int_t sizeqmcmd = qtime.size();
+                            inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
+                            qtime[sizeqmcmd]=u_time;
+                            q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][0];
+                            q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][1];
+                            q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][2];
+                            q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][3];
+                            qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui);
+                            lowerqtime = u_time;
+                            orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi);
+                            RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,L_QQ_Q_l_upper->quat[0][0],L_QQ_Q_l_upper->quat[0][1],L_QQ_Q_l_upper->quat[0][2],L_QQ_Q_l_upper->quat[0][3]);
+                            qRoll[sizeqmcmd]=RYPang_upper->Kren;
+                            qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
+                            qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
+                            CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
+                            break;
+                          }
                        }
                      }
                    }
                  }
                }
              }
+             //if ( debug ) cout << "subpacket " << j3 << "\t qtime = " << qtime[qtime.size()-1] << endl;
            }
          }
+         if(qtime.size()==0){                            // in case if no orientation information in data
+           if ( debug ) cout << "qtime.size() = 0" << endl;
+           for(UInt_t my=0;my<recqtime.size();my++){
+             if(sqrt(pow(recq0[my],2)+pow(recq1[my],2)+pow(recq2[my],2)+pow(recq3[my],2))>0.99999){
+               Int_t sizeqmcmd = qtime.size();
+               inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
+               qtime[sizeqmcmd]=recqtime[my];
+               q0[sizeqmcmd]=recq0[my];
+               q1[sizeqmcmd]=recq1[my];
+               q2[sizeqmcmd]=recq2[my];
+               q3[sizeqmcmd]=recq3[my];
+               qmode[sizeqmcmd]=-10;
+               orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi);
+               RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,recq0[my],recq1[my],recq2[my],recq3[my]);
+               qRoll[sizeqmcmd]=RYPang_upper->Kren;
+               qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
+               qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
+             }
+           }
+         }
-         sineparam(q0sine,qtime,q0,qRoll,qPitch,0.58);
+         if ( debug ) printf(" puffi \n");
-         sineparam(q1sine,qtime,q1,qRoll,qPitch,0.79);
-         sineparam(q2sine,qtime,q2,qRoll,qPitch,0.79);
-         sineparam(q3sine,qtime,q3,qRoll,qPitch,0.58);
-         sineparam(Yawsine,qtime,qYaw,qRoll,qPitch,4);
          Double_t tmin = 9999999999.;
          Double_t tmax = 0.;
          for(UInt_t tre = 0;tre<qtime.size();tre++){
            if(qtime[tre]>tmax)tmax = qtime[tre];
            if(qtime[tre]<tmin)tmin = qtime[tre];
          }
+         // sorting quaternions by time
-         //q0testing->SetName("q0testing");
+        Bool_t t = true;
-         //q1testing->SetName("q1testing");
+         while(t){
-         //q2testing->SetName("q2testing");
+          t=false;
-         //q3testing->SetName("q3testing");
+           for(UInt_t i=0;i<qtime.size()-1;i++){
+             if(qtime[i]>qtime[i+1]){
- //      Int_t ss=10.*(tmax-tmin);
+               Double_t tmpr = qtime[i];
-         //q0testing->SetBins(ss,tmin,tmax,1000,-1.,1.);
+               qtime[i]=qtime[i+1];
-         //Pitchtesting->SetBins(ss,tmin,tmax,1000,-40.,40.);
+               qtime[i+1] = tmpr;
+               tmpr = q0[i];
- //      for(Int_t tre = 0;tre<qtime.size();tre++){
+               q0[i]=q0[i+1];
-           //cout<<"q0["<<tre<<" = "<<q0[tre]<<endl;
+               q0[i+1] = tmpr;
-           //q0testing->Fill(qtime[tre],q0[tre]);
+               tmpr = q1[i];
-           //q1testing->Fill(qtime[tre],q1[tre]);
+               q1[i]=q1[i+1];
-           //Pitchtesting->Fill(qtime[tre],qPitch[tre],100);
+               q1[i+1] = tmpr;
-           //if(qmode[tre] == -10)Pitchtesting->Fill(qtime[tre],10,100);
+               tmpr = q2[i];
-           //q2testing->Fill(qtime[tre],q2[tre],100);
+               q2[i]=q2[i+1];
-           //q3testing->Fill(qtime[tre],q3[tre],100);
+               q2[i+1] = tmpr;
- //      }
+               tmpr = q3[i];
+               q3[i]=q3[i+1];
-         //for(Int_t tre=0;tre<q0sine.size();tre++)cout<<q1sine[tre].A<<"*sin("<<q1sine[tre].b<<"x+"<<q1sine[tre].c<<")\t time start: "<<q1sine[tre].startPoint<<"\ttime end: "<<q1sine[tre].finishPoint<<endl;
+               q3[i+1] = tmpr;
-         //for(Int_t tre=0;tre<q0sine.size();tre++)cout<<q1sine[tre].A<<"*sin("<<q1sine[tre].b<<"x+"<<q1sine[tre].c<<")\t time start: "<<q0sine[tre].startPoint<<"\ttime end: "<<q0sine[tre].finishPoint<<endl;
+               tmpr = qRoll[i];
+               qRoll[i]=qRoll[i+1];
+               qRoll[i+1] = tmpr;
+               tmpr = qYaw[i];
+               qYaw[i]=qYaw[i+1];
+               qYaw[i+1] = tmpr;
+               tmpr = qPitch[i];
+               qPitch[i]=qPitch[i+1];
+               qPitch[i+1] = tmpr;
+                 t=true;
+             }
+           }
+         }
+         if ( debug ){
+           cout << "we have loaded quaternions: size of quaternions set is "<< qtime.size() << endl;
+          for(UInt_t i=0;i<qtime.size();i++) cout << qtime[i] << "\t";
+           cout << endl << endl;
+           Int_t lopu;
+           cin >> lopu;
+        }
        } // if we processed first event
        //Filling Inclination information
        Double_t incli = 0;
-       for(UInt_t mu = must;mu<qtime.size()-1;mu++){
+       if ( qtime.size() > 1 ){
-         if(qtime[mu+1]>qtime[mu]){
+         if ( debug ) cout << "ok quaternions is exist and mu = " << must << endl;
-           if(atime<=qtime[mu+1] && atime>=qtime[mu]){
+         if ( debug ) cout << "qtimes[ " << qtime[0] << " , " << qtime[qtime.size()-1] << " ]\tatime = "<<atime<<endl;
-             must = mu;
+         for(UInt_t mu = must;mu<qtime.size()-1;mu++){
-             incli = (qPitch[mu+1]-qPitch[mu])/(qtime[mu+1]-qtime[mu]);
+           if ( debug ) printf(" ??grfuffi %i sixe %i must %i \n",mu,qtime.size()-1,must);
-             orbitalinfo->theta =  incli*atime+qPitch[mu+1]-incli*qtime[mu+1];
+           if(qtime[mu+1]>qtime[mu]){
-             incli = (qRoll[mu+1]-qRoll[mu])/(qtime[mu+1]-qtime[mu]);
+             if ( debug ) cout << "qtime[" << mu << "] = " << qtime[mu] << "\tqtime[" << mu+1 << "] = " << qtime[mu+1] << "\tatime = " << atime << endl;
-             orbitalinfo->etha =  incli*atime+qRoll[mu+1]-incli*qtime[mu+1];
+             if(atime<=qtime[mu+1] && atime>=qtime[mu]){
-             incli = (qYaw[mu+1]-qYaw[mu])/(qtime[mu+1]-qtime[mu]);
+               if ( debug ) cout << "here we have found proper quaternions for interpolation: mu = "<<mu<<endl;
-             orbitalinfo->phi =  incli*atime+qYaw[mu+1]-incli*qtime[mu+1];
+               must = mu;
+               incli = (qPitch[mu+1]-qPitch[mu])/(qtime[mu+1]-qtime[mu]);
-             incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
+               orbitalinfo->theta =  incli*atime+qPitch[mu+1]-incli*qtime[mu+1];
-             orbitalinfo->q0t =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
+               incli = (qRoll[mu+1]-qRoll[mu])/(qtime[mu+1]-qtime[mu]);
-             incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
+               orbitalinfo->etha =  incli*atime+qRoll[mu+1]-incli*qtime[mu+1];
-             orbitalinfo->q1t =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
+               incli = (qYaw[mu+1]-qYaw[mu])/(qtime[mu+1]-qtime[mu]);
-             incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
+               orbitalinfo->phi =  incli*atime+qYaw[mu+1]-incli*qtime[mu+1];
-             orbitalinfo->q2t =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
-             incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
+               incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
-             orbitalinfo->q3t =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
+               orbitalinfo->q0 =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
+               incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
-             orbitalinfo->TimeGap = qtime[mu+1]-qtime[mu];
+               orbitalinfo->q1 =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
-             orbitalinfo->mode = qmode[mu+1];
+               incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
-             if(qmode[mu+1]==-10) orbitalinfo->R10r = true;else orbitalinfo->R10r = false;
+               orbitalinfo->q2 =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
-             if(qmode[mu+1]==-10 || qmode[mu+1]==0 || qmode[mu+1]==1 || qmode[mu+1]==3 || qmode[mu+1]==4 || qmode[mu+1]==6){
+               incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
-               //linear interpolation
+               orbitalinfo->q3 =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
-               incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
+               Float_t tg = (qtime[mu+1]-qtime[mu])/1000.;
-               orbitalinfo->q0 =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
+               if(tg>=1) tg=0.00;
-               incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
+               orbitalinfo->TimeGap = TMath::Min(TMath::Abs(qtime[mu+1])-atime,TMath::Abs(atime-qtime[mu]))+tg;//qtime[mu+1]-qtime[mu];
-               orbitalinfo->q1 =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
+               orbitalinfo->mode = qmode[mu+1];
-               incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
-               orbitalinfo->q2 =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
+               //if(atime==qtime[mu] || atime==qtime[mu+1]) orbitalinfo->qkind = 0; else orbitalinfo->qkind=1;
-               incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
+               //if(qmode[mu+1]==-10) orbitalinfo->R10r = true;else orbitalinfo->R10r = false;
-               orbitalinfo->q3 =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
+               if ( debug ) printf(" grfuffi4 %i \n",mu);
-             }else{
-               //sine interpolation
+               break;
-               for(UInt_t mt=0;mt<q0sine.size();mt++){
+             }
-                 if(atime<=q0sine[mt].finishPoint && atime>=q0sine[mt].startPoint){
+           }
-                   if(!q0sine[mt].NeedFit)orbitalinfo->q0=q0sine[mt].A*sin(q0sine[mt].b*atime+q0sine[mt].c);else{
+         }
-                     incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
-                     orbitalinfo->q0 =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
-                   }
-                 }
-                 if(atime<=q1sine[mt].finishPoint && atime>=q1sine[mt].startPoint){
-                   if(!q1sine[mt].NeedFit)orbitalinfo->q1=q1sine[mt].A*sin(q1sine[mt].b*atime+q1sine[mt].c);else{
-                     incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
-                     orbitalinfo->q1 =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
-                   }
-                 }
-                 if(atime<=q2sine[mt].finishPoint && atime>=q2sine[mt].startPoint){
-                   if(!q2sine[mt].NeedFit)orbitalinfo->q2=q0sine[mt].A*sin(q2sine[mt].b*atime+q2sine[mt].c);else{
-                     incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
-                     orbitalinfo->q2 =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
-                   }
-                 }
-                 if(atime<=q3sine[mt].finishPoint && atime>=q3sine[mt].startPoint){
-                   if(!q3sine[mt].NeedFit)orbitalinfo->q3=q0sine[mt].A*sin(q3sine[mt].b*atime+q3sine[mt].c);else{
-                     incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
-                     orbitalinfo->q3 =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
-                   }
-                 }
-                 if(atime<=Yawsine[mt].finishPoint && atime>=Yawsine[mt].startPoint){
-                   if(!Yawsine[mt].NeedFit)orbitalinfo->phi=Yawsine[mt].A*sin(Yawsine[mt].b*atime+Yawsine[mt].c);else{
-                     incli = (qYaw[mu+1]-qYaw[mu])/(qtime[mu+1]-qtime[mu]);
-                     orbitalinfo->phi =  incli*atime+qYaw[mu+1]-incli*qtime[mu+1];
-                   }
-                 }
-               }
-             }
-             //q0testing->Fill(atime,orbitalinfo->q0,100);
-             //q1testing->Fill(atime,orbitalinfo->q1,100);
-             //Pitchtesting->Fill(atime,orbitalinfo->etha);
-             //q2testing->Fill(atime,orbitalinfo->q2);
-             //q3testing->Fill(atime,orbitalinfo->q3);
-             break;
-           }
-         }
        }
+       if ( debug ) printf(" grfuffi5  \n");
        //
        // ops no inclination information
        //
        if ( orbitalinfo->q0< -999 || orbitalinfo->q1 < -999 || orbitalinfo->q2 < -999 || orbitalinfo->q3 < -999 || orbitalinfo->q0 != orbitalinfo->q0 || orbitalinfo->q1 != orbitalinfo->q1 || orbitalinfo->q2 != orbitalinfo->q2 || orbitalinfo->q3 != orbitalinfo->q3 ){
+         if ( debug ) cout << "ops no iclination information" << endl;
          orbitalinfo->mode = 10;
          orbitalinfo->q0 = -1000.;
          orbitalinfo->q1 = -1000.;
-Line 1101 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1311 
 int OrbitalInfoCore(UInt_t run, TFile *f
          orbitalinfo->etha = -1000.;
          orbitalinfo->phi = -1000.;
          orbitalinfo->theta = -1000.;
-       };
+         orbitalinfo->TimeGap = -1000.;
+         //orbitalinfo->qkind = -1000;
+         //      if ( debug ){
+         //        Int_t lopu;
+         //         cin >> lopu;
+         //      }
+         if ( debug ) printf(" grfuffi6 \n");
+       }
        //
+       if ( debug ) printf(" filling \n");
        // #########################################################################################################################
        //
        // fill orbital positions
-Line 1113 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1332 
 int OrbitalInfoCore(UInt_t run, TFile *f
        lon = (coo.m_Lon > M_PI) ? rad2deg(coo.m_Lon - 2*M_PI) : rad2deg(coo.m_Lon);
        lat = rad2deg(coo.m_Lat);
        alt = coo.m_Alt;
-       //
+       cOrbit orbits2(*gltle->GetTle());
+       orbits2.getPosition((double) (atime - gltle->GetFromTime())/60., &eCi);
+       //      Float_t x=eCi.getPos().m_x;
+       //      Float_t y=eCi.getPos().m_y;
+       //      Float_t z=eCi.getPos().m_z;
+       TVector3 V(eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z);
+       TVector3 Pos(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z);
+       Float_t dlon=Pos.Phi()*TMath::RadToDeg()-lon;
+       Pos.RotateZ(-dlon*TMath::DegToRad());
+       V.RotateZ(-dlon*TMath::DegToRad());
+       Float_t diro;
+       if(V.Z()>0) diro=1; else diro=-1;
+       // 10REDNEW
+       Int_t errq=0;
+       Int_t azim=0;;
+       for(UInt_t mu = must;mu<RTtime2.size()-1;mu++){
+         if(atime<=RTtime2[mu] && atime>=RTtime1[mu]){
+           errq=RTerrq[mu];
+           azim=RTazim[mu];
+         }
+       }
+       orbitalinfo->errq = errq;
+       orbitalinfo->azim = azim;
+       orbitalinfo->qkind = 0;
+       if ( debug ) printf(" coord done \n");
        if( lon<180 && lon>-180 && lat<90 && lat>-90 && alt>0 ){
          //
          orbitalinfo->lon = lon;
          orbitalinfo->lat = lat;
-         orbitalinfo->alt = alt ;
+         orbitalinfo->alt = alt;
+         orbitalinfo->V = V;
+         //      GMtype_CoordGeodetic  location;
+         location.lambda = lon;
+         location.phi = lat;
+         location.HeightAboveEllipsoid = alt;
+         GM_GeodeticToSpherical(Ellip, location, &CoordSpherical);
+         GM_SphericalToCartesian(CoordSpherical,  &CoordCartesian);
+         GM_EarthCartToDipoleCartCD(Pole, CoordCartesian, &DipoleCartesian);
+         GM_CartesianToSpherical(DipoleCartesian, &DipoleSpherical);
+         orbitalinfo->londip = DipoleSpherical.lambda;
+         orbitalinfo->latdip = DipoleSpherical.phig;
+         if(debug)cout<<"geodetic:\t"<<lon<<"\t"<<lat<<"\tgeomagnetic:\t"<<orbitalinfo->londip<<"\t"<<orbitalinfo->latdip<<endl;
          //
          // compute mag field components and L shell.
          //
+         if ( debug ) printf(" call igrf feldg \n");
          feldg_(&lat, &lon, &alt, &bnorth, &beast, &bdown, &babs);
+         if ( debug ) printf(" call igrf shellg \n");
          shellg_(&lat, &lon, &alt, &dimo, &xl, &icode, &bab1);
+         if ( debug ) printf(" call igrf findb \n");
          findb0_(&stps, &bdel, &value, &bequ, &rr0);
          //
+         if ( debug ) printf(" done igrf \n");
          orbitalinfo->Bnorth = bnorth;
          orbitalinfo->Beast = beast;
          orbitalinfo->Bdown = bdown;
          orbitalinfo->Babs = babs;
+         orbitalinfo->M = dimo;
          orbitalinfo->BB0 = babs/bequ;
          orbitalinfo->L = xl;
          // Set Stormer vertical cutoff using L shell.
-         orbitalinfo->cutoffsvl = 14.9/(xl*xl);
+         orbitalinfo->cutoffsvl = 14.295 / (xl*xl); //
+         if(debug)cout << "L = " << xl << "\tM = " << dimo << "\tvertical cutoff:  "<< orbitalinfo->cutoffsvl << endl;
+         /*
+           ---------- Forwarded message ----------
+           Date: Wed, 09 May 2012 12:16:47 +0200
+           From: Alessandro Bruno <alessandro.bruno@ba.infn.it>
+           To: Mirko Boezio <mirko.boezio@ts.infn.it>
+           Cc: Francesco S. Cafagna <Francesco.Cafagna@ba.infn.it>
+           Subject: St�rmer vertical cutoff
+           Ciao Mirko,
+           volevo segnalarti che il valore dello St�rmer vertical cutoff nel Level2 �
+           sovrastimato di circa il 4%.
+           Dopo un'approfondita analisi con l'IGRF-05 abbiamo ricavano un valore pari
+           a: 14.295 / L^2 anzich� 14.9 / L^2, valore obsoleto in quanto riferito agli
+           anni '50.
+         */
+         //14.9/(xl*xl);
+         orbitalinfo->igrf_icode = icode;
          //
-       };
+       }
        //
        if ( debug ) printf(" pitch angle \n");
        //
        // pitch angles
        //
-       if ( orbitalinfo->mode != 10 && orbitalinfo->mode != 5 && orbitalinfo->mode !=7 && orbitalinfo->mode != 9 ){
+       if( orbitalinfo->TimeGap>0){
          //
-         Float_t Bx = -orbitalinfo->Bdown;                       //don't need for PamExp ExpOnly for all geography areas
+         if ( debug ) printf(" timegap %f \n",orbitalinfo->TimeGap);
-         Float_t By = orbitalinfo->Beast;                        //don't need for PamExp ExpOnly for all geography areas
+         Float_t Bx = -orbitalinfo->Bdown;
-         Float_t Bz = orbitalinfo->Bnorth;                       //don't need for PamExp ExpOnly for all geography areas
+         Float_t By = orbitalinfo->Beast;
-         //
+         Float_t Bz = orbitalinfo->Bnorth;
-         TMatrixD Fij = PO->ECItoGreenwich(PO->QuatoECI(orbitalinfo->q0,orbitalinfo->q1,orbitalinfo->q2,orbitalinfo->q3),orbitalinfo->absTime);
-         TMatrixD Dij = PO->GreenwichtoGEO(orbitalinfo->lat,orbitalinfo->lon,Fij);
+         TMatrixD Qiji(3,3);
+         TMatrixD Qij = PO->QuatoECI(orbitalinfo->q0,orbitalinfo->q1,orbitalinfo->q2,orbitalinfo->q3);
+         TMatrixD Dij = PO->ECItoGEO(Qij,orbitalinfo->absTime,orbitalinfo->lat,orbitalinfo->lon);
+ //10REDNEW
+         /* If initial orientation data have reason to be inaccurate */
+         Double_t tg = 0;
+         if ( debug ) cout<<modf(orbitalinfo->TimeGap,&tg)<<endl;
+ //      if(orbitalinfo->TimeGap>0 && errq==0 && azim==0){               // 10RED CHECK  (comparison between three metod of recovering orientation)
+         if(((orbitalinfo->TimeGap>60.0 && TMath::Abs(orbitalinfo->etha)>0.5) || errq!=0 || modf(orbitalinfo->TimeGap,&tg)*1000>700 || modf(orbitalinfo->TimeGap,&tg)*1000==0.0 ) && azim==0){           //Standard condition to use this;               One of these two cases should be commented
+         /*  found in Rotation Table this data for this time interval*/
+         if(atime<RTtime1[0])
+           orbitalinfo->azim = 5;        //means that RotationTable no started yet
+        else{
+           for(UInt_t mu = must;mu<RTtime2.size()-1;mu++){
+             if(atime<=RTtime2[mu] && atime>=RTtime1[mu]){
+                 // search for angle betwean velosity and direction to north in tangential to Earth surfase plane in satellite position
+               Double_t tlat=orbitalinfo->lat;
+ /*            Double_t phint=(163.7-0.0002387*tlat-0.005802*tlat*tlat-0.005802e-7*tlat*tlat*tlat-1.776e-6*tlat*tlat*tlat*tlat+1.395e-10*tlat*tlat*tlat*tlat*tlat);
+               Double_t phin=TMath::Abs(90.0*(1+diro)-phint);
+               Double_t phi=TMath::Abs(90.0*(1-diro)-TMath::RadToDeg()*atan(TMath::Abs(tan(TMath::DegToRad()*phin))/sqrt(1+pow(tan(TMath::DegToRad()*tlat),2))));
+                 //Get vectors of Satellite reference frame axis in GEO in satndard case (No rotations, all Euler angles equals to 0)
+               TVector3 XDij(0,sin(TMath::DegToRad()*phi),cos(TMath::DegToRad()*phi));
+               TVector3 YDij(1,0,0);
+               TVector3 ZDij(0,sin(TMath::DegToRad()*(phi+90)),cos(TMath::DegToRad()*(phi+90.0)));
+                 //Get Vectors to rotate about
+               TVector3 B1 = V;
+               B1.RotateZ(-lon*TMath::DegToRad());
+               B1.RotateY(lat*TMath::DegToRad());
+               Float_t elipangle=TMath::ACos((pow(B1.Y(),2)+pow(B1.Z(),2))/B1.Mag()/sqrt(pow(B1.Y(),2)+pow(B1.Z(),2)));
+               TVector3 Tre(0,B1.Y(),B1.Z());
+               if(B1.X()<0) elipangle=-elipangle;
+               TVector3 Vperp=B1;                // axis to rotate around initial Dij on ellip and spitch angles
+               Vperp.RotateX(TMath::Pi()/2.);
+               Vperp.SetX(0);
+ */            Double_t kar=(RTbank2[mu]-RTbank1[mu])/(RTtime2[mu]-RTtime1[mu]);
+               Double_t bak=RTbank1[mu]-kar*RTtime1[mu];
+               Double_t bank=kar*atime+bak;
+               Float_t spitch = 0.00001;  // temprary not zero to avoid problem with tranzition from Euler angles to orientation matrix
+                 //Estimations of pitch angle of satellite
+               if(TMath::Abs(bank)>0.7){
+                  Float_t spitch1=TMath::DegToRad()*0.7*RTdir1[mu];
+                  Float_t spitch2=TMath::DegToRad()*0.7*RTdir2[mu];
+                  Float_t kva=(spitch2-spitch1)/(RTtime2[mu]-RTtime1[mu]);
+                  Float_t bva=spitch1-kva*RTtime1[mu];
+                  spitch=kva*atime+bva;
+               }
+ /*            //spitch=0.0;
+               //Rotations future Dij matrix on ellip and spitch angles
+               XDij.Rotate(-elipangle-spitch,Vperp);
+               YDij.Rotate(-elipangle-spitch,Vperp);
+               ZDij.Rotate(-elipangle-spitch,Vperp);
+                 //Rotation on bank angle;
+               if(TMath::Abs(bank)>0.5){
+                  XDij.Rotate(TMath::DegToRad()*bank,B1);
+                  YDij.Rotate(TMath::DegToRad()*bank,B1);
+                  ZDij.Rotate(TMath::DegToRad()*bank,B1);
+               }
+               Dij(0,0)=XDij.X(); Dij(1,0)=XDij.Y(); Dij(2,0)=XDij.Z();
+               Dij(0,1)=YDij.X(); Dij(1,1)=YDij.Y(); Dij(2,1)=YDij.Z();
+               Dij(0,2)=ZDij.X(); Dij(1,2)=ZDij.Y(); Dij(2,2)=ZDij.Z();
+ */
+               //Calculate Yaw angle accordingly with fit, see picture FitYaw.jpg
+               Double_t yaw=0.00001;  // temprary not zero to avoid problem with tranzition from Euler angles to orientation matrix
+               if(TMath::Abs(tlat)<70)
+                     yaw = -3.7e-8*tlat*tlat*tlat*tlat + 1.4e-7*tlat*tlat*tlat - 0.0005*tlat*tlat - 0.00025*tlat + 3.6;
+               yaw = diro*yaw;   //because should be different sign for ascending and descending orbits!
+               if(TMath::Abs(bank)>0.5 && TMath::Abs(yaw-orbitalinfo->phi)<3.0) yaw=orbitalinfo->phi;
+ //            Qiji = PO->EulertoEci(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,bank,yaw,spitch);             // 10RED CHECK
+               Qij = PO->EulertoEci(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,bank,yaw,spitch);              // STANDARD
+               orbitalinfo->qkind = 1;
+               break;
+             }
+           }     // enf of  loop for(UInt_t mu = must;mu<RTtime2.size()-1;mu++){
+           //Qij = PO->GEOtoECI(Dij,orbitalinfo->absTime,orbitalinfo->lat,orbitalinfo->lon); // to convert from Dij to Qij
+         } // end of if(atime<RTtime1[0]
+         } // end of f(((orbitalinfo->TimeGap>60.0 && TMath...
+         TMatrixD qij = PO->ColPermutation(Qij);
+         TMatrixD Fij = PO->ECItoGreenwich(Qij,orbitalinfo->absTime);
+         TMatrixD Gij = PO->ColPermutation(Fij);
+         Dij = PO->ECItoGEO(Qij,orbitalinfo->absTime,orbitalinfo->lat,orbitalinfo->lon);
          TMatrixD Iij = PO->ColPermutation(Dij);
-         //
+         TVector3 SP = PO->GetSunPosition(orbitalinfo->absTime);
+         // go to Pamela reference frame from Resurs reference frame
+         Float_t tmpy = SP.Y();
+         SP.SetY(SP.Z());
+         SP.SetZ(-tmpy);
+         TVector3 SunZenith;
+         SunZenith.SetMagThetaPhi(1,23.439281*TMath::DegToRad(),TMath::Pi()/2.);
+         TVector3 SunMag = -SP;
+         SunMag.Rotate(-45*TMath::DegToRad(),SunZenith);
+         tmpy=SunMag.Y();
+         SunMag.SetY(SunMag.Z());
+         SunMag.SetZ(-tmpy);
          orbitalinfo->Iij.ResizeTo(Iij);
          orbitalinfo->Iij = Iij;
          //
-         A1 = Iij(0,2);
+         //      A1 = Iij(0,2);
-         A2 = Iij(1,2);
+         //      A2 = Iij(1,2);
-         A3 = Iij(2,2);
+         //      A3 = Iij(2,2);
          //
          //      orbitalinfo->pamzenitangle = (Float_t)PO->GetPitchAngle(1,0,0,A1,A2,A3);                        // Angle between zenit and Pamela's main axiz
          //      orbitalinfo->pamBangle = (Float_t)PO->GetPitchAngle(A1,A2,A3,Bx,By,Bz);                 // Angle between Pamela's main axiz and B
          //
+         if ( debug ) printf(" matrixes done  \n");
          if ( !standalone && tof->ntrk() > 0 ){
+           if ( debug ) printf(" !standalone \n");
            //
            Int_t nn = 0;
            for(Int_t nt=0; nt < tof->ntrk(); nt++){
              //
              ToFTrkVar *ptt = tof->GetToFTrkVar(nt);
+             if (debug) cout<<"tof->ntrk() = "<<tof->ntrk()<<"\tptt->trkseqno = "<<ptt->trkseqno<<"\ttrke->ntrk() = "<<trke->ntrk()<<endl;
              Double_t E11x = ptt->xtr_tof[0]; // tr->x[0];
              Double_t E11y = ptt->ytr_tof[0]; //tr->y[0];
              Double_t E11z = zin[0];
-Line 1174 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1568 
 int OrbitalInfoCore(UInt_t run, TFile *f
              Double_t E22y = ptt->ytr_tof[3];//tr->y[3];
              Double_t E22z = zin[3];
              if ( (E11x < 100. && E11y < 100. && E22x < 100. && E22y < 100.) || ptt->trkseqno != -1  ){
+               TrkTrack *mytrack = trke->GetStoredTrack(ptt->trkseqno);
+               Float_t rig=1/mytrack->GetDeflection();
                Double_t norm = sqrt(pow(E22x-E11x,2)+pow(E22y-E11y,2)+pow(E22z-E11z,2));
                //              Double_t MyAzim = TMath::RadToDeg()*atan(TMath::Abs(E22y-E11y)/TMath::Abs(E22x-E11x));
                //              if(E22x-E11x>=0 && E22y-E11y <0) MyAzim =  360. - MyAzim;
-Line 1190 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1586 
 int OrbitalInfoCore(UInt_t run, TFile *f
                t_orb->Eij.ResizeTo(Eij);
                t_orb->Eij = Eij;
                //
-               TMatrixD Sij = PO->PamelatoGEO(Fij,Px,Py,Pz);
+               TMatrixD Sij = PO->PamelatoGEO(Gij,Px,Py,Pz);
                t_orb->Sij.ResizeTo(Sij);
                t_orb->Sij = Sij;
                //
                t_orb->pitch = (Float_t)PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),Bx,By,Bz);
                //
+                 // SunPosition in instrumental reference frame
+               TMatrixD Kij = PO->PamelatoGEO(qij,Px,Py,Pz);
+               TMatrixD Lij = PO->PamelatoGEO(qij,0,0,1);
+               t_orb->sunangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),-SP.X(),-SP.Y(),-SP.Z());
+               t_orb->sunmagangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),SunMag.X(),SunMag.Y(),SunMag.Z());
                //
-               Double_t omega = PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),cos(orbitalinfo->lon+TMath::Pi()/2)-sin(orbitalinfo->lon+TMath::Pi()/2),cos(orbitalinfo->lon+TMath::Pi()/2)+sin(orbitalinfo->lon+TMath::Pi()/2),1);
                //
-               t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow((1+sqrt(1-pow(orbitalinfo->L,-3/2)*cos(omega))),2));
+               //Double_t omega = PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),cos(orbitalinfo->lon+TMath::Pi()/2)-sin(orbitalinfo->lon+TMath::Pi()/2),cos(orbitalinfo->lon+TMath::Pi()/2)+sin(orbitalinfo->lon+TMath::Pi()/2),1);
+               Double_t omega = PO->GetPitchAngle(-Eij(0,0),-Eij(1,0),-Eij(2,0),1,0,0) * TMath::DegToRad();
+               TVector3 Bxy(0,By,Bz);
+               TVector3 Exy(0,-Eij(1,0),-Eij(2,0));
+               Double_t dzeta=Bxy.Angle(Exy);
+               if (-Eij(1,0) < 0) dzeta=2.0*TMath::Pi() - dzeta;
+                 if(debug) cout << "omega = "<<omega*TMath::RadToDeg()<<"\tdzeta = "<<dzeta*TMath::RadToDeg()<<endl;
+                 // Formula from D.F. Smart *, M.A. Shea [2005]; A review of geomagnetic cutoff rigidities for earth-orbiting spacecraft
+               if(rig>=0) t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2));
+               else t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(TMath::Pi()+dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2));
+               if (debug) cout << "R = " << rig << "\tcutoff = " << t_orb->cutoff << endl;
+               //t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow((1+sqrt(1-pow(orbitalinfo->L,-3/2)*cos(omega))),2));
                //
                if ( t_orb->pitch != t_orb->pitch ) t_orb->pitch = -1000.;
                if ( t_orb->cutoff != t_orb->cutoff ) t_orb->cutoff = -1000.;
+               if ( t_orb->sunangle != t_orb->sunangle ) t_orb->sunangle = -1000.;
+               if ( t_orb->sunmagangle != t_orb->sunmagangle ) t_orb->sunmagangle = -1000.;
                //
                if ( debug ) printf(" orbitalinfo->cutoffsvl %f vitaly %f \n",orbitalinfo->cutoffsvl,t_orb->cutoff);
                //
-Line 1215 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1633 
 int OrbitalInfoCore(UInt_t run, TFile *f
              //
            };
          } else {
-           if ( debug ) printf(" mmm... mode %u standalone %i ntrk %i \n",orbitalinfo->mode,standalone,tof->ntrk());
+           if ( debug ) printf(" mmm... mode %u standalone  \n",orbitalinfo->mode);
-         };
+         }
          //
        } else {
          if ( !standalone && tof->ntrk() > 0 ){
-Line 1235 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1653 
 int OrbitalInfoCore(UInt_t run, TFile *f
                //
                t_orb->pitch = -1000.;
                //
+               t_orb->sunangle = -1000.;
+               //
+               t_orb->sunmagangle = -1000;
+               //
                t_orb->cutoff = -1000.;
                //
                new(tor[nn]) OrbitalInfoTrkVar(*t_orb);
-Line 1246 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1668 
 int OrbitalInfoCore(UInt_t run, TFile *f
              //
            };
          };
-       };
+       };        // if( orbitalinfo->TimeGap>0){
        //
        // Fill the class
        //
-Line 1259 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1681 
 int OrbitalInfoCore(UInt_t run, TFile *f
      // Here you may want to clear some variables before processing another run
      //
-     //gStyle->SetOptStat(000000);
+     if ( verbose ) printf(" Clear before new run \n");
-     //gStyle->SetPalette(1);
-     /*TCanvas* c1 = new TCanvas("c1","",1200,800);
-     //c1->Divide(1,4);
-     c1->cd(1);
-     //q0testing->Draw("colz");
-     //c1->cd(2);
-     //q1testing->Draw("colz");
-     //c1->cd(3);
-     Pitchtesting->Draw("colz");
-     //c1->cd(4);
-     //q3testing->Draw("colz");
-     c1->SaveAs("9.Rollhyst.png");
-     delete c1;*/
      delete dbtime;
-     if ( L_QQ_Q_l_upper ) delete L_QQ_Q_l_upper;
+     if ( mcmdrc ) mcmdrc->Clear();
+     mcmdrc = 0;
+     if ( verbose ) printf(" Clear before new run1 \n");
      if ( L_QQ_Q_l_lower ) delete L_QQ_Q_l_lower;
+     if ( verbose ) printf(" Clear before new run2 \n");
+     if ( L_QQ_Q_l_upper ) delete L_QQ_Q_l_upper;
+     if ( verbose ) printf(" Clear before new run3 \n");
      if ( RYPang_upper ) delete RYPang_upper;
+     if ( verbose ) printf(" Clear before new run4 \n");
      if ( RYPang_lower ) delete RYPang_lower;
+     if ( l0tr ) l0tr->Delete();
+     if ( verbose ) printf(" End run \n");
    }; // process all the runs
    if (verbose) printf("\n Finished processing data \n");
-Line 1313 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1733 
 int OrbitalInfoCore(UInt_t run, TFile *f
        };
        if (verbose) printf(" Finished successful copying!\n");
      };
+     //if ( OrbitalInfotrclone )    OrbitalInfotrclone->Clear();
+     //if ( OrbitalInfotrclone )    OrbitalInfotrclone->Delete();
    };
    //
    // Close files, delete old tree(s), write and close level2 file
    //
    if ( l0File ) l0File->Close();
-   if ( tempfile ) tempfile->Close();
    if ( myfold ) gSystem->Unlink(tempname.str().c_str());
    //
-   if ( runinfo ) runinfo->Close();
    if ( OrbitalInfotr ) OrbitalInfotr->SetName("OrbitalInfo");
-   if ( tof ) tof->Delete();
-   if ( ttof ) ttof->Delete();
    //
    if ( file ){
      file->cd();
-     file->Write();
+     if ( OrbitalInfotr ) OrbitalInfotr->Write("OrbitalInfo", TObject::kOverwrite); // 10 RED bug fixed
    };
    //
+   if (verbose) printf("\n Exiting...\n");
    if ( myfold ) gSystem->Unlink(OrbitalInfofolder.str().c_str());
    //
    // the end
-Line 1339 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1760 
 int OrbitalInfoCore(UInt_t run, TFile *f
      dbc->Close();
      delete dbc;
    };
-   if (verbose) printf("\n Exiting...\n");
-   if(OrbitalInfotr)OrbitalInfotr->Delete();
    //
+   if (verbose) printf("\n Exiting...\n");
+   if ( tempfile ) tempfile->Close();
    if ( PO ) delete PO;
-   if ( orbitalinfo ) delete orbitalinfo;
+   if ( gltle ) delete gltle;
-   if ( orbitalinfoclone ) delete orbitalinfoclone;
+   if ( glparam ) delete glparam;
+   if ( glparam2 ) delete glparam2;
+   if ( glparam3 ) delete glparam3;
+   if (verbose) printf("\n Exiting3...\n");
    if ( glroot ) delete glroot;
+   if (verbose) printf("\n Exiting4...\n");
+   if ( runinfo ) runinfo->Close();
    if ( runinfo ) delete runinfo;
+   if ( tof ) delete tof;
+   if ( trke ) delete trke;
+   if ( debug ){
+   cout << "1   0x" << OrbitalInfotr << endl;
+   cout << "2   0x" << OrbitalInfotrclone << endl;
+   cout << "3   0x" << l0tr << endl;
+   cout << "4   0x" << tempOrbitalInfo << endl;
+   cout << "5   0x" << ttof << endl;
+   }
+   //
+   if ( debug )  file->ls();
    //
    if(code < 0)  throw code;
    return(code);
-Line 1394 
 UInt_t holeq(Double_t lower,Double_t upp
+Line 1834 
 UInt_t holeq(Double_t lower,Double_t upp
    Bool_t R10l = false;     // Sign of R10 mode in lower quaternions array
    Bool_t R10u = false;     // Sign of R10 mode in upper quaternions array
    Bool_t insm = false;     // Sign that we inside quaternions array
-   Bool_t mxtml = false;    // Sign of mixt mode in lower quaternions array
+   //  Bool_t mxtml = false;    // Sign of mixt mode in lower quaternions array
-   Bool_t mxtmu = false;    // Sign of mixt mode in upper quaternions array
+   //  Bool_t mxtmu = false;    // Sign of mixt mode in upper quaternions array
    Bool_t npasm = false;     // Sign of normall pass between R10 and non R10 or between non R10 and R10
    UInt_t NCQl = 6;       // Number of correct quaternions in lower array
-   UInt_t NCQu = 6;       // Number of correct quaternions in upper array
+   //  UInt_t NCQu = 6;       // Number of correct quaternions in upper array
    if (f>0){
      insm = true;
      if(Qupper->time[f]-Qupper->time[f-1]==30) R10u = false;
-Line 1410 
 UInt_t holeq(Double_t lower,Double_t upp
+Line 1850 
 UInt_t holeq(Double_t lower,Double_t upp
      if((Qlower->time[5]-Qlower->time[0]==150)&&(Qlower->time[1]-Qlower->time[0]==30)) R10l = false;
      if((Qupper->time[5]-Qupper->time[0]==150)&&(Qupper->time[1]-Qupper->time[0]==30)) R10u = false;
      if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]==30)){
-       mxtml = true;
+       //      mxtml = true;
        for(UInt_t i = 1; i < 6; i++){
          if(Qlower->time[i]-Qlower->time[0]==30*i) NCQl=i;
        }
      }
-     if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]==30)){
+     //    if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]==30)){
-       mxtmu = true;
+       //      mxtmu = true;
-       for(UInt_t i = 1; i < 6; i++){
+       //      for(UInt_t i = 1; i < 6; i++){
-         if(Qupper->time[i]-Qupper->time[0]==30*i) NCQu=i;
+       //        if(Qupper->time[i]-Qupper->time[0]==30*i) NCQu=i;
-       }
+       //      }
-     }
+     //    }
    }
    if(((upper-lower==1.5)||(upper-lower==3.)||(upper-lower==30.)||(upper-lower==31.5)||(upper-lower==33.)||(upper-lower==181.5)||(upper-lower==210.)||(upper-lower==211.5))&&!insm) npasm = true;
-Line 1452 
 void inclresize(vector<Double_t>& t,vect
+Line 1892 
 void inclresize(vector<Double_t>& t,vect
    Yaw.resize(sizee);
  }
- //Find fitting sine functions for q0,q1,q2,q3 and Yaw-angle;
+ // geomagnetic calculation staff
- void sineparam(vector<Sine>& qsine, vector<Double_t>& qtime, vector<Float_t>& q, vector<Float_t>& Roll, vector<Float_t>& Pitch, Float_t limsin){
-   UInt_t mulast = 0;
+ //void GM_ScanIGRF(TString PATH, GMtype_Data *G0, GMtype_Data *G1, GMtype_Data *H1)
-   UInt_t munow = 0;
+ void GM_ScanIGRF(TSQLServer *dbc, GMtype_Data *G0, GMtype_Data *G1, GMtype_Data *H1)
-   UInt_t munext = 0;
+ {
-   Bool_t increase = false;
+   GL_PARAM *glp = new GL_PARAM();
-   Bool_t decrease = false;
+   Int_t parerror=glp->Query_GL_PARAM(1,304,dbc); // parameters stored in DB in GL_PRAM table
-   Bool_t Max_is_defined = false;
+   if ( parerror<0 ) {
-   Bool_t Start_point_is_defined = false;
+     throw -902;
-   Bool_t Period_is_defined = false;
+   }
-   Bool_t Large_gap = false;
+         /*This function scans inputs G0, G1, and H1 of the IGRF table into 3 data arrays*/
-   Bool_t normal_way = true;
+   //    TString SATH="/data03/Malakhov/pam9Malakhov/installed10/calib/orb-param/";
-   Bool_t small_gap_on_ridge = false;
+         int i;
-   Double_t t1 = 0;
+         double temp;
-   Double_t t1A = 0;
+         char buffer[200];
-   Int_t sinesize = 0;
+         FILE *IGRF;
-   Int_t nfi = 0;
+         IGRF = fopen((glp->PATH+glp->NAME).Data(), "r");
-   for(UInt_t mu = 0;mu<qtime.size();mu++){
+         //      IGRF = fopen(PATH+"IGRF.tab", "r");
-     if(Roll[mu]<1. && Pitch[mu]<1.){
+         G0->size = 25;
-     if(munext==0 && munow!=0)munext=mu;
+         G1->size = 25;
-     if(munow==0 && mulast!=0)munow=mu;
+         H1->size = 25;
-     if(mulast==0)mulast=mu;
+         for( i = 0; i < 4; i++)
-     if(mulast!=0 && munow!=0 && munext!=0){mulast=munow;munow=munext;munext=mu;}
+         {
-     if(TMath::Abs(q[munow])>TMath::Abs(q[mulast]) && TMath::Abs(q[munow])>TMath::Abs(q[munext]) && TMath::Abs(q[munow])>limsin && qtime[munext]-qtime[mulast]>400)small_gap_on_ridge = true;
+                 fgets(buffer, 200, IGRF);
-     if(munext>mulast && (qtime[munext]-qtime[mulast]>=2000 || qtime[munext]-qtime[mulast]<0)){if(Large_gap){normal_way = false;Large_gap = false;}else{Large_gap = true;normal_way = false;}}else normal_way = true;
-     if(Large_gap || small_gap_on_ridge){
-       //cout<<"Large gap..."<<endl;
-       //if(small_gap_on_ridge)cout<<"small gap..."<<endl;
-       increase = false;
-       decrease = false;
-       if(nfi>0){
-         qsine.resize(qsine.size()-1);
-         sinesize = qsine.size();
-       }else{
-         if(!Period_is_defined){
-           if(qsine.size()>1){
-             qsine[sinesize-1].b = qsine[sinesize-2].b;
-             qsine[sinesize-1].c = qsine[sinesize-2].c;
-           }else{
-             qsine[sinesize-1].b = TMath::Pi()/1591.54;
-             qsine[sinesize-1].c = qsine[sinesize-1].startPoint;
-           }
-         }
-         if(!Max_is_defined){
-           if(qsine.size()>1)qsine[sinesize-1].A = qsine[sinesize-2].A;else qsine[sinesize-1].A = limsin;
-         }
-         qsine[sinesize-1].NeedFit = true;
-       }
-       qsine[sinesize-1].finishPoint = qtime[munow];
-       nfi = 0;
-       Max_is_defined = false;
-       Start_point_is_defined = false;
-       Period_is_defined = false;
-       small_gap_on_ridge = false;
-     }
-     if(munext > munow && munow > mulast && normal_way){
-       if(!increase && !decrease){
-         qsine.resize(qsine.size()+1);
-         sinesize = qsine.size();
-         qsine[sinesize-1].startPoint=qtime[mulast];
-         if(q[munext]>q[munow] && q[munow]>q[mulast]) increase = true;
-         if(q[munext]<q[munow] && q[munow]<q[mulast]) decrease = true;
-       }
-       //if(TMath::Abs(q[munow])>TMath::Abs(q[mulast]) && TMath::Abs(q[munow])>TMath::Abs(q[munext]) && TMath::Abs(q[munow])>limsin && qtime[munow]-qtime[mulast]>=400 || qtime[munext]-qtime[munow]>=400){small_gap_on_ridge = true;mu--;continue;}
-       if(TMath::Abs(q[munow])>TMath::Abs(q[mulast]) && TMath::Abs(q[munow])>TMath::Abs(q[munext]) && TMath::Abs(q[munow])>limsin && qtime[munow]-qtime[mulast]<400 && qtime[munext]-qtime[munow]<400){
-         //cout<<"Max point is qtime = "<<qtime[munow]<<"\tq = "<<q[munow]<<endl;
-         if(q[munow]>q[mulast]){
-           increase = false;
-           decrease = true;
-         }
-         if(q[munow]<q[mulast]){
-           increase = true;
-           decrease = false;
          }
-         if(Max_is_defined && !Start_point_is_defined){
+         fscanf(IGRF, "g 1 0 %lf ", &G0->element[0]);
-           Double_t qPer = qtime[munow]-t1A;
+         for(i = 1; i <= 22; i++)
-           if(qPer>1000){
+         {
-             //cout<<"qsine["<<sinesize-1<<"] = "<<qPer<<" = "<<qtime[munow]<<" - "<<t1A<<"\tlim = "<<limsin<<endl;
+                 fscanf(IGRF ,"%lf ", &G0->element[i]);
-             qsine[sinesize-1].b=TMath::Pi()/qPer;
-             if(decrease)qsine[sinesize-1].c=-qsine[sinesize-1].b*t1A;
-             if(increase)qsine[sinesize-1].c=-qsine[sinesize-1].b*(t1A-qPer);
-             Period_is_defined = true;
-           }
          }
-         Max_is_defined = true;
+         fscanf(IGRF ,"%lf\n", &temp);
-         qsine[sinesize-1].A = TMath::Abs(q[munow]);
+         G0->element[23] = temp * 5 + G0->element[22];
-         if(Start_point_is_defined && Period_is_defined){
+         G0->element[24] = G0->element[23] + 5 * temp;
-           qsine[sinesize-1].finishPoint = qtime[munow];
+         fscanf(IGRF, "g 1 1 %lf ", &G1->element[0]);
-           nfi++;
+         for(i = 1; i <= 22; i++)
-           qsine[sinesize-1].NeedFit = false;
+         {
-           Max_is_defined = false;
+                 fscanf( IGRF, "%lf ", &G1->element[i]);
-           Start_point_is_defined = false;
-           Period_is_defined = false;
-           qsine.resize(qsine.size()+1);
-           sinesize = qsine.size();
-           qsine[sinesize-1].startPoint = qtime[munow];
          }
-         if(!Start_point_is_defined) t1A=qtime[munow];
+         fscanf(IGRF, "%lf\n", &temp);
-       }
+         G1->element[23] = temp * 5 + G1->element[22];
-       //if((q[munow]>=0 && q[mulast]<=0) || (q[munow]<=0 && q[mulast]>=0))cout<<"cross zero point diference = "<<qtime[munext] - qtime[mulast]<<"\tqlast = "<<qtime[mulast]<<"\tqnow = "<<qtime[munow]<<"\tqnext = "<<qtime[munext]<<endl;
+         G1->element[24] = temp * 5 + G1->element[23];
-       if(((q[munow]>=0 && q[mulast]<=0) || (q[munow]<=0 && q[mulast]>=0)) && qtime[munow]-qtime[mulast]<2000 && qtime[munext]-qtime[munow]<2000){
+         fscanf(IGRF, "h 1 1 %lf ", &H1->element[0]);
-         Double_t tcrosszero = 0;
+         for(i = 1; i <= 22; i++)
-         //cout<<"cross zero point...qtime = "<<qtime[munow]<<endl;
+         {
-         if(q[munow]==0.) tcrosszero = qtime[munow];else
+                 fscanf( IGRF, "%lf ", &H1->element[i]);
-           if(q[mulast]==0.)tcrosszero = qtime[mulast];else{
-             Double_t k_ = (q[munow]-q[mulast])/(qtime[munow]-qtime[mulast]);
-             Double_t b_ = q[munow]-k_*qtime[munow];
-             tcrosszero = -b_/k_;
-           }
-         if(Start_point_is_defined){
-           //cout<<"Start Point allready defined"<<endl;
-           Double_t qPer = tcrosszero - t1;
-           qsine[sinesize-1].b = TMath::Pi()/qPer;
-           //cout<<"qsine["<<sinesize-1<<"].b = "<<TMath::Pi()/qPer<<endl;
-           Period_is_defined = true;
-           Float_t x0 = 0;
-           if(decrease)x0 = t1;
-           if(increase)x0 = tcrosszero;
-           qsine[sinesize-1].c = -qsine[sinesize-1].b*x0;
-           if(Max_is_defined){
-             //cout<<"Max was previous defined"<<endl;
-             qsine[sinesize-1].finishPoint = qtime[munow];
-             nfi++;
-             qsine[sinesize-1].NeedFit = false;
-             Max_is_defined = false;
-             t1 = tcrosszero;
-             Start_point_is_defined = true;
-             Period_is_defined = false;
-             qsine.resize(qsine.size()+1);
-             sinesize = qsine.size();
-             qsine[sinesize-1].startPoint = qtime[munow];
-           }
-         }else{
-           t1 = tcrosszero;
-           Start_point_is_defined = true;
          }
-       }
+         fscanf(IGRF, "%lf\n", &temp);
-     }
+         H1->element[23] = temp * 5 + H1->element[22];
-     }
+         H1->element[24] = temp * 5 + H1->element[23];
-   }
+   if ( glp ) delete glp;
+ } /*GM_ScanIGRF*/
-   //cout<<"FINISH SINE INTERPOLATION FUNCTION..."<<endl<<endl;
+ void GM_SetEllipsoid(GMtype_Ellipsoid *Ellip)
- }
+ {
+         /*This function sets the WGS84 reference ellipsoid to its default values*/
+         Ellip->a        =                       6378.137; /*semi-major axis of the ellipsoid in */
+         Ellip->b        =                       6356.7523142;/*semi-minor axis of the ellipsoid in */
+         Ellip->fla      =                       1/298.257223563;/* flattening */
+         Ellip->eps      =                       sqrt(1- ( Ellip->b *    Ellip->b) / (Ellip->a * Ellip->a ));  /*first eccentricity */
+         Ellip->epssq    =                       (Ellip->eps * Ellip->eps);   /*first eccentricity squared */
+         Ellip->re       =                       6371.2;/* Earth's radius */
+ } /*GM_SetEllipsoid*/
+ void GM_EarthCartToDipoleCartCD(GMtype_Pole Pole, GMtype_CoordCartesian EarthCoord, GMtype_CoordCartesian *DipoleCoords)
+ {
+         /*This function converts from Earth centered cartesian coordinates to dipole centered cartesian coordinates*/
+         double X, Y, Z, CosPhi, SinPhi, CosLambda, SinLambda;
+         CosPhi = cos(TMath::DegToRad()*Pole.phi);
+         SinPhi = sin(TMath::DegToRad()*Pole.phi);
+         CosLambda = cos(TMath::DegToRad()*Pole.lambda);
+         SinLambda = sin(TMath::DegToRad()*Pole.lambda);
+         X = EarthCoord.x;
+         Y = EarthCoord.y;
+         Z = EarthCoord.z;
+         /*These equations are taken from a document by Wallace H. Campbell*/
+         DipoleCoords->x = X * CosPhi * CosLambda + Y * CosPhi * SinLambda - Z * SinPhi;
+         DipoleCoords->y = -X * SinLambda + Y * CosLambda;
+         DipoleCoords->z = X * SinPhi * CosLambda + Y * SinPhi * SinLambda + Z * CosPhi;
+ } /*GM_EarthCartToDipoleCartCD*/
+ void GM_GeodeticToSpherical(GMtype_Ellipsoid Ellip, GMtype_CoordGeodetic CoordGeodetic, GMtype_CoordSpherical *CoordSpherical)
+ {
+         double CosLat, SinLat, rc, xp, zp; /*all local variables */
+         /*
+         ** Convert geodetic coordinates, (defined by the WGS-84
+         ** reference ellipsoid), to Earth Centered Earth Fixed Cartesian
+         ** coordinates, and then to spherical coordinates.
+         */
+         CosLat = cos(TMath::DegToRad()*CoordGeodetic.phi);
+         SinLat = sin(TMath::DegToRad()*CoordGeodetic.phi);
+         /* compute the local radius of curvature on the WGS-84 reference ellipsoid */
+         rc = Ellip.a / sqrt(1.0 - Ellip.epssq * SinLat * SinLat);
+         /* compute ECEF Cartesian coordinates of specified point (for longitude=0) */
+         xp = (rc + CoordGeodetic.HeightAboveEllipsoid) * CosLat;
+         zp = (rc*(1.0 - Ellip.epssq) + CoordGeodetic.HeightAboveEllipsoid) * SinLat;
+         /* compute spherical radius and angle lambda and phi of specified point */
+         CoordSpherical->r = sqrt(xp * xp + zp * zp);
+         CoordSpherical->phig = TMath::RadToDeg()*asin(zp / CoordSpherical->r);     /* geocentric latitude */
+         CoordSpherical->lambda = CoordGeodetic.lambda;                   /* longitude */
+ } /*GM_GeodeticToSpherical*/
+ void GM_PoleLocation(GMtype_Model Model, GMtype_Pole *Pole)
+ {
+         /*This function finds the location of the north magnetic pole in spherical coordinates.  The equations are
+         **from Wallace H. Campbell's Introduction to Geomagnetic Fields*/
+         Pole->phi = TMath::RadToDeg()*-atan(sqrt(Model.h1 * Model.h1 + Model.g1 * Model.g1)/Model.g0);
+         Pole->lambda = TMath::RadToDeg()*atan(Model.h1/Model.g1);
+ } /*GM_PoleLocation*/
+ void GM_SphericalToCartesian(GMtype_CoordSpherical CoordSpherical, GMtype_CoordCartesian *CoordCartesian)
+ {
+         /*This function converts spherical coordinates into Cartesian coordinates*/
+         double CosPhi = cos(TMath::DegToRad()*CoordSpherical.phig);
+         double SinPhi = sin(TMath::DegToRad()*CoordSpherical.phig);
+         double CosLambda = cos(TMath::DegToRad()*CoordSpherical.lambda);
+         double SinLambda = sin(TMath::DegToRad()*CoordSpherical.lambda);
+         CoordCartesian->x = CoordSpherical.r * CosPhi * CosLambda;
+         CoordCartesian->y = CoordSpherical.r * CosPhi * SinLambda;
+         CoordCartesian->z = CoordSpherical.r * SinPhi;
+ } /*GM_SphericalToCartesian*/
+ void GM_TimeAdjustCoefs(Float_t year, Float_t jyear, GMtype_Data g0d, GMtype_Data g1d, GMtype_Data h1d, GMtype_Model *Model)
+ {
+         /*This function calls GM_LinearInterpolation for the coefficients to estimate the value of the
+         **coefficient for the given date*/
+         int index;
+         double x;
+         index = (year - GM_STARTYEAR) / 5;
+         x = (jyear - GM_STARTYEAR) / 5;
+         Model->g0 = GM_LinearInterpolation(index, index+1, g0d.element[index], g0d.element[index+1], x);
+         Model->g1 = GM_LinearInterpolation(index, index+1, g1d.element[index], g1d.element[index+1], x);
+         Model->h1 = GM_LinearInterpolation(index, index+1, h1d.element[index], h1d.element[index+1], x);
+ } /*GM_TimeAdjustCoefs*/
+ double GM_LinearInterpolation(double x1, double x2, double y1, double y2, double x)
+ {
+         /*This function takes a linear interpolation between two given points for x*/
+         double weight, y;
+         weight  = (x - x1) / (x2 - x1);
+         y = y1 * (1 - weight) + y2 * weight;
+         return y;
+ }/*GM_LinearInterpolation*/
+ void GM_CartesianToSpherical(GMtype_CoordCartesian CoordCartesian, GMtype_CoordSpherical *CoordSpherical)
+ {
+         /*This function converts a point from Cartesian coordinates into spherical coordinates*/
+         double X, Y, Z;
+         X = CoordCartesian.x;
+         Y = CoordCartesian.y;
+         Z = CoordCartesian.z;
+         CoordSpherical->r = sqrt(X * X + Y * Y + Z * Z);
+         CoordSpherical->phig = TMath::RadToDeg()*asin(Z / (CoordSpherical->r));
+         CoordSpherical->lambda = TMath::RadToDeg()*atan2(Y, X);
+ } /*GM_CartesianToSpherical*/

 Legend:



Removed from v.1.44
 


changed lines


 
Added in v.1.72
 Legend:



Removed from v.1.44
 


changed lines


 
Added in v.1.72
-Removed from v.1.44
+Added in v.1.72

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