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

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

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-revision 1.34 by mocchiut,
Fri Nov 28 09:05:21 2008 UTC
+revision 1.60 by pam-mep,
Thu Jun  7 14:04:00 2012 UTC
 Line 1
- //
  // C/C++ headers
  //
  #include <fstream>
-Line 9
+Line 8
  //
  // ROOT headers
  //
+ //#include <TCanvas.h>
+ #include <TH2F.h> //for test only. Vitaly.
+ #include <TVector3.h>
+ //#include <TF1.h>
  #include <TTree.h>
  #include <TClassEdit.h>
  #include <TObject.h>
-Line 44
+Line 48
  #include <OrbitalInfoCore.h>
  #include <InclinationInfo.h>
  using namespace std;
  //
-Line 61 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 66 
 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 124 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 129 
 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.
    //
-   //  UInt_t iev = 0;
+ //  UInt_t oi = 0;
-   //  UInt_t j3 = 0;
-   UInt_t oi = 0;
    Int_t tmpSize = 0;
    //
    // variables needed to handle error signals
-Line 141 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 145 
 int OrbitalInfoCore(UInt_t run, TFile *f
    //
    OrbitalInfo *orbitalinfo = new OrbitalInfo();
    OrbitalInfo *orbitalinfoclone = new OrbitalInfo();
    //
    // define variables for opening and reading level0 file
    //
    TFile *l0File = 0;
    TTree *l0tr = 0;
-   TTree *l0trm = 0;
+   //  TTree *l0trm = 0;
+   TChain *ch = 0;
    // EM: open also header branch
    TBranch *l0head = 0;
    pamela::EventHeader *eh = 0;
-Line 176 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 182 
 int OrbitalInfoCore(UInt_t run, TFile *f
    //
    // IGRF stuff
    //
-   float dimo = 0.0; // dipole moment (computed from dat files)
+   Float_t dimo = 0.0; // dipole moment (computed from dat files)
-   float bnorth, beast, bdown, babs;
+   Float_t bnorth, beast, bdown, babs;
-   float xl; // L value
+   Float_t xl; // L value
-   float icode; // code value for L accuracy (see fortran code)
+   Float_t icode; // code value for L accuracy (see fortran code)
-   float bab1; // What's  the difference with babs?
+   Float_t bab1; // What's  the difference with babs?
-   float stps = 0.005; // step size for field line tracing
+   Float_t stps = 0.005; // step size for field line tracing
-   float bdel = 0.01; // required accuracy
+   Float_t bdel = 0.01; // required accuracy
-   float bequ;  // equatorial b value (also called b_0)
+   Float_t bequ;  // equatorial b value (also called b_0)
-   bool value = 0; // false if bequ is not the minimum b value
+   Bool_t value = 0; // false if bequ is not the minimum b value
-   float rr0; // equatorial radius normalized to earth radius
+   Float_t rr0; // equatorial radius normalized to earth radius
    //
    // Working filename
-Line 209 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 215 
 int OrbitalInfoCore(UInt_t run, TFile *f
    OrbitalInfofolder << tempname.str().c_str();
    tempname << "/OrbitalInfotree_run";
    tempname << run << ".root";
+   UInt_t totnorun = 0;
    //
    // DB classes
    //
-Line 218 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 225 
 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;
-   char *niente = " ";
+   //  const char *niente = " ";
    GL_PARAM *glparam = new GL_PARAM();
    GL_PARAM *glparam2 = new GL_PARAM();
-   Int_t parerror=glparam->Query_GL_PARAM(1,301,dbc); // parameters stored in DB in GL_PRAM table
+   GL_PARAM *glparam3 = new GL_PARAM();
    //
-   // Orientation variables
+   // Orientation variables. Vitaly
    //
    UInt_t evfrom = 0;
    UInt_t jumped = 0;
-Line 251 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 260 
 int OrbitalInfoCore(UInt_t run, TFile *f
    Int_t nz = 6;
    Float_t zin[6];
    Int_t nevtofl2 = 0;
-   //
+   if ( verbose ) cout<<"Reading quaternions external file"<<endl;
-   if ( parerror<0 ) {
+   cout.setf(ios::fixed,ios::floatfield);
-     code = parerror;
+   /******Reading recovered quaternions...*********/
-     goto closeandexit;
+   vector<Double_t> recqtime;
-   };
+   vector<Float_t> recq0;
-   ltp2 = (Int_t)(glparam->PATH+glparam->NAME).Length();
+   vector<Float_t> recq1;
-   if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam->PATH+glparam->NAME).Data());
+   vector<Float_t> recq2;
-   //
+   vector<Float_t> recq3;
-   parerror=glparam2->Query_GL_PARAM(1,302,dbc); // parameters stored in DB in GL_PRAM table
+   Float_t Norm = 1;
+   Int_t parerror=glparam->Query_GL_PARAM(1,303,dbc); // parameters stored in DB in GL_PRAM table
+   ifstream in((glparam->PATH+glparam->NAME).Data(),ios::in);
    if ( parerror<0 ) {
      code = parerror;
      goto closeandexit;
-   };
+   }
-   ltp3 = (Int_t)(glparam2->PATH+glparam2->NAME).Length();
+   while(!in.eof()){
-   if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam2->PATH+glparam2->NAME).Data());
+     recqtime.resize(recqtime.size()+1);
-   //
+     Int_t sizee = recqtime.size();
-   initize_((char *)niente,&uno,(char *)(glparam->PATH+glparam->NAME).Data(),&ltp2,(char *)(glparam2->PATH+glparam2->NAME).Data(),&ltp3);
+     recq0.resize(sizee);
-   //
+     recq1.resize(sizee);
-   // End IGRF stuff//
+     recq2.resize(sizee);
-   //
+     recq3.resize(sizee);
+     in>>recqtime[sizee-1];
+     in>>recq0[sizee-1];
+     in>>recq1[sizee-1];
+     in>>recq2[sizee-1];
+     in>>recq3[sizee-1];
+     in>>Norm;
+   }
+   if ( verbose ) cout<<"We have read recovered data"<<endl;
+   // IGRF stuff moved inside run loop!
    for (Int_t ip=0;ip<nz;ip++){
      zin[ip] = tof->GetZTOF(tof->GetToFPlaneID(ip));
    };
-Line 342 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 364 
 int OrbitalInfoCore(UInt_t run, TFile *f
    // number of run to be processed
    //
    numbofrun = runinfo->GetNoRun();
-   UInt_t totnorun = runinfo->GetRunEntries();
+   totnorun = runinfo->GetRunEntries();
    //
    // Try to access the OrbitalInfo tree in the file, if it exists we are reprocessing data if not we are processing a new run
    //
-Line 376 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 398 
 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 394 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 416 
 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 430 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 454 
 int OrbitalInfoCore(UInt_t run, TFile *f
        }
        for (UInt_t j = 0; j < nobefrun; j++){
          //
-         OrbitalInfotrclone->GetEntry(j);
+         if ( OrbitalInfotrclone->GetEntry(j) <= 0 ) throw -36;
          //
          // copy orbitalinfoclone to mydec
          //
-Line 444 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 468 
 int OrbitalInfoCore(UInt_t run, TFile *f
          //
        };
        if (verbose) printf(" Finished successful copying!\n");
      };
    };
    //
+   //
    // Get the list of run to be processed, if only one run has to be processed the list will contain one entry only.
    //
    runlist = runinfo->GetRunList();
-Line 454 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 479 
 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 502 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 533 
 int OrbitalInfoCore(UInt_t run, TFile *f
      fname = ftmpname.str().c_str();
      ftmpname.str("");
      //
-     // print out informations
+     // print nout informations
      //
      totevent = runinfo->NEVENTS;
      evfrom = runinfo->EV_FROM;
-Line 516 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 547 
 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 554 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 586 
 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 ( irun == 0 ){
+       if ( l0head->GetEntry(runinfo->EV_FROM) <= 0 ) throw -36;
+       //
+       // 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+glparam->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+glparam2->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);
+       //
+     }
+     //
+     // End IGRF stuff//
+     //
+     //
+     //     TTree *tp = (TTree*)l0File->Get("RunHeader");
+     //     tp->SetBranchAddress("Header", &eH);
+     //     tp->SetBranchAddress("RunHeader", &reh);
+     //     tp->GetEntry(0);
+     //     ph = eH->GetPscuHeader();
+     //     ULong_t TimeSync = reh->LAST_TIME_SYNC_INFO;
+     //     ULong_t ObtSync = reh->OBT_TIME_SYNC;
+     //     if ( debug ) printf(" 1 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",TimeSync,ObtSync,TimeSync-ObtSync);
      //
- //     TTree *tp = (TTree*)l0File->Get("RunHeader");
- //     tp->SetBranchAddress("Header", &eH);
- //     tp->SetBranchAddress("RunHeader", &reh);
- //     tp->GetEntry(0);
- //     ph = eH->GetPscuHeader();
- //     ULong_t TimeSync = reh->LAST_TIME_SYNC_INFO;
- //     ULong_t ObtSync = reh->OBT_TIME_SYNC;
- //     if ( debug ) printf(" 1 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",TimeSync,ObtSync,TimeSync-ObtSync);
- //
      ULong_t TimeSync = (ULong_t)dbtime->GetTimesync();
      ULong_t ObtSync = (ULong_t)(dbtime->GetObt0()/1000);
      ULong_t DeltaOBT = TimeSync - ObtSync;
      if ( debug ) printf(" 2 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",(ULong_t)(dbtime->GetTimesync()/1000),(ULong_t)dbtime->GetObt0(),TimeSync-ObtSync);
+     //
-     l0trm = (TTree*)l0File->Get("Mcmd");
+     // Read MCMDs from up to 11 files, 5 before and 5 after the present one in order to have some kind of inclination information
-     neventsm = l0trm->GetEntries();
+     //
+     ch = new TChain("Mcmd","Mcmd");
+     //
+     // look in the DB to find the closest files to this run
+     //
+     TSQLResult *pResult = 0;
+     TSQLRow *Row = 0;
+     stringstream myquery;
+     UInt_t l0fid[10];
+     Int_t i = 0;
+     memset(l0fid,0,10*sizeof(Int_t));
+     //
+     myquery.str("");
+     myquery << "select ID_ROOT_L0 from GL_RUN where RUNHEADER_TIME<=" << runinfo->RUNHEADER_TIME << " group by ID_ROOT_L0 order by RUNHEADER_TIME desc limit 5;";
+     //
+     pResult = dbc->Query(myquery.str().c_str());
+     //
+     i = 9;
+     if( pResult ){
+       //
+       Row = pResult->Next();
+       //
+       while ( Row ){
+         //
+         // store infos and exit
+         //
+         l0fid[i] = (UInt_t)atoll(Row->GetField(0));
+         i--;
+         Row = pResult->Next();
+         //
+       };
+       pResult->Delete();
+     };
+     //
+     myquery.str("");
+     myquery << "select ID_ROOT_L0 from GL_RUN where RUNHEADER_TIME>" << runinfo->RUNHEADER_TIME << " group by ID_ROOT_L0 order by RUNHEADER_TIME asc limit 5;";
+     //
+     pResult = dbc->Query(myquery.str().c_str());
+     //
+     i = 0;
+     if( pResult ){
+       //
+       Row = pResult->Next();
+       //
+       while ( Row ){
+         //
+         // store infos and exit
+         //
+         l0fid[i] = (UInt_t)atoll(Row->GetField(0));
+         i++;
+         Row = pResult->Next();
+         //
+       };
+       pResult->Delete();
+     };
+     //
+     i = 0;
+     UInt_t previd = 0;
+     while ( i < 10 ){
+       if ( l0fid[i] && previd != l0fid[i] ){
+         previd = l0fid[i];
+         myquery.str("");
+         myquery << "select PATH,NAME from GL_ROOT where ID=" << l0fid[i] << " ;";
+         //
+         pResult = dbc->Query(myquery.str().c_str());
+         //
+         if( pResult ){
+           //
+           Row = pResult->Next();
+           //
+           if ( debug ) printf(" Using inclination informations from file: %s \n",(((TString)gSystem->ExpandPathName(Row->GetField(0)))+"/"+(TString)Row->GetField(1)).Data());
+           ch->Add(((TString)gSystem->ExpandPathName(Row->GetField(0)))+"/"+(TString)Row->GetField(1));
+           //
+           pResult->Delete();
+         };
+       };
+       i++;
+     };
+     //
+     //    l0trm = (TTree*)l0File->Get("Mcmd");
+     //    ch->ls();
+     ch->SetBranchAddress("Mcmd",&mcmdev);
+     //    printf(" entries %llu \n", ch->GetEntries());
+     //    l0trm = ch->GetTree();
+     //    neventsm = l0trm->GetEntries();
+     neventsm = ch->GetEntries();
+     if ( debug ) printf(" entries %u \n", neventsm);
      //    neventsm = 0;
      //
      if (neventsm == 0){
-Line 582 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 743 
 int OrbitalInfoCore(UInt_t run, TFile *f
      }
      //
-     l0trm->SetBranchAddress("Mcmd", &mcmdev);
+     //    l0trm->SetBranchAddress("Mcmd", &mcmdev);
      //    l0trm->SetBranchAddress("Header", &eh);
      //
      //
      //
-     UInt_t mctren = 0;
-     UInt_t mcreen = 0;
+ //    UInt_t mctren = 0;
+ //    UInt_t mcreen = 0;
      UInt_t numrec = 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 sync
+     // 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;
+     vector<Float_t> q2;
+     vector<Float_t> q3;
+     vector<Double_t> qtime;
+     vector<Float_t> qPitch;
+     vector<Float_t> qRoll;
+     vector<Float_t> qYaw;
+     vector<Int_t> qmode;
+     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;
      //
      // run over all the events of the run
      //
      if (verbose) printf("\n Ready to start! \n\n Processed events: \n\n");
      //
-      //
+     //
      for ( re = runinfo->EV_FROM; re < (runinfo->EV_FROM+runinfo->NEVENTS); re++){
        //
        if ( procev%1000 == 0 && procev > 0 && verbose ) printf(" %iK \n",procev/1000);
        if ( debug ) printf(" %i \n",procev);
        //
-       l0head->GetEntry(re);
+       if ( l0head->GetEntry(re) <= 0 ) throw -36;
        //
        // absolute time of this event
        //
        ph = eh->GetPscuHeader();
        atime = dbtime->DBabsTime(ph->GetOrbitalTime());
+       if ( debug ) printf(" %i absolute time \n",procev);
        //
        // paranoid check
        //
        if ( (atime > (runinfo->RUNTRAILER_TIME+1)) || (atime < (runinfo->RUNHEADER_TIME-1))  ) {
          if (verbose) printf(" OrbitalInfo - WARNING: event at time outside the run time window, skipping it\n");
          jumped++;
- //      debug = true;
+         //      debug = true;
          continue;
        }
-Line 651 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 843 
 int OrbitalInfoCore(UInt_t run, TFile *f
          //
          tof->Clear();
          //
-         ttof->GetEntry(itr);
+         if ( ttof->GetEntry(itr) <= 0 ) throw -36;
          //
        };
        //
-Line 659 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 851 
 int OrbitalInfoCore(UInt_t run, TFile *f
        //
        // start processing
        //
+       if ( debug ) printf(" %i start processing \n",procev);
        orbitalinfo->Clear();
        //
        OrbitalInfoTrkVar *t_orb = new OrbitalInfoTrkVar();
-Line 670 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 863 
 int OrbitalInfoCore(UInt_t run, TFile *f
        orbitalinfo->pkt_num = ph->GetCounter();
        orbitalinfo->OBT = ph->GetOrbitalTime();
        orbitalinfo->absTime = atime;
+       if ( debug ) printf(" %i pktnum obt abstime \n",procev);
        //
        // Propagate the orbit from the tle time to atime, using SGP(D)4.
        //
+       if ( debug ) printf(" %i sgp4 \n",procev);
        cCoordGeo coo;
-       float jyear=0;
+       Float_t jyear=0.;
        //
        if(atime >= gltle->GetToTime()) {
          if ( !gltle->Query(atime, dbc) ){
            //
            // Compute the magnetic dipole moment.
            //
+           if ( debug ) printf(" %i compute magnetic dipole moment \n",procev);
            UInt_t year, month, day, hour, min, sec;
            //
            TTimeStamp t = TTimeStamp(atime, kTRUE);
-Line 688 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 884 
 int OrbitalInfoCore(UInt_t run, TFile *f
            t.GetTime(kTRUE, 0, &hour, &min, &sec);
            jyear = (float) year
              + (month*31.+ (float) day)/365.
-             + (hour*3600.+min*60.+(float)sec)/(24*3600*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);
          } else {
            code = -56;
            goto closeandexit;
-Line 705 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 904 
 int OrbitalInfoCore(UInt_t run, TFile *f
        // synchronize with quaternions data
        //
        if ( isf && neventsm>0 ){
-         if ( debug ) printf(" I am here \n");
          //
          // First event
          //
          isf = false;
          upperqtime = atime;
          lowerqtime = runinfo->RUNHEADER_TIME;
-         for ( ik = 0; ik < neventsm; ik++){
+         for ( ik = 0; ik < neventsm; ik++){  //number of macrocommad packets
-           l0trm->GetEntry(ik);
+           if ( ch->GetEntry(ik) <= 0 ) throw -36;
            tmpSize = mcmdev->Records->GetEntries();
            numrec = tmpSize;
-           for (Int_t j3 = 0;j3<tmpSize;j3++){
+           for (Int_t j3 = 0;j3<tmpSize;j3++){  //number of subpackets
-             if ( debug ) printf(" eh eh eh \n");
+             if ( debug ) printf(" ik %i j3 %i eh eh eh \n",ik,j3);
              mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(j3);
-             if ((int)mcmdrc->ID1 == 226){
+             if ( mcmdrc ){ // missing inclination bug [8RED 090116]
-               L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
+               if ( debug ) printf(" pluto \n");
-               for (UInt_t ui = 0; ui < 6; ui++){
+               if ((int)mcmdrc->ID1 == 226 && mcmdrc->Mcmd_Block_crc_ok == 1){ //Check that it is Inclination Packet
-                 if (ui>0){
+                 L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
-                   if (L_QQ_Q_l_upper->time[ui]>L_QQ_Q_l_upper->time[0]){
+                 for (UInt_t ui = 0; ui < 6; ui++){
-                     if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000))<atime){
+                   if (ui>0){
-                       upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));
+                     if (L_QQ_Q_l_upper->time[ui]>L_QQ_Q_l_upper->time[0]){
-                       orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
+                         if ( debug ) printf(" here1 %i \n",ui);
-                       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]);
+                       Double_t u_time = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));
-                     }else {
+                       Int_t recSize = recqtime.size();
-                       lowerqtime = upperqtime;
+                       if(lowerqtime > recqtime[recSize-1]){
-                       upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));
+                           Int_t sizeqmcmd = qtime.size();
-                       orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
+                           inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
-                       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]);
+                           qtime[sizeqmcmd]=u_time;
-                       mcreen = j3;
+                           q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][0];
-                       mctren = ik;
+                           q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][1];
-                       if(fgh==0){
+                           q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][2];
-                         CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
+                           q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][3];
-                         CopyAng(RYPang_lower,RYPang_upper);
+                           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;
+                       }
+                       for(Int_t mu = nt;mu<recSize;mu++){
+                         if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){
+                           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;
+                           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;
+                         }
                        }
-                       oi=ui;
-                       goto closethisloop;
                      }
-                     fgh++;
+                   }else{
-                     CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
+                         if ( debug ) printf(" here2 %i \n",ui);
-                     CopyAng(RYPang_lower,RYPang_upper);
+                     Double_t u_time = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-                   }
+                     if(lowerqtime>u_time)nt=0;
-                 }else{
+                     Int_t recSize = recqtime.size();
-                   if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))<atime){
+                     if(lowerqtime > recqtime[recSize-1]){
-                     upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
+                         Int_t sizeqmcmd = qtime.size();
-                     orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
+                         inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
-                     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]);
+                         qtime[sizeqmcmd]=u_time;
-                   }
+                         q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][0];
-                   else {
+                         q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][1];
-                     lowerqtime = upperqtime;
+                         q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][2];
-                     upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
+                         q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][3];
-                     orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
+                         qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui);
-                     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]);
+                         lowerqtime = u_time;
-                     mcreen = j3;
+                         orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi);
-                     mctren = ik;
+                         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]);
-                     if(fgh==0){
+                         qRoll[sizeqmcmd]=RYPang_upper->Kren;
-                       CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
+                         qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
-                       CopyAng(RYPang_lower,RYPang_upper);
+                         qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
-                       lowerqtime = atime-1;
+                     }
+                     for(Int_t mu = nt;mu<recSize;mu++){
+                       if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){
+                         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;
+                         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;
+                       }
                      }
-                     oi=ui;
-                     goto closethisloop;
-                     //_0 = true;
                    }
-                   fgh++;
+                 }
-                   CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
-                   CopyAng(RYPang_lower,RYPang_upper);
-                   //_0 = true;
-                 };
-                 //cin>>grib;
-               };
-             };
-           };
-         };
-       };
-     closethisloop:
-       //
-       if ( debug ) printf(" I am There \n");
-       //
-       if (((atime>(UInt_t)upperqtime)||(atime<(UInt_t)lowerqtime)) && neventsm>0 ){
-         if ( debug ) printf(" I am there \n");
-         //
-         lowerqtime = upperqtime;
-         Long64_t maxloop = 100000000LL;
-         Long64_t mn = 0;
-         bool gh=false;
-         ooi=oi;
-         if ( verbose ) printf(" OrbitalInfoCore: sync with quaternions data upperqtime %u lowerqtime %u atime %u \n",(UInt_t)upperqtime,(UInt_t)lowerqtime,atime);
-         while (!gh){
-           if ( mn > maxloop ){
-             if ( verbose ) printf(" OrbitalInfoCore: quaternions sync out of range! exiting\n");
-             gh = true;
-             neventsm = 0;
-           };
-           mn++;
-           if (oi<5) oi++;
-           else oi=0;
-           if (oi==0 && numrec > 0){
-             if ( debug ) printf(" mumble \n");
-             mcreen++;
-             if (mcreen == numrec){
-               mctren++;
-               mcreen = 0;
-               l0trm->GetEntry(mctren);
-               numrec = mcmdev->Records->GetEntries();
-             }
-             CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
-             CopyAng(RYPang_lower,RYPang_upper);
-             mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(mcreen);
-             if ((int)mcmdrc->ID1 == 226){
-               L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
-               upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-               if (upperqtime<lowerqtime){
-                 upperqtime=runinfo->RUNTRAILER_TIME;
-                 CopyQ(L_QQ_Q_l_upper,L_QQ_Q_l_lower);
-                 CopyAng(RYPang_upper,RYPang_lower);
-               }else{
-                 orbits.getPosition((double) (upperqtime - 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]);
                }
-               //              re--;
-               gh=true;
              }
-           }else{
+             if ( debug ) printf(" ciccio \n");
-             if ((Int_t)L_QQ_Q_l_upper->time[oi]>(Int_t)L_QQ_Q_l_upper->time[0]){
-               upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-               orbits.getPosition((double) (upperqtime - 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[oi][0],L_QQ_Q_l_upper->quat[oi][1],L_QQ_Q_l_upper->quat[oi][2],L_QQ_Q_l_upper->quat[oi][3]);
-               orbits.getPosition((double) (lowerqtime - gltle->GetFromTime())/60., &eCi);
-               RYPang_lower->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[oi-1][0],L_QQ_Q_l_upper->quat[oi-1][1],L_QQ_Q_l_upper->quat[oi-1][2],L_QQ_Q_l_upper->quat[oi-1][3]);
-               //              re--;
-               gh=true;
-             };
-           };
-         };
-         if ( verbose ) printf(" OrbitalInfoCore: sync with quaternions data now we have upperqtime %u lowerqtime %u atime %u \n",(UInt_t)upperqtime,(UInt_t)lowerqtime,atime);
-       };
-       //
-       if ( debug ) printf(" I am THIS \n");
-       //
-       // Fill in quaternions and angles
-       //
-       if ((atime<=(UInt_t)upperqtime)&&(atime>=(UInt_t)lowerqtime)&& neventsm>0){
-         if ( debug ) printf(" I am this \n");
-         UInt_t tut = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi);
-         if (oi == 0){
-           if ((tut!=5)||(tut!=6)){
-             incli = (L_QQ_Q_l_upper->quat[0][0]-L_QQ_Q_l_lower->quat[ooi][0])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-             orbitalinfo->q0 =  incli*atime+L_QQ_Q_l_upper->quat[0][0]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-             incli =     (L_QQ_Q_l_upper->quat[0][1]-L_QQ_Q_l_lower->quat[ooi][1])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-             orbitalinfo->q1 =  incli*atime+L_QQ_Q_l_upper->quat[0][1]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-             incli = (L_QQ_Q_l_upper->quat[0][2]-L_QQ_Q_l_lower->quat[ooi][2])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-             orbitalinfo->q2 =  incli*atime+L_QQ_Q_l_upper->quat[0][2]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-             incli = (L_QQ_Q_l_upper->quat[0][3]-L_QQ_Q_l_lower->quat[ooi][3])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-             orbitalinfo->q3 =  incli*atime+L_QQ_Q_l_upper->quat[0][3]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-             incli = (RYPang_upper->Tangazh-RYPang_lower->Tangazh)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-             orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-             incli = (RYPang_upper->Ryskanie-RYPang_lower->Ryskanie)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-             orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-             incli = (RYPang_upper->Kren-RYPang_lower->Kren)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000)));
-             orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
            }
-           if (tut==6){
+         }
-             if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){
-               incli = (L_QQ_Q_l_upper->quat[0][0]-L_QQ_Q_l_lower->quat[ooi][0])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-               orbitalinfo->q0 =  incli*atime+L_QQ_Q_l_upper->quat[0][0]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-               incli =           (L_QQ_Q_l_upper->quat[0][1]-L_QQ_Q_l_lower->quat[ooi][1])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-               orbitalinfo->q1 =  incli*atime+L_QQ_Q_l_upper->quat[0][1]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-               incli = (L_QQ_Q_l_upper->quat[0][2]-L_QQ_Q_l_lower->quat[ooi][2])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-               orbitalinfo->q2 =  incli*atime+L_QQ_Q_l_upper->quat[0][2]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-               incli = (L_QQ_Q_l_upper->quat[0][3]-L_QQ_Q_l_lower->quat[ooi][3])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
-               orbitalinfo->q3 =  incli*atime+L_QQ_Q_l_upper->quat[0][3]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
-               incli = (RYPang_upper->Tangazh-RYPang_lower->Tangazh)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
+         if(qtime.size()==0){
-               orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
+             for(UInt_t my=0;my<recqtime.size();my++){
-               incli = (RYPang_upper->Ryskanie-RYPang_lower->Ryskanie)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
+                 Int_t sizeqmcmd = qtime.size();
-               orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
+                 inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
-               //cout<<"upper = "<<RYPang_upper->Ryskanie<<" lower = "<<RYPang_lower->Ryskanie<<" timeupper[0] = "<<L_QQ_Q_l_upper->time[0]-5500000<<" timelower["<<ooi<<"] = "<<L_QQ_Q_l_lower->time[ooi]-5500000<<" Ryscanie = "<<orbitalinfo->phi<<" incli = "<<incli<<" upper-lower = "<<RYPang_upper->Ryskanie-RYPang_lower->Ryskanie<<" Dtime = "<<dbtime->DBabsTime((UInt_t)L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)<<"-"<<dbtime->DBabsTime((UInt_t)L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)<<" atime = "<<atime<<"\n";
+                 qtime[sizeqmcmd]=recqtime[my];
-               //cin>>grib;
+                 q0[sizeqmcmd]=recq0[my];
-               incli = (RYPang_upper->Kren-RYPang_lower->Kren)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_lower->time[ooi]*1000-DeltaOBT*1000)));
+                 q1[sizeqmcmd]=recq1[my];
-               orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
+                 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;
              }
-           }
+         }
-         } else {
-           if((tut!=6)||(tut!=7)||(tut!=9)){
-             incli = (L_QQ_Q_l_upper->quat[oi][0]-L_QQ_Q_l_upper->quat[oi-1][0])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-             orbitalinfo->q0 =  incli*atime+L_QQ_Q_l_upper->quat[oi][0]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-             incli = (L_QQ_Q_l_upper->quat[oi][1]-L_QQ_Q_l_upper->quat[oi-1][1])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-             orbitalinfo->q1 =  incli*atime+L_QQ_Q_l_upper->quat[oi][1]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-             incli = (L_QQ_Q_l_upper->quat[oi][2]-L_QQ_Q_l_upper->quat[oi-1][2])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-             orbitalinfo->q2 =  incli*atime+L_QQ_Q_l_upper->quat[oi][2]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-             incli = (L_QQ_Q_l_upper->quat[oi][3]-L_QQ_Q_l_upper->quat[oi-1][3])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-             orbitalinfo->q3 =  incli*atime+L_QQ_Q_l_upper->quat[oi][3]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-             incli = (RYPang_upper->Tangazh-RYPang_lower->Tangazh)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
+         if ( debug ) printf(" fuffi \n");
-             orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-             incli = (RYPang_upper->Ryskanie-RYPang_lower->Ryskanie)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
+         if ( debug ) printf(" puffi \n");
-             orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
+         Double_t tmin = 9999999999.;
-             //cout<<"upper = "<<RYPang_upper->Ryskanie<<" lower = "<<RYPang_lower->Ryskanie<<" timeupper["<<oi<<"] = "<<L_QQ_Q_l_upper->time[oi]-5500000<<" timelower["<<oi-1<<"] = "<<L_QQ_Q_l_lower->time[oi-1]-5500000<<" Ryscanie = "<<orbitalinfo->phi<<" incli = "<<incli<<" upper-lower = "<<RYPang_upper->Ryskanie-RYPang_lower->Ryskanie<<" Dtime = "<<dbtime->DBabsTime((UInt_t)L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)<<"-"<<dbtime->DBabsTime((UInt_t)L_QQ_Q_l_lower->time[oi-1]*1000-DeltaOBT*1000)<<" atime = "<<atime<<"\n";
+         Double_t tmax = 0.;
-             //cin>>grib;
+         for(UInt_t tre = 0;tre<qtime.size();tre++){
-             incli = (RYPang_upper->Kren-RYPang_lower->Kren)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
+           if(qtime[tre]>tmax)tmax = qtime[tre];
-             orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
+           if(qtime[tre]<tmin)tmin = qtime[tre];
+         }
+         if ( debug ) printf(" gnfuffi \n");
+       } // if we processed first event
+       //Filling Inclination information
+       Double_t incli = 0;
+       if ( qtime.size() > 1 ){
+       for(UInt_t mu = must;mu<qtime.size()-1;mu++){
+         if ( debug ) printf(" ??grfuffi %i sixe %i must %i \n",mu,qtime.size()-1,must);
+         if(qtime[mu+1]>qtime[mu]){
+           if ( debug ) printf(" grfuffi2 %i \n",mu);
+           if(atime<=qtime[mu+1] && atime>=qtime[mu]){
+             must = mu;
+             incli = (qPitch[mu+1]-qPitch[mu])/(qtime[mu+1]-qtime[mu]);
+             orbitalinfo->theta =  incli*atime+qPitch[mu+1]-incli*qtime[mu+1];
+             incli = (qRoll[mu+1]-qRoll[mu])/(qtime[mu+1]-qtime[mu]);
+             orbitalinfo->etha =  incli*atime+qRoll[mu+1]-incli*qtime[mu+1];
+             incli = (qYaw[mu+1]-qYaw[mu])/(qtime[mu+1]-qtime[mu]);
+             orbitalinfo->phi =  incli*atime+qYaw[mu+1]-incli*qtime[mu+1];
+             incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
+             orbitalinfo->q0 =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
+             incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
+             orbitalinfo->q1 =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
+             incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
+             orbitalinfo->q2 =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
+             incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
+             orbitalinfo->q3 =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
+             orbitalinfo->TimeGap = qtime[mu+1]-qtime[mu];
+             orbitalinfo->mode = qmode[mu+1];
+             //if(qmode[mu+1]==-10) orbitalinfo->R10r = true;else orbitalinfo->R10r = false;
+             //reserved for next versions Vitaly.
+             /*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){
+               //linear interpolation
+               incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
+               orbitalinfo->q0 =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
+               incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
+               orbitalinfo->q1 =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
+               incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
+               orbitalinfo->q2 =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
+               incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
+               orbitalinfo->q3 =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
+             }else{
+               //sine interpolation
+               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 (tut==6){
-             if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){
-               incli = (L_QQ_Q_l_upper->quat[oi][0]-L_QQ_Q_l_upper->quat[oi-1][0])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-               orbitalinfo->q0 =  incli*atime+L_QQ_Q_l_upper->quat[oi][0]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-               incli = (L_QQ_Q_l_upper->quat[oi][1]-L_QQ_Q_l_upper->quat[oi-1][1])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-               orbitalinfo->q1 =  incli*atime+L_QQ_Q_l_upper->quat[oi][1]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-               incli = (L_QQ_Q_l_upper->quat[oi][2]-L_QQ_Q_l_upper->quat[oi-1][2])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-               orbitalinfo->q2 =  incli*atime+L_QQ_Q_l_upper->quat[oi][2]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-               incli = (L_QQ_Q_l_upper->quat[oi][3]-L_QQ_Q_l_upper->quat[oi-1][3])/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-               orbitalinfo->q3 =  incli*atime+L_QQ_Q_l_upper->quat[oi][3]-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-               incli = (RYPang_upper->Tangazh-RYPang_lower->Tangazh)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-               orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-               incli = (RYPang_upper->Ryskanie-RYPang_lower->Ryskanie)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-               orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-               //cout<<"upper = "<<RYPang_upper->Ryskanie<<" lower = "<<RYPang_lower->Ryskanie<<" timeupper["<<oi<<"] = "<<L_QQ_Q_l_upper->time[oi]-5500000<<" timelower["<<oi-1<<"] = "<<L_QQ_Q_l_lower->time[oi-1]-5500000<<" Ryscanie = "<<orbitalinfo->phi<<" incli = "<<incli<<" upper-lower = "<<RYPang_upper->Ryskanie-RYPang_lower->Ryskanie<<" Dtime = "<<dbtime->DBabsTime((UInt_t)L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)<<"-"<<dbtime->DBabsTime((UInt_t)L_QQ_Q_l_lower->time[oi-1]*1000-DeltaOBT*1000)<<" atime = "<<atime<<"\n";
-               //cin>>grib;
-               incli = (RYPang_upper->Kren-RYPang_lower->Kren)/(dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000))-dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi-1]*1000-DeltaOBT*1000)));
-               orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
-             }
-           }
          }
-         //
+       }
-         orbitalinfo->mode = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi);
+       }
-         //
-       } else {
-         if ( debug ) printf(" ops no incl! \n");
-         orbitalinfo->mode = 10;
-       };
        //
        // 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 ){
          orbitalinfo->mode = 10;
          orbitalinfo->q0 = -1000.;
-Line 978 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1202 
 int OrbitalInfoCore(UInt_t run, TFile *f
          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); //
+         /*
+ ---------- 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->mode != 10 && orbitalinfo->mode != 5 && orbitalinfo->mode !=7 && orbitalinfo->mode != 9 ){
+       if( orbitalinfo->TimeGap>0 && orbitalinfo->TimeGap<2000000){
          //
-         Float_t Bx = -orbitalinfo->Bdown;                       //don't need for PamExp ExpOnly for all geography areas
+         Float_t Bx = -orbitalinfo->Bdown;
-         Float_t By = orbitalinfo->Beast;                        //don't need for PamExp ExpOnly for all geography areas
+         Float_t By = orbitalinfo->Beast;
-         Float_t Bz = orbitalinfo->Bnorth;                       //don't need for PamExp ExpOnly for all geography areas
+         Float_t Bz = orbitalinfo->Bnorth;
          //
          TMatrixD Fij = PO->ECItoGreenwich(PO->QuatoECI(orbitalinfo->q0,orbitalinfo->q1,orbitalinfo->q2,orbitalinfo->q3),orbitalinfo->absTime);
+         TMatrixD Gij = PO->ColPermutation(Fij);
          TMatrixD Dij = PO->GreenwichtoGEO(orbitalinfo->lat,orbitalinfo->lon,Fij);
          TMatrixD Iij = PO->ColPermutation(Dij);
          //
-Line 1003 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1249 
 int OrbitalInfoCore(UInt_t run, TFile *f
          A1 = Iij(0,2);
          A2 = Iij(1,2);
          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
          //
-Line 1021 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1267 
 int OrbitalInfoCore(UInt_t run, TFile *f
              Double_t E22z = zin[3];
              if ( (E11x < 100. && E11y < 100. && E22x < 100. && E22y < 100.) || ptt->trkseqno != -1  ){
                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));
+               //              Double_t MyAzim = TMath::RadToDeg()*atan(TMath::Abs(E22y-E11y)/TMath::Abs(E22x-E11x));
-               if(E22x-E11x>=0 && E22y-E11y <0) MyAzim =  360. - MyAzim;
+               //              if(E22x-E11x>=0 && E22y-E11y <0) MyAzim =  360. - MyAzim;
-               if(E22x-E11x>=0 && E22y-E11y >=0) MyAzim = MyAzim;
+               //              if(E22x-E11x>=0 && E22y-E11y >=0) MyAzim = MyAzim;
-               if(E22x-E11x<0 && E22y-E11y >0) MyAzim = 180. - MyAzim;
+               //              if(E22x-E11x<0 && E22y-E11y >0) MyAzim = 180. - MyAzim;
-               if(E22x-E11x<0 && E22y-E11y <0) MyAzim = 180. + MyAzim;
+               //              if(E22x-E11x<0 && E22y-E11y <0) MyAzim = 180. + MyAzim;
                Px = (E22x-E11x)/norm;
                Py = (E22y-E11y)/norm;
                Pz = (E22z-E11z)/norm;
-Line 1036 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1282 
 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;
                //
-Line 1047 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1293 
 int OrbitalInfoCore(UInt_t run, TFile *f
                //
                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 ( debug ) printf(" orbitalinfo->cutoffsvl %f vitaly %f \n",orbitalinfo->cutoffsvl,t_orb->cutoff);
                //
                new(tor[nn]) OrbitalInfoTrkVar(*t_orb);
-Line 1061 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1310 
 int OrbitalInfoCore(UInt_t run, TFile *f
            if ( debug ) printf(" mmm... mode %u standalone %i ntrk %i \n",orbitalinfo->mode,standalone,tof->ntrk());
          };
          //
+       } else {
+         if ( !standalone && tof->ntrk() > 0 ){
+           //
+           Int_t nn = 0;
+           for(Int_t nt=0; nt < tof->ntrk(); nt++){
+             //
+             ToFTrkVar *ptt = tof->GetToFTrkVar(nt);
+             if ( ptt->trkseqno != -1  ){
+               //
+               t_orb->trkseqno = ptt->trkseqno;
+               //
+               t_orb->Eij = 0;
+               //
+               t_orb->Sij = 0;
+               //
+               t_orb->pitch = -1000.;
+               //
+               t_orb->cutoff = -1000.;
+               //
+               new(tor[nn]) OrbitalInfoTrkVar(*t_orb);
+               nn++;
+               //
+               t_orb->Clear();
+               //
+             };
+             //
+           };
+         };
        };
        //
        // Fill the class
-Line 1073 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1350 
 int OrbitalInfoCore(UInt_t run, TFile *f
      //
      // Here you may want to clear some variables before processing another run
      //
+     //gStyle->SetOptStat(000000);
+     //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;*/
+     if ( verbose ) printf(" Clear before new run \n");
      delete dbtime;
-     if ( L_QQ_Q_l_upper ) delete L_QQ_Q_l_upper;
+     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 1097 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1405 
 int OrbitalInfoCore(UInt_t run, TFile *f
          //
          // Get entry from old tree
          //
-         OrbitalInfotrclone->GetEntry(j);
+         if ( OrbitalInfotrclone->GetEntry(j) <= 0 ) throw -36;
          //
          // copy orbitalinfoclone to OrbitalInfo
          //
-Line 1111 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1419 
 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();
+     OrbitalInfotr->Write("OrbitalInfo", TObject::kOverwrite);
    };
    //
+   if (verbose) printf("\n Exiting...\n");
    if ( myfold ) gSystem->Unlink(OrbitalInfofolder.str().c_str());
    //
    // the end
-Line 1137 
 int OrbitalInfoCore(UInt_t run, TFile *f
+Line 1445 
 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 ( 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 1189 
 void CopyAng(InclinationInfo *A1, Inclin
+Line 1513 
 void CopyAng(InclinationInfo *A1, Inclin
  UInt_t holeq(Double_t lower,Double_t upper,Quaternions *Qlower, Quaternions *Qupper, UInt_t f){
    UInt_t hole = 10;
-   bool R10l = false;     // Sign of R10 mode in lower quaternions array
+   Bool_t R10l = false;     // Sign of R10 mode in lower quaternions array
-   bool R10u = false;     // Sign of R10 mode in upper quaternions array
+   Bool_t R10u = false;     // Sign of R10 mode in upper quaternions array
-   bool insm = false;     // Sign that we inside quaternions array
+   Bool_t insm = false;     // Sign that we inside quaternions array
-   bool mxtml = false;    // Sign of mixt mode in lower quaternions array
+   Bool_t mxtml = false;    // Sign of mixt mode in lower quaternions array
-   bool mxtmu = false;    // Sign of mixt mode in upper quaternions array
+   Bool_t mxtmu = false;    // Sign of mixt mode in upper quaternions array
-   bool npasm = false;     // Sign of normall pass between R10 and non R10 or between non R10 and R10
+   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
    if (f>0){
-Line 1237 
 UInt_t holeq(Double_t lower,Double_t upp
+Line 1561 
 UInt_t holeq(Double_t lower,Double_t upp
    return hole;
  }
+ void inclresize(vector<Double_t>& t,vector<Float_t>& q0,vector<Float_t>& q1,vector<Float_t>& q2,vector<Float_t>& q3,vector<Int_t>& mode,vector<Float_t>& Roll,vector<Float_t>& Pitch,vector<Float_t>& Yaw){
+   Int_t sizee = t.size()+1;
+   t.resize(sizee);
+   q0.resize(sizee);
+   q1.resize(sizee);
+   q2.resize(sizee);
+   q3.resize(sizee);
+   mode.resize(sizee);
+   Roll.resize(sizee);
+   Pitch.resize(sizee);
+   Yaw.resize(sizee);
+ }
+ //Find fitting sine functions for q0,q1,q2,q3 and Yaw-angle;
+ 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;
+   UInt_t munow = 0;
+   UInt_t munext = 0;
+   Bool_t increase = false;
+   Bool_t decrease = false;
+   Bool_t Max_is_defined = false;
+   Bool_t Start_point_is_defined = false;
+   Bool_t Period_is_defined = false;
+   Bool_t Large_gap = false;
+   Bool_t normal_way = true;
+   Bool_t small_gap_on_ridge = false;
+   Double_t t1 = 0;
+   Double_t t1A = 0;
+   Int_t sinesize = 0;
+   Int_t nfi = 0;
+   for(UInt_t mu = 0;mu<qtime.size();mu++){
+     //cout<<"Roll["<<mu<<"] = "<<Roll[mu]<<endl;
+     if(TMath::Abs(Roll[mu])<1. && TMath::Abs(Pitch[mu])<1. && TMath::Abs(q[mu])<limsin){
+     //cout<<"q["<<mu<<endl<<"] = "<<q[mu]<<endl;
+     if(mulast!=0 && munow!=0 && munext!=0){mulast=munow;munow=munext;munext=mu;}
+     if(munext==0 && munow!=0)munext=mu;
+     if(munow==0 && mulast!=0)munow=mu;
+     if(mulast==0)mulast=mu;
+     //cout<<"mulast = "<<mulast<<"\tmunow = "<<munow<<"\tmunext = "<<munext<<endl;
+     //Int_t ref;
+     //cin>>ref;
+     if(TMath::Abs(q[munow])>TMath::Abs(q[mulast]) && TMath::Abs(q[munow])>TMath::Abs(q[munext]) && q[mulast]*q[munext]>0 && qtime[munext]-qtime[mulast]>400)small_gap_on_ridge = true;
+     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(normal_way)cout<<"Normal_Way"<<endl;
+     if(Large_gap || small_gap_on_ridge){
+       //cout<<"Large gap..."<<endl;
+       //if(small_gap_on_ridge)cout<<"small gap..."<<endl;
+       //cout<<"q["<<mulast<<"] = "<<q[mulast]<<"\tq["<<munow<<"] = "<<q[munow]<<"\tq["<<munext<<"] = "<<q[munext]<<endl;
+       //cout<<"qtime["<<mulast<<"] = "<<qtime[mulast]<<"\tqtime["<<munow<<"] = "<<qtime[munow]<<"\tqtime["<<munext<<"] = "<<qtime[munext]<<endl;
+       increase = false;
+       decrease = false;
+       if(nfi>0){
+         qsine.resize(qsine.size()-1);
+         sinesize = qsine.size();
+         //cout<<"nfi was larger then zero"<<endl;
+       }else{
+         //cout<<"nfi was not larger then zero :( nfi = "<<nfi<<endl;
+         //cout<<"qsine.size = "<<qsine.size()<<endl;
+         if(!Period_is_defined){
+           //cout<<"Period was defined"<<endl;
+           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){
+           //cout<<"Max was already defined"<<endl;
+           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];
+       //cout<<"finish point before large gap = "<<qtime[munow]<<endl;
+       nfi = 0;
+       Max_is_defined = false;
+       Start_point_is_defined = false;
+       Period_is_defined = false;
+       small_gap_on_ridge = false;
+     }
+     //cout<<"Slope "<<increase<<"\t"<<decrease<<endl;
+     //cout<<"mulast = "<<mulast<<"\tmunow = "<<munow<<"\tmunext = "<<munext<<endl;
+     if((munext>munow) && (munow>mulast) && normal_way){
+       if(!increase && !decrease){
+         //cout<<"Normal way have started"<<endl;
+         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])>0.9*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){
+           Double_t qPer = qtime[munow]-t1A;
+           if(qPer>1000){
+             //cout<<"qsine["<<sinesize-1<<"] = "<<qPer<<" = "<<qtime[munow]<<" - "<<t1A<<"\tlim = "<<limsin<<endl;
+             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;
+         qsine[sinesize-1].A = TMath::Abs(q[munow]);
+         if(Start_point_is_defined && Period_is_defined){
+           qsine[sinesize-1].finishPoint = qtime[munow];
+           nfi++;
+           qsine[sinesize-1].NeedFit = false;
+           Max_is_defined = false;
+           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];
+       }
+       //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;
+       if(((q[munow]>=0 && q[mulast]<=0) || (q[munow]<=0 && q[mulast]>=0)) && qtime[munow]-qtime[mulast]<2000 && qtime[munext]-qtime[munow]<2000){
+         Double_t tcrosszero = 0;
+         //cout<<"cross zero point...qtime = "<<qtime[munow]<<endl;
+         if(q[munow]==0.) tcrosszero = qtime[munow];else
+           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;
+         }
+       }
+     }
+     }
+   }
+   //cout<<"FINISH SINE INTERPOLATION FUNCTION..."<<endl<<endl;
+ }

 Legend:



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+Added in v.1.60

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