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

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revision 1.31 by mocchiut, Wed Oct 1 15:31:32 2008 UTC revision 1.66 by mocchiut, Mon Feb 3 16:45:14 2014 UTC
# Line 1  Line 1 
 //  
1  // C/C++ headers  // C/C++ headers
2  //  //
3  #include <fstream>  #include <fstream>
# Line 9  Line 8 
8  //  //
9  // ROOT headers  // ROOT headers
10  //  //
11    //#include <TCanvas.h>
12    #include <TH2F.h> //for test only. Vitaly.
13    #include <TVector3.h>
14    //#include <TF1.h>
15    
16  #include <TTree.h>  #include <TTree.h>
17  #include <TClassEdit.h>  #include <TClassEdit.h>
18  #include <TObject.h>  #include <TObject.h>
# Line 44  Line 48 
48  #include <OrbitalInfoCore.h>  #include <OrbitalInfoCore.h>
49  #include <InclinationInfo.h>  #include <InclinationInfo.h>
50    
51    
52  using namespace std;  using namespace std;
53    
54  //  //
# Line 61  int OrbitalInfoCore(UInt_t run, TFile *f Line 66  int OrbitalInfoCore(UInt_t run, TFile *f
66    stringstream myquery;    stringstream myquery;
67    myquery.str("");    myquery.str("");
68    myquery << "SET time_zone='+0:00'";    myquery << "SET time_zone='+0:00'";
69    dbc->Query(myquery.str().c_str());    delete dbc->Query(myquery.str().c_str());
70    //    //
71    TString processFolder = Form("OrbitalInfoFolder_%u",run);    TString processFolder = Form("OrbitalInfoFolder_%u",run);
72    //    //
# Line 117  int OrbitalInfoCore(UInt_t run, TFile *f Line 122  int OrbitalInfoCore(UInt_t run, TFile *f
122    TTree *OrbitalInfotrclone = 0;    TTree *OrbitalInfotrclone = 0;
123    Bool_t reproc = false;    Bool_t reproc = false;
124    Bool_t reprocall = false;    Bool_t reprocall = false;
125      Bool_t igrfloaded = false;
126    UInt_t nobefrun = 0;    UInt_t nobefrun = 0;
127    UInt_t noaftrun = 0;    UInt_t noaftrun = 0;
128    UInt_t numbofrun = 0;    UInt_t numbofrun = 0;
# Line 124  int OrbitalInfoCore(UInt_t run, TFile *f Line 130  int OrbitalInfoCore(UInt_t run, TFile *f
130    TString fname;    TString fname;
131    UInt_t totfileentries = 0;    UInt_t totfileentries = 0;
132    UInt_t idRun = 0;    UInt_t idRun = 0;
133      UInt_t anni5 = 60 * 60 * 24 * 365 * 5 ;//1576800
134    //    //
135    // My variables. Vitaly.    // My variables. Vitaly.
136    //    //
137    //  UInt_t iev = 0;  //  UInt_t oi = 0;
   //  UInt_t j3 = 0;  
   UInt_t oi = 0;  
138    Int_t tmpSize = 0;    Int_t tmpSize = 0;
139    //    //
140    // variables needed to handle error signals    // variables needed to handle error signals
# Line 141  int OrbitalInfoCore(UInt_t run, TFile *f Line 146  int OrbitalInfoCore(UInt_t run, TFile *f
146    //    //
147    OrbitalInfo *orbitalinfo = new OrbitalInfo();    OrbitalInfo *orbitalinfo = new OrbitalInfo();
148    OrbitalInfo *orbitalinfoclone = new OrbitalInfo();    OrbitalInfo *orbitalinfoclone = new OrbitalInfo();
149    
150    //    //
151    // define variables for opening and reading level0 file    // define variables for opening and reading level0 file
152    //    //
153    TFile *l0File = 0;    TFile *l0File = 0;
154    TTree *l0tr = 0;    TTree *l0tr = 0;
155    TTree *l0trm = 0;    //  TTree *l0trm = 0;
156      TChain *ch = 0;
157    // EM: open also header branch    // EM: open also header branch
158    TBranch *l0head = 0;    TBranch *l0head = 0;
159    pamela::EventHeader *eh = 0;    pamela::EventHeader *eh = 0;
# Line 176  int OrbitalInfoCore(UInt_t run, TFile *f Line 183  int OrbitalInfoCore(UInt_t run, TFile *f
183    //    //
184    // IGRF stuff    // IGRF stuff
185    //    //
186    float dimo = 0.0; // dipole moment (computed from dat files)    Double_t dimo = 0.0; // dipole moment (computed from dat files) // EM GCC 4.7
187    float bnorth, beast, bdown, babs;    Float_t bnorth, beast, bdown, babs;
188    float xl; // L value    Float_t xl; // L value
189    float icode; // code value for L accuracy (see fortran code)    Float_t icode; // code value for L accuracy (see fortran code)
190    float bab1; // What's  the difference with babs?    Float_t bab1; // What's  the difference with babs?
191    float stps = 0.005; // step size for field line tracing    Float_t stps = 0.005; // step size for field line tracing
192    float bdel = 0.01; // required accuracy    Float_t bdel = 0.01; // required accuracy
193    float bequ;  // equatorial b value (also called b_0)    Float_t bequ;  // equatorial b value (also called b_0)
194    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
195    float rr0; // equatorial radius normalized to earth radius    Float_t rr0; // equatorial radius normalized to earth radius
196    
197    //    //
198    // Working filename    // Working filename
# Line 209  int OrbitalInfoCore(UInt_t run, TFile *f Line 216  int OrbitalInfoCore(UInt_t run, TFile *f
216    OrbitalInfofolder << tempname.str().c_str();    OrbitalInfofolder << tempname.str().c_str();
217    tempname << "/OrbitalInfotree_run";    tempname << "/OrbitalInfotree_run";
218    tempname << run << ".root";      tempname << run << ".root";  
219      UInt_t totnorun = 0;
220    //    //
221    // DB classes    // DB classes
222    //    //
# Line 218  int OrbitalInfoCore(UInt_t run, TFile *f Line 226  int OrbitalInfoCore(UInt_t run, TFile *f
226    //    //
227    //Quaternions classes    //Quaternions classes
228    //    //
229    Quaternions *L_QQ_Q_l_lower = new Quaternions();    Quaternions *L_QQ_Q_l_lower = 0;
230    InclinationInfo *RYPang_lower = new InclinationInfo();    InclinationInfo *RYPang_lower = 0;
231    Quaternions *L_QQ_Q_l_upper = new Quaternions();    Quaternions *L_QQ_Q_l_upper = 0;
232    InclinationInfo *RYPang_upper = new InclinationInfo();    InclinationInfo *RYPang_upper = 0;
233        
234    cEci eCi;    cEci eCi;
235        
236    // Initialize fortran routines!!!    // Initialize fortran routines!!!
237      Int_t ltp1 = 0;
238    Int_t ltp2 = 0;    Int_t ltp2 = 0;
239    Int_t ltp3 = 0;    Int_t ltp3 = 0;
240    Int_t uno = 1;    //  Int_t uno = 1;
241    char *niente = " ";    //  const char *niente = " ";
242    GL_PARAM *glparam = new GL_PARAM();    GL_PARAM *glparam = new GL_PARAM();
243    GL_PARAM *glparam2 = new GL_PARAM();    GL_PARAM *glparam2 = new GL_PARAM();
244    Int_t parerror=glparam->Query_GL_PARAM(1,301,dbc); // parameters stored in DB in GL_PRAM table    GL_PARAM *glparam3 = new GL_PARAM();
245    
246    //    //
247    // Orientation variables    // Orientation variables. Vitaly
248    //    //
249    UInt_t evfrom = 0;    UInt_t evfrom = 0;
250    UInt_t jumped = 0;    UInt_t jumped = 0;
251    Int_t itr = -1;        Int_t itr = -1;    
252    Double_t A1;    //  Double_t A1;
253    Double_t A2;    //  Double_t A2;
254    Double_t A3;    //  Double_t A3;
255    Double_t Px = 0;    Double_t Px = 0;
256    Double_t Py = 0;          Double_t Py = 0;      
257    Double_t Pz = 0;      Double_t Pz = 0;  
# Line 251  int OrbitalInfoCore(UInt_t run, TFile *f Line 261  int OrbitalInfoCore(UInt_t run, TFile *f
261    Int_t nz = 6;    Int_t nz = 6;
262    Float_t zin[6];    Float_t zin[6];
263    Int_t nevtofl2 = 0;    Int_t nevtofl2 = 0;
264    //      if ( verbose ) cout<<"Reading quaternions external file"<<endl;
265      cout.setf(ios::fixed,ios::floatfield);  
266      /******Reading recovered quaternions...*********/
267      vector<Double_t> recqtime;
268      vector<Float_t> recq0;
269      vector<Float_t> recq1;
270      vector<Float_t> recq2;
271      vector<Float_t> recq3;
272      Float_t Norm = 1;
273      Int_t parerror=glparam->Query_GL_PARAM(1,303,dbc); // parameters stored in DB in GL_PRAM table  
274      ifstream in((glparam->PATH+glparam->NAME).Data(),ios::in);
275    if ( parerror<0 ) {    if ( parerror<0 ) {
276      code = parerror;      code = parerror;
277      goto closeandexit;      goto closeandexit;
278    };    }
279    ltp2 = (Int_t)(glparam->PATH+glparam->NAME).Length();    while(!in.eof()){
280    if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam->PATH+glparam->NAME).Data());      recqtime.resize(recqtime.size()+1);
281    //      Int_t sizee = recqtime.size();
282    parerror=glparam2->Query_GL_PARAM(1,302,dbc); // parameters stored in DB in GL_PRAM table      recq0.resize(sizee);
283    if ( parerror<0 ) {      recq1.resize(sizee);
284      code = parerror;      recq2.resize(sizee);
285      goto closeandexit;      recq3.resize(sizee);
286    };      in>>recqtime[sizee-1];
287    ltp3 = (Int_t)(glparam2->PATH+glparam2->NAME).Length();      in>>recq0[sizee-1];
288    if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam2->PATH+glparam2->NAME).Data());      in>>recq1[sizee-1];
289    //      in>>recq2[sizee-1];
290    initize_((char *)niente,&uno,(char *)(glparam->PATH+glparam->NAME).Data(),&ltp2,(char *)(glparam2->PATH+glparam2->NAME).Data(),&ltp3);      in>>recq3[sizee-1];
291    //      in>>Norm;
292    // End IGRF stuff//    }
293    //    if ( verbose ) cout<<"We have read recovered data"<<endl;
294    
295      // IGRF stuff moved inside run loop!  
296    
297    for (Int_t ip=0;ip<nz;ip++){    for (Int_t ip=0;ip<nz;ip++){
298      zin[ip] = tof->GetZTOF(tof->GetToFPlaneID(ip));      zin[ip] = tof->GetZTOF(tof->GetToFPlaneID(ip));
299    };    };
# Line 342  int OrbitalInfoCore(UInt_t run, TFile *f Line 365  int OrbitalInfoCore(UInt_t run, TFile *f
365    // number of run to be processed    // number of run to be processed
366    //    //
367    numbofrun = runinfo->GetNoRun();    numbofrun = runinfo->GetNoRun();
368    UInt_t totnorun = runinfo->GetRunEntries();    totnorun = runinfo->GetRunEntries();
369    //    //
370    // Try to access the OrbitalInfo tree in the file, if it exists we are reprocessing data if not we are processing a new run    // Try to access the OrbitalInfo tree in the file, if it exists we are reprocessing data if not we are processing a new run
371    //    //
# Line 376  int OrbitalInfoCore(UInt_t run, TFile *f Line 399  int OrbitalInfoCore(UInt_t run, TFile *f
399        //        //
400        reprocall = true;        reprocall = true;
401        //        //
402        if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing all runs\n");        if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing all runs\n Deleting old tree...\n");
403        //        //
404      } else {      } else {
405        //        //
# Line 394  int OrbitalInfoCore(UInt_t run, TFile *f Line 417  int OrbitalInfoCore(UInt_t run, TFile *f
417        tempOrbitalInfo = OrbitalInfotrclone->CloneTree(-1,"fast");        tempOrbitalInfo = OrbitalInfotrclone->CloneTree(-1,"fast");
418        tempOrbitalInfo->SetName("OrbitalInfo-old");        tempOrbitalInfo->SetName("OrbitalInfo-old");
419        tempfile->Write();        tempfile->Write();
420          tempOrbitalInfo->Delete();
421        tempfile->Close();          tempfile->Close();  
422      }      }
423      //      //
424      // Delete the old tree from old file and memory      // Delete the old tree from old file and memory
425      //      //
426        OrbitalInfotrclone->Clear();
427      OrbitalInfotrclone->Delete("all");      OrbitalInfotrclone->Delete("all");
428      //      //
429      if (verbose) printf(" ...done!\n");      if (verbose) printf(" ...done!\n");
# Line 430  int OrbitalInfoCore(UInt_t run, TFile *f Line 455  int OrbitalInfoCore(UInt_t run, TFile *f
455        }        }
456        for (UInt_t j = 0; j < nobefrun; j++){        for (UInt_t j = 0; j < nobefrun; j++){
457          //          //
458          OrbitalInfotrclone->GetEntry(j);                    if ( OrbitalInfotrclone->GetEntry(j) <= 0 ) throw -36;    
459          //          //
460          // copy orbitalinfoclone to mydec          // copy orbitalinfoclone to mydec
461          //          //
# Line 444  int OrbitalInfoCore(UInt_t run, TFile *f Line 469  int OrbitalInfoCore(UInt_t run, TFile *f
469          //          //
470        };        };
471        if (verbose) printf(" Finished successful copying!\n");        if (verbose) printf(" Finished successful copying!\n");
472      };                };
473    };    };
474    //    //
475      //
476    // Get the list of run to be processed, if only one run has to be processed the list will contain one entry only.    // Get the list of run to be processed, if only one run has to be processed the list will contain one entry only.
477    //    //
478    runlist = runinfo->GetRunList();    runlist = runinfo->GetRunList();
# Line 454  int OrbitalInfoCore(UInt_t run, TFile *f Line 480  int OrbitalInfoCore(UInt_t run, TFile *f
480    // Loop over the run to be processed    // Loop over the run to be processed
481    //    //
482    for (UInt_t irun=0; irun < numbofrun; irun++){    for (UInt_t irun=0; irun < numbofrun; irun++){
483    
484        L_QQ_Q_l_lower = new Quaternions();
485        RYPang_lower = new InclinationInfo();
486        L_QQ_Q_l_upper = new Quaternions();
487        RYPang_upper = new InclinationInfo();
488    
489      //      //
490      // retrieve the first run ID to be processed using the RunInfo list      // retrieve the first run ID to be processed using the RunInfo list
491      //      //
# Line 502  int OrbitalInfoCore(UInt_t run, TFile *f Line 534  int OrbitalInfoCore(UInt_t run, TFile *f
534      fname = ftmpname.str().c_str();      fname = ftmpname.str().c_str();
535      ftmpname.str("");      ftmpname.str("");
536      //      //
537      // print out informations      // print nout informations
538      //      //
539      totevent = runinfo->NEVENTS;      totevent = runinfo->NEVENTS;
540      evfrom = runinfo->EV_FROM;      evfrom = runinfo->EV_FROM;
# Line 516  int OrbitalInfoCore(UInt_t run, TFile *f Line 548  int OrbitalInfoCore(UInt_t run, TFile *f
548      //      //
549      //    if ( !totevent ) goto closeandexit;      //    if ( !totevent ) goto closeandexit;
550      // Open Level0 file      // Open Level0 file
551        if ( l0File ) l0File->Close();
552      l0File = new TFile(fname.Data());      l0File = new TFile(fname.Data());
553      if ( !l0File ) {      if ( !l0File ) {
554        if ( debug ) printf(" OrbitalInfo - ERROR: problems opening Level0 file\n");        if ( debug ) printf(" OrbitalInfo - ERROR: problems opening Level0 file\n");
# Line 554  int OrbitalInfoCore(UInt_t run, TFile *f Line 587  int OrbitalInfoCore(UInt_t run, TFile *f
587        code = -12;        code = -12;
588        goto closeandexit;        goto closeandexit;
589      };      };
590    
591        //
592        // open IGRF files and do it only once if we are processing a full level2 file
593        //
594        if ( reprocall && !igrfloaded ){
595    
596          if ( l0head->GetEntry(runinfo->EV_FROM) > 0 ){
597            igrfloaded = true;
598          //
599          // absolute time of first event of the run (it should not matter a lot)
600          //
601          ph = eh->GetPscuHeader();
602          atime = dbtime->DBabsTime(ph->GetOrbitalTime());
603          
604          parerror=glparam->Query_GL_PARAM(atime-anni5,301,dbc); // parameters stored in DB in GL_PRAM table  
605          if ( parerror<0 ) {
606            code = parerror;
607            goto closeandexit;
608          }
609          ltp1 = (Int_t)(glparam->PATH+glparam->NAME).Length();
610          if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam->PATH+glparam->NAME).Data());
611          //
612          parerror=glparam2->Query_GL_PARAM(atime,301,dbc); // parameters stored in DB in GL_PRAM table  
613          if ( parerror<0 ) {
614            code = parerror;
615            goto closeandexit;
616          }
617          ltp2 = (Int_t)(glparam2->PATH+glparam2->NAME).Length();
618          if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam2->PATH+glparam2->NAME).Data());
619          //
620          parerror=glparam3->Query_GL_PARAM(atime,302,dbc); // parameters stored in DB in GL_PRAM table
621          if ( parerror<0 ) {
622            code = parerror;
623            goto closeandexit;
624          }
625          ltp3 = (Int_t)(glparam3->PATH+glparam3->NAME).Length();
626          if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam3->PATH+glparam3->NAME).Data());
627          //
628          initize_((char *)(glparam->PATH+glparam->NAME).Data(),&ltp1,(char *)(glparam2->PATH+glparam2->NAME).Data(),&ltp2,(char *)(glparam3->PATH+glparam3->NAME).Data(),&ltp3);
629          //
630          }
631        }
632        //
633        // End IGRF stuff//
634        //
635    
636        //
637        //     TTree *tp = (TTree*)l0File->Get("RunHeader");
638        //     tp->SetBranchAddress("Header", &eH);
639        //     tp->SetBranchAddress("RunHeader", &reh);
640        //     tp->GetEntry(0);
641        //     ph = eH->GetPscuHeader();
642        //     ULong_t TimeSync = reh->LAST_TIME_SYNC_INFO;
643        //     ULong_t ObtSync = reh->OBT_TIME_SYNC;    
644        //     if ( debug ) printf(" 1 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",TimeSync,ObtSync,TimeSync-ObtSync);
645      //      //
 //     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);  
 //  
646      ULong_t TimeSync = (ULong_t)dbtime->GetTimesync();      ULong_t TimeSync = (ULong_t)dbtime->GetTimesync();
647      ULong_t ObtSync = (ULong_t)(dbtime->GetObt0()/1000);      ULong_t ObtSync = (ULong_t)(dbtime->GetObt0()/1000);
648      ULong_t DeltaOBT = TimeSync - ObtSync;      ULong_t DeltaOBT = TimeSync - ObtSync;
649    
650      if ( debug ) printf(" 2 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",(ULong_t)(dbtime->GetTimesync()/1000),(ULong_t)dbtime->GetObt0(),TimeSync-ObtSync);      if ( debug ) printf(" 2 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",(ULong_t)(dbtime->GetTimesync()/1000),(ULong_t)dbtime->GetObt0(),TimeSync-ObtSync);
651            //
652      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
653      neventsm = l0trm->GetEntries();      //
654        ch = new TChain("Mcmd","Mcmd");
655        //
656        // look in the DB to find the closest files to this run
657        //
658        TSQLResult *pResult = 0;
659        TSQLRow *Row = 0;
660        stringstream myquery;
661        UInt_t l0fid[10];
662        Int_t i = 0;
663        memset(l0fid,0,10*sizeof(Int_t));
664        //
665        myquery.str("");
666        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;";
667        //
668        pResult = dbc->Query(myquery.str().c_str());
669        //
670        i = 9;
671        if( pResult ){
672          //
673          Row = pResult->Next();
674          //
675          while ( Row ){
676            //
677            // store infos and exit
678            //
679            l0fid[i] = (UInt_t)atoll(Row->GetField(0));
680            i--;
681            Row = pResult->Next();  
682            //
683          };
684          pResult->Delete();
685        };
686        //
687        myquery.str("");
688        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;";
689        //
690        pResult = dbc->Query(myquery.str().c_str());
691        //
692        i = 0;
693        if( pResult ){
694          //
695          Row = pResult->Next();
696          //
697          while ( Row ){
698            //
699            // store infos and exit
700            //
701            l0fid[i] = (UInt_t)atoll(Row->GetField(0));
702            i++;
703            Row = pResult->Next();  
704            //
705          };
706          pResult->Delete();
707        };
708        //
709        i = 0;
710        UInt_t previd = 0;
711        while ( i < 10 ){
712          if ( l0fid[i] && previd != l0fid[i] ){
713            previd = l0fid[i];
714            myquery.str("");
715            myquery << "select PATH,NAME from GL_ROOT where ID=" << l0fid[i] << " ;";
716            //
717            pResult = dbc->Query(myquery.str().c_str());
718            //
719            if( pResult ){
720              //
721              Row = pResult->Next();
722              //
723              if ( debug ) printf(" Using inclination informations from file: %s \n",(((TString)gSystem->ExpandPathName(Row->GetField(0)))+"/"+(TString)Row->GetField(1)).Data());
724              ch->Add(((TString)gSystem->ExpandPathName(Row->GetField(0)))+"/"+(TString)Row->GetField(1));
725              //
726              pResult->Delete();
727            };
728          };
729          i++;
730        };
731        //
732        //    l0trm = (TTree*)l0File->Get("Mcmd");
733        //    ch->ls();
734        ch->SetBranchAddress("Mcmd",&mcmdev);
735        //    printf(" entries %llu \n", ch->GetEntries());
736        //    l0trm = ch->GetTree();
737        //    neventsm = l0trm->GetEntries();
738        neventsm = ch->GetEntries();
739        if ( debug ) printf(" entries %u \n", neventsm);
740      //    neventsm = 0;      //    neventsm = 0;
741      //      //
742      if (neventsm == 0){      if (neventsm == 0){
# Line 582  int OrbitalInfoCore(UInt_t run, TFile *f Line 747  int OrbitalInfoCore(UInt_t run, TFile *f
747      }      }
748      //      //
749            
750      l0trm->SetBranchAddress("Mcmd", &mcmdev);      //    l0trm->SetBranchAddress("Mcmd", &mcmdev);
751      //    l0trm->SetBranchAddress("Header", &eh);      //    l0trm->SetBranchAddress("Header", &eh);
752      //      //
753      //      //
754      //      //
755      UInt_t mctren = 0;      
756      UInt_t mcreen = 0;    //    UInt_t mctren = 0;    
757      UInt_t numrec = 0;  //    UInt_t mcreen = 0;        
758    //    UInt_t numrec = 0;
759      //      //
760      Double_t upperqtime = 0;      //    Double_t upperqtime = 0;
761      Double_t lowerqtime = 0;      Double_t lowerqtime = 0;
762            
763      Double_t incli = 0;      //    Double_t incli = 0;
764      oi = 0;      //    oi = 0;
765      UInt_t ooi = 0;      //    UInt_t ooi = 0;
766      //      //
767      // init quaternions sync      // init quaternions information from mcmd-packets
768      //      //
769      Bool_t isf = true;      Bool_t isf = true;
770      Int_t fgh = 0;      //    Int_t fgh = 0;
771    
772        vector<Float_t> q0;
773        vector<Float_t> q1;
774        vector<Float_t> q2;
775        vector<Float_t> q3;
776        vector<Double_t> qtime;
777        vector<Float_t> qPitch;
778        vector<Float_t> qRoll;
779        vector<Float_t> qYaw;
780        vector<Int_t> qmode;
781    
782        Int_t nt = 0;
783        
784        //init sine-function interpolation
785        
786        //cout<<"Sine coeficient initialisation..."<<endl;
787        vector<Sine> q0sine;
788        vector<Sine> q1sine;
789        vector<Sine> q2sine;
790        vector<Sine> q3sine;
791        vector<Sine> Yawsine;
792    
793        /*TH2F* q0testing = new TH2F();
794          TH2F* q1testing = new TH2F();
795          TH2F* q2testing = new TH2F();
796          TH2F* q3testing = new TH2F();
797          TH2F* Pitchtesting = new TH2F();
798        */
799        UInt_t must = 0;
800    
801      //      //
802      // run over all the events of the run      // run over all the events of the run
803      //      //
804      if (verbose) printf("\n Ready to start! \n\n Processed events: \n\n");      if (verbose) printf("\n Ready to start! \n\n Processed events: \n\n");
805      //      //
806       //      //
807      for ( re = runinfo->EV_FROM; re < (runinfo->EV_FROM+runinfo->NEVENTS); re++){      for ( re = runinfo->EV_FROM; re < (runinfo->EV_FROM+runinfo->NEVENTS); re++){
       
808        //        //
809        if ( procev%1000 == 0 && procev > 0 && verbose ) printf(" %iK \n",procev/1000);          if ( procev%1000 == 0 && procev > 0 && verbose ) printf(" %iK \n",procev/1000);  
810        if ( debug ) printf(" %i \n",procev);              if ( debug ) printf(" %i \n",procev);      
811        //        //
812        l0head->GetEntry(re);        if ( l0head->GetEntry(re) <= 0 ) throw -36;
813        //        //
814        // absolute time of this event        // absolute time of this event
815        //        //
816        ph = eh->GetPscuHeader();        ph = eh->GetPscuHeader();
817        atime = dbtime->DBabsTime(ph->GetOrbitalTime());        atime = dbtime->DBabsTime(ph->GetOrbitalTime());
818          if ( debug ) printf(" %i absolute time \n",procev);      
819        //        //
820        // paranoid check        // paranoid check
821        //        //
822        if ( (atime > runinfo->RUNTRAILER_TIME) || (atime < runinfo->RUNHEADER_TIME)  ) {        if ( (atime > (runinfo->RUNTRAILER_TIME+1)) || (atime < (runinfo->RUNHEADER_TIME-1))  ) {
823          if (verbose) printf(" OrbitalInfo - WARNING: event at time outside the run time window, skipping it\n");          if (verbose) printf(" OrbitalInfo - WARNING: event at time outside the run time window, skipping it\n");
824          jumped++;          jumped++;
825  //      debug = true;          //      debug = true;
826          continue;          continue;
827        }        }
828    
# Line 651  int OrbitalInfoCore(UInt_t run, TFile *f Line 847  int OrbitalInfoCore(UInt_t run, TFile *f
847          //          //
848          tof->Clear();          tof->Clear();
849          //          //
850          ttof->GetEntry(itr);          if ( ttof->GetEntry(itr) <= 0 ) throw -36;
851          //          //
852        };        };
853        //        //
# Line 659  int OrbitalInfoCore(UInt_t run, TFile *f Line 855  int OrbitalInfoCore(UInt_t run, TFile *f
855        //        //
856        // start processing        // start processing
857        //        //
858          if ( debug ) printf(" %i start processing \n",procev);      
859        orbitalinfo->Clear();        orbitalinfo->Clear();
860        //        //
861        OrbitalInfoTrkVar *t_orb = new OrbitalInfoTrkVar();        OrbitalInfoTrkVar *t_orb = new OrbitalInfoTrkVar();
# Line 670  int OrbitalInfoCore(UInt_t run, TFile *f Line 867  int OrbitalInfoCore(UInt_t run, TFile *f
867        orbitalinfo->pkt_num = ph->GetCounter();        orbitalinfo->pkt_num = ph->GetCounter();
868        orbitalinfo->OBT = ph->GetOrbitalTime();        orbitalinfo->OBT = ph->GetOrbitalTime();
869        orbitalinfo->absTime = atime;        orbitalinfo->absTime = atime;
870          if ( debug ) printf(" %i pktnum obt abstime \n",procev);      
871        //        //
872        // Propagate the orbit from the tle time to atime, using SGP(D)4.        // Propagate the orbit from the tle time to atime, using SGP(D)4.
873        //        //
874          if ( debug ) printf(" %i sgp4 \n",procev);      
875        cCoordGeo coo;        cCoordGeo coo;
876        float jyear=0;            Float_t jyear=0.;    
877        //        //
878        if(atime >= gltle->GetToTime()) {        if(atime >= gltle->GetToTime()) {
879          if ( !gltle->Query(atime, dbc) ){          if ( !gltle->Query(atime, dbc) ){
880            //                  //      
881            // Compute the magnetic dipole moment.            // Compute the magnetic dipole moment.
882            //            //
883              if ( debug ) printf(" %i compute magnetic dipole moment \n",procev);      
884            UInt_t year, month, day, hour, min, sec;            UInt_t year, month, day, hour, min, sec;
885            //            //
886            TTimeStamp t = TTimeStamp(atime, kTRUE);            TTimeStamp t = TTimeStamp(atime, kTRUE);
# Line 688  int OrbitalInfoCore(UInt_t run, TFile *f Line 888  int OrbitalInfoCore(UInt_t run, TFile *f
888            t.GetTime(kTRUE, 0, &hour, &min, &sec);            t.GetTime(kTRUE, 0, &hour, &min, &sec);
889            jyear = (float) year            jyear = (float) year
890              + (month*31.+ (float) day)/365.              + (month*31.+ (float) day)/365.
891              + (hour*3600.+min*60.+(float)sec)/(24*3600*365.);              + (hour*3600.+min*60.+(float)sec)/(24.*3600.*365.);
892            //            //
893              if ( debug ) printf(" %i compute magnetic dipole moment get dipole moment for year\n",procev);      
894              if ( debug ) printf(" %i jyear %f dimo %f \n",procev,jyear,dimo);      
895            feldcof_(&jyear, &dimo); // get dipole moment for year            feldcof_(&jyear, &dimo); // get dipole moment for year
896              if ( debug ) printf(" %i compute magnetic dipole moment end\n",procev);      
897          } else {          } else {
898            code = -56;            code = -56;
899            goto closeandexit;            goto closeandexit;
# Line 705  int OrbitalInfoCore(UInt_t run, TFile *f Line 908  int OrbitalInfoCore(UInt_t run, TFile *f
908        // synchronize with quaternions data        // synchronize with quaternions data
909        //        //
910        if ( isf && neventsm>0 ){        if ( isf && neventsm>0 ){
         if ( debug ) printf(" I am here \n");  
911          //          //
912          // First event          // First event
913          //          //
914          isf = false;          isf = false;
915          upperqtime = atime;          //      upperqtime = atime;
916          lowerqtime = runinfo->RUNHEADER_TIME;          lowerqtime = runinfo->RUNHEADER_TIME;
917          for ( ik = 0; ik < neventsm; ik++){          for ( ik = 0; ik < neventsm; ik++){  //number of macrocommad packets
918            l0trm->GetEntry(ik);            if ( ch->GetEntry(ik) <= 0 ) throw -36;
919            tmpSize = mcmdev->Records->GetEntries();            tmpSize = mcmdev->Records->GetEntries();
920            numrec = tmpSize;            //      numrec = tmpSize;
921            for (Int_t j3 = 0;j3<tmpSize;j3++){            for (Int_t j3 = 0;j3<tmpSize;j3++){  //number of subpackets
922              if ( debug ) printf(" eh eh eh \n");              if ( debug ) printf(" ik %i j3 %i eh eh eh \n",ik,j3);
923              mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(j3);              mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(j3);
924              if ((int)mcmdrc->ID1 == 226){              if ( mcmdrc ){ // missing inclination bug [8RED 090116]
925                L_QQ_Q_l_upper->fill(mcmdrc->McmdData);                if ( debug ) printf(" pluto \n");
926                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
927                  if (ui>0){                  L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
928                    if (L_QQ_Q_l_upper->time[ui]>L_QQ_Q_l_upper->time[0]){                  for (UInt_t ui = 0; ui < 6; ui++){
929                      if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000))<atime){                    if (ui>0){
930                        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]){
931                        orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);                        if ( debug ) printf(" here1 %i \n",ui);
932                        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));
933                      }else {                        Int_t recSize = recqtime.size();
934                        lowerqtime = upperqtime;                        if(lowerqtime > recqtime[recSize-1]){
935                        upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));                          Int_t sizeqmcmd = qtime.size();
936                        orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);                          inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
937                        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;
938                        mcreen = j3;                          q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][0];
939                        mctren = ik;                          q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][1];
940                        if(fgh==0){                          q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][2];
941                          CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);                          q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][3];
942                          CopyAng(RYPang_lower,RYPang_upper);                          qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui);
943                            lowerqtime = u_time;
944                            orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi);
945                            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]);
946                            qRoll[sizeqmcmd]=RYPang_upper->Kren;
947                            qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
948                            qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
949                          }
950                          for(Int_t mu = nt;mu<recSize;mu++){
951                            if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){
952                              nt=mu;
953                              Int_t sizeqmcmd = qtime.size();
954                              inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
955                              qtime[sizeqmcmd]=recqtime[mu];
956                              q0[sizeqmcmd]=recq0[mu];
957                              q1[sizeqmcmd]=recq1[mu];
958                              q2[sizeqmcmd]=recq2[mu];
959                              q3[sizeqmcmd]=recq3[mu];
960                              qmode[sizeqmcmd]=-10;
961                              orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi);
962                              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]);
963                              qRoll[sizeqmcmd]=RYPang_upper->Kren;
964                              qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
965                              qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
966                            }
967                            if(recqtime[mu]>=u_time){
968                              Int_t sizeqmcmd = qtime.size();
969                              inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
970                              qtime[sizeqmcmd]=u_time;
971                              q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][0];
972                              q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][1];
973                              q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][2];
974                              q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][3];
975                              qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui);
976                              lowerqtime = u_time;
977                              orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi);
978                              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]);
979                              qRoll[sizeqmcmd]=RYPang_upper->Kren;
980                              qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
981                              qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
982                              break;
983                            }
984                        }                        }
                       oi=ui;  
                       goto closethisloop;  
985                      }                      }
986                      fgh++;                    }else{
987                      CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);                      if ( debug ) printf(" here2 %i \n",ui);
988                      CopyAng(RYPang_lower,RYPang_upper);                      Double_t u_time = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
989                    }                      if(lowerqtime>u_time)nt=0;
990                  }else{                      Int_t recSize = recqtime.size();
991                    if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))<atime){                      if(lowerqtime > recqtime[recSize-1]){
992                      upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));                        Int_t sizeqmcmd = qtime.size();
993                      orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);                        inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
994                      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;
995                    }                        q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][0];
996                    else {                        q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][1];
997                      lowerqtime = upperqtime;                        q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][2];
998                      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];
999                      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);
1000                      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;
1001                      mcreen = j3;                        orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi);
1002                      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]);
1003                      if(fgh==0){                        qRoll[sizeqmcmd]=RYPang_upper->Kren;
1004                        CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);                        qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
1005                        CopyAng(RYPang_lower,RYPang_upper);                        qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
1006                        lowerqtime = atime-1;                      }
1007                        for(Int_t mu = nt;mu<recSize;mu++){
1008                          if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){
1009                            nt=mu;
1010                            Int_t sizeqmcmd = qtime.size();
1011                            inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
1012                            qtime[sizeqmcmd]=recqtime[mu];
1013                            q0[sizeqmcmd]=recq0[mu];
1014                            q1[sizeqmcmd]=recq1[mu];
1015                            q2[sizeqmcmd]=recq2[mu];
1016                            q3[sizeqmcmd]=recq3[mu];
1017                            qmode[sizeqmcmd]=-10;
1018                            orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi);
1019                            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]);
1020                            qRoll[sizeqmcmd]=RYPang_upper->Kren;
1021                            qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
1022                            qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
1023                          }
1024                          if(recqtime[mu]>=u_time){
1025                            Int_t sizeqmcmd = qtime.size();
1026                            inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
1027                            qtime[sizeqmcmd]=u_time;
1028                            q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][0];
1029                            q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][1];
1030                            q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][2];
1031                            q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][3];
1032                            qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui);
1033                            lowerqtime = u_time;
1034                            orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi);
1035                            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]);
1036                            qRoll[sizeqmcmd]=RYPang_upper->Kren;
1037                            qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
1038                            qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
1039                            CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
1040                            break;
1041                          }
1042                      }                      }
                     oi=ui;  
                     goto closethisloop;  
                     //_0 = true;  
1043                    }                    }
1044                    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]);  
1045                }                }
               //              re--;  
               gh=true;  
             }  
           }else{  
             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)));  
               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));  
               //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";  
               //cin>>grib;  
               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)));  
               orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));  
1046              }              }
1047                if ( debug ) printf(" ciccio \n");
1048            }            }
1049          } 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));  
1050                    
1051              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(qtime.size()==0){
1052              orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));            for(UInt_t my=0;my<recqtime.size();my++){
1053              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)));              Int_t sizeqmcmd = qtime.size();
1054              orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));              inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw);
1055              //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";              qtime[sizeqmcmd]=recqtime[my];
1056              //cin>>grib;              q0[sizeqmcmd]=recq0[my];
1057              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)));              q1[sizeqmcmd]=recq1[my];
1058              orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));              q2[sizeqmcmd]=recq2[my];
1059            }              q3[sizeqmcmd]=recq3[my];
1060            if (tut==6){              qmode[sizeqmcmd]=-10;
1061              if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){              orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi);
1062                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)));              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]);
1063                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));              qRoll[sizeqmcmd]=RYPang_upper->Kren;
1064                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)));              qYaw[sizeqmcmd]=RYPang_upper->Ryskanie;
1065                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));              qPitch[sizeqmcmd]=RYPang_upper->Tangazh;
1066                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)));            }
1067                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));  
1068                    
1069                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");
1070                orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));  
1071                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");
1072                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.;
1073                //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.;
1074                //cin>>grib;          for(UInt_t tre = 0;tre<qtime.size();tre++){
1075                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];
1076                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];
             }  
           }              
1077          }          }
1078          //          if ( debug ) printf(" gnfuffi \n");
1079          orbitalinfo->mode = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi);  
1080          //        } // if we processed first event
1081        } else {  
1082          if ( debug ) printf(" ops no incl! \n");        
1083          orbitalinfo->mode = 10;        //Filling Inclination information
1084        };        Double_t incli = 0;
1085          if ( qtime.size() > 1 ){
1086            for(UInt_t mu = must;mu<qtime.size()-1;mu++){
1087              if ( debug ) printf(" ??grfuffi %i sixe %i must %i \n",mu,qtime.size()-1,must);
1088              if(qtime[mu+1]>qtime[mu]){
1089                if ( debug ) printf(" grfuffi2 %i \n",mu);
1090                if(atime<=qtime[mu+1] && atime>=qtime[mu]){
1091                  must = mu;
1092                  if ( debug ) printf(" grfuffi3 %i \n",mu);
1093                  incli = (qPitch[mu+1]-qPitch[mu])/(qtime[mu+1]-qtime[mu]);
1094                  orbitalinfo->theta =  incli*atime+qPitch[mu+1]-incli*qtime[mu+1];
1095                  incli = (qRoll[mu+1]-qRoll[mu])/(qtime[mu+1]-qtime[mu]);
1096                  orbitalinfo->etha =  incli*atime+qRoll[mu+1]-incli*qtime[mu+1];
1097                  incli = (qYaw[mu+1]-qYaw[mu])/(qtime[mu+1]-qtime[mu]);
1098                  orbitalinfo->phi =  incli*atime+qYaw[mu+1]-incli*qtime[mu+1];
1099                  
1100                  incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
1101                  orbitalinfo->q0 =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
1102                  incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
1103                  orbitalinfo->q1 =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
1104                  incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
1105                  orbitalinfo->q2 =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
1106                  incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
1107                  orbitalinfo->q3 =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
1108                  
1109                  orbitalinfo->TimeGap = qtime[mu+1]-qtime[mu];
1110                  orbitalinfo->mode = qmode[mu+1];
1111                  //if(qmode[mu+1]==-10) orbitalinfo->R10r = true;else orbitalinfo->R10r = false;
1112                  //reserved for next versions Vitaly.
1113                  /*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){
1114                  //linear interpolation
1115                  incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
1116                  orbitalinfo->q0 =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
1117                  incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
1118                  orbitalinfo->q1 =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
1119                  incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
1120                  orbitalinfo->q2 =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
1121                  incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
1122                  orbitalinfo->q3 =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
1123                  }else{
1124                  //sine interpolation
1125                  for(UInt_t mt=0;mt<q0sine.size();mt++){
1126                  if(atime<=q0sine[mt].finishPoint && atime>=q0sine[mt].startPoint){
1127                  if(!q0sine[mt].NeedFit)orbitalinfo->q0=q0sine[mt].A*sin(q0sine[mt].b*atime+q0sine[mt].c);else{
1128                  incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]);
1129                  orbitalinfo->q0 =  incli*atime+q0[mu+1]-incli*qtime[mu+1];
1130                  }
1131                  }
1132                  if(atime<=q1sine[mt].finishPoint && atime>=q1sine[mt].startPoint){
1133                  if(!q1sine[mt].NeedFit)orbitalinfo->q1=q1sine[mt].A*sin(q1sine[mt].b*atime+q1sine[mt].c);else{
1134                  incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]);
1135                  orbitalinfo->q1 =  incli*atime+q1[mu+1]-incli*qtime[mu+1];
1136                  }
1137                  }
1138                  if(atime<=q2sine[mt].finishPoint && atime>=q2sine[mt].startPoint){
1139                  if(!q2sine[mt].NeedFit)orbitalinfo->q2=q0sine[mt].A*sin(q2sine[mt].b*atime+q2sine[mt].c);else{
1140                  incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]);
1141                  orbitalinfo->q2 =  incli*atime+q2[mu+1]-incli*qtime[mu+1];
1142                  }
1143                  }
1144                  if(atime<=q3sine[mt].finishPoint && atime>=q3sine[mt].startPoint){
1145                  if(!q3sine[mt].NeedFit)orbitalinfo->q3=q0sine[mt].A*sin(q3sine[mt].b*atime+q3sine[mt].c);else{
1146                  incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]);
1147                  orbitalinfo->q3 =  incli*atime+q3[mu+1]-incli*qtime[mu+1];
1148                  }
1149                  }
1150                  if(atime<=Yawsine[mt].finishPoint && atime>=Yawsine[mt].startPoint){
1151                  if(!Yawsine[mt].NeedFit)orbitalinfo->phi=Yawsine[mt].A*sin(Yawsine[mt].b*atime+Yawsine[mt].c);else{
1152                  incli = (qYaw[mu+1]-qYaw[mu])/(qtime[mu+1]-qtime[mu]);
1153                  orbitalinfo->phi =  incli*atime+qYaw[mu+1]-incli*qtime[mu+1];
1154                  }
1155                  }
1156                  }
1157                  }*/
1158                  //q0testing->Fill(atime,orbitalinfo->q0,100);
1159                  //q1testing->Fill(atime,orbitalinfo->q1,100);
1160                  //Pitchtesting->Fill(atime,orbitalinfo->etha);
1161                  //q2testing->Fill(atime,orbitalinfo->q2);
1162                  //q3testing->Fill(atime,orbitalinfo->q3);
1163                  if ( debug ) printf(" grfuffi4 %i \n",mu);
1164                  break;
1165                }
1166              }
1167            }
1168          }
1169          if ( debug ) printf(" grfuffi5  \n");
1170        //        //
1171        // ops no inclination information        // ops no inclination information
1172        //        //
1173          
1174        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 ( 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 ){
1175          orbitalinfo->mode = 10;          orbitalinfo->mode = 10;
1176          orbitalinfo->q0 = -1000.;          orbitalinfo->q0 = -1000.;
# Line 949  int OrbitalInfoCore(UInt_t run, TFile *f Line 1180  int OrbitalInfoCore(UInt_t run, TFile *f
1180          orbitalinfo->etha = -1000.;          orbitalinfo->etha = -1000.;
1181          orbitalinfo->phi = -1000.;          orbitalinfo->phi = -1000.;
1182          orbitalinfo->theta = -1000.;          orbitalinfo->theta = -1000.;
1183        };          if ( debug ) printf(" grfuffi6 \n");
1184          }
1185        //        //
1186          if ( debug ) printf(" filling \n");
1187        // #########################################################################################################################          // #########################################################################################################################  
1188        //        //
1189        // fill orbital positions        // fill orbital positions
# Line 961  int OrbitalInfoCore(UInt_t run, TFile *f Line 1194  int OrbitalInfoCore(UInt_t run, TFile *f
1194        lon = (coo.m_Lon > M_PI) ? rad2deg(coo.m_Lon - 2*M_PI) : rad2deg(coo.m_Lon);        lon = (coo.m_Lon > M_PI) ? rad2deg(coo.m_Lon - 2*M_PI) : rad2deg(coo.m_Lon);
1195        lat = rad2deg(coo.m_Lat);        lat = rad2deg(coo.m_Lat);
1196        alt = coo.m_Alt;        alt = coo.m_Alt;
1197          if ( debug ) printf(" coord done \n");
1198        //        //
1199        if( lon<180 && lon>-180 && lat<90 && lat>-90 && alt>0 ){          if( lon<180 && lon>-180 && lat<90 && lat>-90 && alt>0 ){  
1200          //                //      
# Line 970  int OrbitalInfoCore(UInt_t run, TFile *f Line 1204  int OrbitalInfoCore(UInt_t run, TFile *f
1204          //          //
1205          // compute mag field components and L shell.          // compute mag field components and L shell.
1206          //          //
1207            if ( debug ) printf(" call igrf feldg \n");
1208          feldg_(&lat, &lon, &alt, &bnorth, &beast, &bdown, &babs);          feldg_(&lat, &lon, &alt, &bnorth, &beast, &bdown, &babs);
1209            if ( debug ) printf(" call igrf shellg \n");
1210          shellg_(&lat, &lon, &alt, &dimo, &xl, &icode, &bab1);          shellg_(&lat, &lon, &alt, &dimo, &xl, &icode, &bab1);
1211            if ( debug ) printf(" call igrf findb \n");
1212          findb0_(&stps, &bdel, &value, &bequ, &rr0);          findb0_(&stps, &bdel, &value, &bequ, &rr0);
1213          //          //
1214            if ( debug ) printf(" done igrf \n");
1215          orbitalinfo->Bnorth = bnorth;          orbitalinfo->Bnorth = bnorth;
1216          orbitalinfo->Beast = beast;          orbitalinfo->Beast = beast;
1217          orbitalinfo->Bdown = bdown;          orbitalinfo->Bdown = bdown;
1218          orbitalinfo->Babs = babs;          orbitalinfo->Babs = babs;
1219            orbitalinfo->M = dimo;
1220          orbitalinfo->BB0 = babs/bequ;          orbitalinfo->BB0 = babs/bequ;
1221          orbitalinfo->L = xl;                orbitalinfo->L = xl;      
1222          // Set Stormer vertical cutoff using L shell.          // Set Stormer vertical cutoff using L shell.
1223          orbitalinfo->cutoff[0] = 14.9/(xl*xl);          orbitalinfo->cutoffsvl = 14.295 / (xl*xl); //
1224            /*
1225              ---------- Forwarded message ----------
1226              Date: Wed, 09 May 2012 12:16:47 +0200
1227              From: Alessandro Bruno <alessandro.bruno@ba.infn.it>
1228              To: Mirko Boezio <mirko.boezio@ts.infn.it>
1229              Cc: Francesco S. Cafagna <Francesco.Cafagna@ba.infn.it>
1230              Subject: Störmer vertical cutoff
1231    
1232              Ciao Mirko,
1233              volevo segnalarti che il valore dello Störmer vertical cutoff nel Level2 è
1234              sovrastimato di circa il 4%.
1235              Dopo un'approfondita analisi con l'IGRF-05 abbiamo ricavano un valore pari
1236              a: 14.295 / L^2 anzichè 14.9 / L^2, valore obsoleto in quanto riferito agli
1237              anni '50.
1238            */
1239            //14.9/(xl*xl);
1240            orbitalinfo->igrf_icode = icode;
1241          //          //
1242        };              }      
1243          //
1244          if ( debug ) printf(" pitch angle \n");
1245        //        //
1246        // pitch angles        // pitch angles
1247        //        //
1248        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 ){
1249          if( orbitalinfo->TimeGap>0 && orbitalinfo->TimeGap<2000000){
1250          //          //
1251          Float_t Bx = -orbitalinfo->Bdown;                       //don't need for PamExp ExpOnly for all geography areas          if ( debug ) printf(" timegap %f \n",orbitalinfo->TimeGap);
1252          Float_t By = orbitalinfo->Beast;                        //don't need for PamExp ExpOnly for all geography areas          Float_t Bx = -orbitalinfo->Bdown;
1253          Float_t Bz = orbitalinfo->Bnorth;                       //don't need for PamExp ExpOnly for all geography areas          Float_t By = orbitalinfo->Beast;
1254            Float_t Bz = orbitalinfo->Bnorth;
1255          //          //
1256          TMatrixD Fij = PO->ECItoGreenwich(PO->QuatoECI(orbitalinfo->q0,orbitalinfo->q1,orbitalinfo->q2,orbitalinfo->q3),orbitalinfo->absTime);          TMatrixD Fij = PO->ECItoGreenwich(PO->QuatoECI(orbitalinfo->q0,orbitalinfo->q1,orbitalinfo->q2,orbitalinfo->q3),orbitalinfo->absTime);
1257            TMatrixD Gij = PO->ColPermutation(Fij);
1258          TMatrixD Dij = PO->GreenwichtoGEO(orbitalinfo->lat,orbitalinfo->lon,Fij);          TMatrixD Dij = PO->GreenwichtoGEO(orbitalinfo->lat,orbitalinfo->lon,Fij);
1259          TMatrixD Iij = PO->ColPermutation(Dij);          TMatrixD Iij = PO->ColPermutation(Dij);
1260          //          //
1261          A1 = Iij(0,2);          orbitalinfo->Iij.ResizeTo(Iij);
1262          A2 = Iij(1,2);          orbitalinfo->Iij = Iij;
1263          A3 = Iij(2,2);          //
1264          //                //      A1 = Iij(0,2);
1265          orbitalinfo->pamzenitangle = (Float_t)PO->GetPitchAngle(1,0,0,A1,A2,A3);                        // Angle between zenit and Pamela's main axiz          //      A2 = Iij(1,2);
1266          orbitalinfo->pamBangle = (Float_t)PO->GetPitchAngle(A1,A2,A3,Bx,By,Bz);                 // Angle between Pamela's main axiz and B          //      A3 = Iij(2,2);
1267          //          //
1268            //      orbitalinfo->pamzenitangle = (Float_t)PO->GetPitchAngle(1,0,0,A1,A2,A3);                        // Angle between zenit and Pamela's main axiz
1269            //      orbitalinfo->pamBangle = (Float_t)PO->GetPitchAngle(A1,A2,A3,Bx,By,Bz);                 // Angle between Pamela's main axiz and B
1270            //
1271            if ( debug ) printf(" matrixes done  \n");
1272          if ( !standalone && tof->ntrk() > 0 ){          if ( !standalone && tof->ntrk() > 0 ){
1273              if ( debug ) printf(" !standalone \n");
1274            //            //
1275            Int_t nn = 0;            Int_t nn = 0;
1276            for(Int_t nt=0; nt < tof->ntrk(); nt++){              for(Int_t nt=0; nt < tof->ntrk(); nt++){  
# Line 1016  int OrbitalInfoCore(UInt_t run, TFile *f Line 1282  int OrbitalInfoCore(UInt_t run, TFile *f
1282              Double_t E22x = ptt->xtr_tof[3];//tr->x[3];              Double_t E22x = ptt->xtr_tof[3];//tr->x[3];
1283              Double_t E22y = ptt->ytr_tof[3];//tr->y[3];              Double_t E22y = ptt->ytr_tof[3];//tr->y[3];
1284              Double_t E22z = zin[3];              Double_t E22z = zin[3];
1285              if ( E11x < 100. && E11y < 100. && E22x < 100. && E22y < 100.  ){              if ( (E11x < 100. && E11y < 100. && E22x < 100. && E22y < 100.) || ptt->trkseqno != -1  ){
1286                Double_t norm = sqrt(pow(E22x-E11x,2)+pow(E22y-E11y,2)+pow(E22z-E11z,2));                Double_t norm = sqrt(pow(E22x-E11x,2)+pow(E22y-E11y,2)+pow(E22z-E11z,2));
1287                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));
1288                if(E22x-E11x>=0 && E22y-E11y <0) MyAzim =  360. - MyAzim;                //              if(E22x-E11x>=0 && E22y-E11y <0) MyAzim =  360. - MyAzim;
1289                if(E22x-E11x>=0 && E22y-E11y >=0) MyAzim = MyAzim;                //              if(E22x-E11x>=0 && E22y-E11y >=0) MyAzim = MyAzim;
1290                if(E22x-E11x<0 && E22y-E11y >0) MyAzim = 180. - MyAzim;                //              if(E22x-E11x<0 && E22y-E11y >0) MyAzim = 180. - MyAzim;
1291                if(E22x-E11x<0 && E22y-E11y <0) MyAzim = 180. + MyAzim;                //              if(E22x-E11x<0 && E22y-E11y <0) MyAzim = 180. + MyAzim;
1292                Px = (E22x-E11x)/norm;                Px = (E22x-E11x)/norm;
1293                Py = (E22y-E11y)/norm;                Py = (E22y-E11y)/norm;
1294                Pz = (E22z-E11z)/norm;                Pz = (E22z-E11z)/norm;
1295                //                //
               TMatrixD Eij = PO->PamelatoGEO(Iij,Px,Py,Pz);              
               //              
1296                t_orb->trkseqno = ptt->trkseqno;                t_orb->trkseqno = ptt->trkseqno;
1297                  //
1298                  TMatrixD Eij = PO->PamelatoGEO(Iij,Px,Py,Pz);
1299                  t_orb->Eij.ResizeTo(Eij);
1300                  t_orb->Eij = Eij;
1301                  //
1302                  TMatrixD Sij = PO->PamelatoGEO(Gij,Px,Py,Pz);
1303                  t_orb->Sij.ResizeTo(Sij);
1304                  t_orb->Sij = Sij;
1305                  //            
1306                t_orb->pitch = (Float_t)PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),Bx,By,Bz);                t_orb->pitch = (Float_t)PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),Bx,By,Bz);
1307                  //
1308                  //
1309                  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);
1310                  //
1311                  t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow((1+sqrt(1-pow(orbitalinfo->L,-3/2)*cos(omega))),2));
1312                  //
1313                  if ( t_orb->pitch != t_orb->pitch ) t_orb->pitch = -1000.;
1314                  if ( t_orb->cutoff != t_orb->cutoff ) t_orb->cutoff = -1000.;
1315                  //
1316                  if ( debug ) printf(" orbitalinfo->cutoffsvl %f vitaly %f \n",orbitalinfo->cutoffsvl,t_orb->cutoff);
1317                //                //
1318                new(tor[nn]) OrbitalInfoTrkVar(*t_orb);                new(tor[nn]) OrbitalInfoTrkVar(*t_orb);
1319                nn++;                nn++;
# Line 1041  int OrbitalInfoCore(UInt_t run, TFile *f Line 1324  int OrbitalInfoCore(UInt_t run, TFile *f
1324              //              //
1325            };            };
1326          } else {          } else {
1327            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);
1328          };          }
1329          //          //
1330          } else {
1331            if ( !standalone && tof->ntrk() > 0 ){
1332              //
1333              Int_t nn = 0;
1334              for(Int_t nt=0; nt < tof->ntrk(); nt++){  
1335                //
1336                ToFTrkVar *ptt = tof->GetToFTrkVar(nt);
1337                if ( ptt->trkseqno != -1  ){
1338                  //
1339                  t_orb->trkseqno = ptt->trkseqno;
1340                  //
1341                  t_orb->Eij = 0;  
1342                  //
1343                  t_orb->Sij = 0;
1344                  //            
1345                  t_orb->pitch = -1000.;
1346                  //
1347                  t_orb->cutoff = -1000.;
1348                  //
1349                  new(tor[nn]) OrbitalInfoTrkVar(*t_orb);
1350                  nn++;
1351                  //
1352                  t_orb->Clear();
1353                  //
1354                };
1355                //
1356              };    
1357            };
1358        };        };
1359        //        //
1360        // Fill the class        // Fill the class
# Line 1056  int OrbitalInfoCore(UInt_t run, TFile *f Line 1367  int OrbitalInfoCore(UInt_t run, TFile *f
1367      //      //
1368      // Here you may want to clear some variables before processing another run        // Here you may want to clear some variables before processing another run  
1369      //      //
1370    
1371        //gStyle->SetOptStat(000000);
1372        //gStyle->SetPalette(1);
1373        
1374        /*TCanvas* c1 = new TCanvas("c1","",1200,800);
1375        //c1->Divide(1,4);
1376        c1->cd(1);
1377        //q0testing->Draw("colz");
1378        //c1->cd(2);
1379        //q1testing->Draw("colz");
1380        //c1->cd(3);
1381        Pitchtesting->Draw("colz");
1382        //c1->cd(4);
1383        //q3testing->Draw("colz");
1384        c1->SaveAs("9.Rollhyst.png");
1385        delete c1;*/
1386    
1387        if ( verbose ) printf(" Clear before new run \n");
1388      delete dbtime;      delete dbtime;
1389      if ( L_QQ_Q_l_upper ) delete L_QQ_Q_l_upper;  
1390        if ( mcmdrc ) mcmdrc->Clear();
1391        mcmdrc = 0;
1392        
1393        if ( verbose ) printf(" Clear before new run1 \n");
1394      if ( L_QQ_Q_l_lower ) delete L_QQ_Q_l_lower;      if ( L_QQ_Q_l_lower ) delete L_QQ_Q_l_lower;
1395        if ( verbose ) printf(" Clear before new run2 \n");
1396        if ( L_QQ_Q_l_upper ) delete L_QQ_Q_l_upper;
1397        if ( verbose ) printf(" Clear before new run3 \n");
1398      if ( RYPang_upper ) delete RYPang_upper;      if ( RYPang_upper ) delete RYPang_upper;
1399        if ( verbose ) printf(" Clear before new run4 \n");
1400      if ( RYPang_lower ) delete RYPang_lower;      if ( RYPang_lower ) delete RYPang_lower;
1401    
1402        if ( l0tr ) l0tr->Delete();
1403        
1404        if ( verbose ) printf(" End run \n");
1405    
1406    }; // process all the runs    }; // process all the runs
1407        
1408    if (verbose) printf("\n Finished processing data \n");    if (verbose) printf("\n Finished processing data \n");
# Line 1080  int OrbitalInfoCore(UInt_t run, TFile *f Line 1422  int OrbitalInfoCore(UInt_t run, TFile *f
1422          //          //
1423          // Get entry from old tree          // Get entry from old tree
1424          //          //
1425          OrbitalInfotrclone->GetEntry(j);                    if ( OrbitalInfotrclone->GetEntry(j) <= 0 ) throw -36;    
1426          //          //
1427          // copy orbitalinfoclone to OrbitalInfo          // copy orbitalinfoclone to OrbitalInfo
1428          //          //
# Line 1094  int OrbitalInfoCore(UInt_t run, TFile *f Line 1436  int OrbitalInfoCore(UInt_t run, TFile *f
1436        };        };
1437        if (verbose) printf(" Finished successful copying!\n");        if (verbose) printf(" Finished successful copying!\n");
1438      };      };
1439        //if ( OrbitalInfotrclone )    OrbitalInfotrclone->Clear();        
1440        //if ( OrbitalInfotrclone )    OrbitalInfotrclone->Delete();        
1441    };    };
1442    //    //
1443    // Close files, delete old tree(s), write and close level2 file    // Close files, delete old tree(s), write and close level2 file
1444    //    //
1445    if ( l0File ) l0File->Close();    if ( l0File ) l0File->Close();
   if ( tempfile ) tempfile->Close();              
1446    if ( myfold ) gSystem->Unlink(tempname.str().c_str());    if ( myfold ) gSystem->Unlink(tempname.str().c_str());
1447    //    //
   if ( runinfo ) runinfo->Close();      
1448    if ( OrbitalInfotr ) OrbitalInfotr->SetName("OrbitalInfo");        if ( OrbitalInfotr ) OrbitalInfotr->SetName("OrbitalInfo");    
   if ( tof ) tof->Delete();  
   if ( ttof ) ttof->Delete();  
1449    //    //
1450    if ( file ){    if ( file ){
1451      file->cd();      file->cd();
1452      file->Write();      if ( OrbitalInfotr ) OrbitalInfotr->Write("OrbitalInfo", TObject::kOverwrite); // 10 RED bug fixed
1453    };    };
1454    //    //
1455      if (verbose) printf("\n Exiting...\n");
1456    
1457    if ( myfold ) gSystem->Unlink(OrbitalInfofolder.str().c_str());    if ( myfold ) gSystem->Unlink(OrbitalInfofolder.str().c_str());
1458    //    //
1459    // the end    // the end
# Line 1120  int OrbitalInfoCore(UInt_t run, TFile *f Line 1462  int OrbitalInfoCore(UInt_t run, TFile *f
1462      dbc->Close();      dbc->Close();
1463      delete dbc;      delete dbc;
1464    };    };
   if (verbose) printf("\n Exiting...\n");  
   if(OrbitalInfotr)OrbitalInfotr->Delete();  
1465    //    //
1466      if (verbose) printf("\n Exiting...\n");
1467      if ( tempfile ) tempfile->Close();            
1468      
1469    if ( PO ) delete PO;    if ( PO ) delete PO;
1470    if ( orbitalinfo ) delete orbitalinfo;    if ( gltle ) delete gltle;
1471    if ( orbitalinfoclone ) delete orbitalinfoclone;    if ( glparam ) delete glparam;
1472      if ( glparam2 ) delete glparam2;
1473      if ( glparam3 ) delete glparam3;
1474      if (verbose) printf("\n Exiting3...\n");
1475    if ( glroot ) delete glroot;    if ( glroot ) delete glroot;
1476      if (verbose) printf("\n Exiting4...\n");
1477      if ( runinfo ) runinfo->Close();    
1478    if ( runinfo ) delete runinfo;    if ( runinfo ) delete runinfo;
1479    
1480      if ( debug ){  
1481      cout << "1   0x" << OrbitalInfotr << endl;
1482      cout << "2   0x" << OrbitalInfotrclone << endl;
1483      cout << "3   0x" << l0tr << endl;
1484      cout << "4   0x" << tempOrbitalInfo << endl;
1485      cout << "5   0x" << ttof << endl;
1486      }
1487      //
1488      if ( debug )  file->ls();
1489    //    //
1490    if(code < 0)  throw code;    if(code < 0)  throw code;
1491    return(code);    return(code);
# Line 1172  void CopyAng(InclinationInfo *A1, Inclin Line 1530  void CopyAng(InclinationInfo *A1, Inclin
1530  UInt_t holeq(Double_t lower,Double_t upper,Quaternions *Qlower, Quaternions *Qupper, UInt_t f){  UInt_t holeq(Double_t lower,Double_t upper,Quaternions *Qlower, Quaternions *Qupper, UInt_t f){
1531        
1532    UInt_t hole = 10;    UInt_t hole = 10;
1533    bool R10l = false;     // Sign of R10 mode in lower quaternions array    Bool_t R10l = false;     // Sign of R10 mode in lower quaternions array
1534    bool R10u = false;     // Sign of R10 mode in upper quaternions array    Bool_t R10u = false;     // Sign of R10 mode in upper quaternions array
1535    bool insm = false;     // Sign that we inside quaternions array    Bool_t insm = false;     // Sign that we inside quaternions array
1536    bool mxtml = false;    // Sign of mixt mode in lower quaternions array    //  Bool_t mxtml = false;    // Sign of mixt mode in lower quaternions array
1537    bool mxtmu = false;    // Sign of mixt mode in upper quaternions array    //  Bool_t mxtmu = false;    // Sign of mixt mode in upper quaternions array
1538    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
1539    UInt_t NCQl = 6;       // Number of correct quaternions in lower array    UInt_t NCQl = 6;       // Number of correct quaternions in lower array
1540    UInt_t NCQu = 6;       // Number of correct quaternions in upper array    //  UInt_t NCQu = 6;       // Number of correct quaternions in upper array
1541    if (f>0){    if (f>0){
1542      insm = true;      insm = true;
1543      if(Qupper->time[f]-Qupper->time[f-1]==30) R10u = false;      if(Qupper->time[f]-Qupper->time[f-1]==30) R10u = false;
# Line 1191  UInt_t holeq(Double_t lower,Double_t upp Line 1549  UInt_t holeq(Double_t lower,Double_t upp
1549      if((Qlower->time[5]-Qlower->time[0]==150)&&(Qlower->time[1]-Qlower->time[0]==30)) R10l = false;      if((Qlower->time[5]-Qlower->time[0]==150)&&(Qlower->time[1]-Qlower->time[0]==30)) R10l = false;
1550      if((Qupper->time[5]-Qupper->time[0]==150)&&(Qupper->time[1]-Qupper->time[0]==30)) R10u = false;      if((Qupper->time[5]-Qupper->time[0]==150)&&(Qupper->time[1]-Qupper->time[0]==30)) R10u = false;
1551      if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]==30)){      if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]==30)){
1552        mxtml = true;        //      mxtml = true;
1553        for(UInt_t i = 1; i < 6; i++){        for(UInt_t i = 1; i < 6; i++){
1554          if(Qlower->time[i]-Qlower->time[0]==30*i) NCQl=i;          if(Qlower->time[i]-Qlower->time[0]==30*i) NCQl=i;
1555        }        }
1556      }      }
1557      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)){
1558        mxtmu = true;        //      mxtmu = true;
1559        for(UInt_t i = 1; i < 6; i++){        //      for(UInt_t i = 1; i < 6; i++){
1560          if(Qupper->time[i]-Qupper->time[0]==30*i) NCQu=i;        //        if(Qupper->time[i]-Qupper->time[0]==30*i) NCQu=i;
1561        }        //      }
1562      }      //    }
1563    }    }
1564        
1565    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;    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 1220  UInt_t holeq(Double_t lower,Double_t upp Line 1578  UInt_t holeq(Double_t lower,Double_t upp
1578    return hole;    return hole;
1579  }  }
1580    
1581    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){
1582      Int_t sizee = t.size()+1;
1583      t.resize(sizee);
1584      q0.resize(sizee);
1585      q1.resize(sizee);
1586      q2.resize(sizee);
1587      q3.resize(sizee);
1588      mode.resize(sizee);
1589      Roll.resize(sizee);
1590      Pitch.resize(sizee);
1591      Yaw.resize(sizee);
1592    }
1593    
1594    //Find fitting sine functions for q0,q1,q2,q3 and Yaw-angle;
1595    void sineparam(vector<Sine>& qsine, vector<Double_t>& qtime, vector<Float_t>& q, vector<Float_t>& Roll, vector<Float_t>& Pitch, Float_t limsin){
1596      UInt_t mulast = 0;
1597      UInt_t munow = 0;
1598      UInt_t munext = 0;
1599      Bool_t increase = false;
1600      Bool_t decrease = false;
1601      Bool_t Max_is_defined = false;
1602      Bool_t Start_point_is_defined = false;
1603      Bool_t Period_is_defined = false;
1604      Bool_t Large_gap = false;
1605      Bool_t normal_way = true;
1606      Bool_t small_gap_on_ridge = false;
1607      Double_t t1 = 0;
1608      Double_t t1A = 0;
1609      Int_t sinesize = 0;
1610      Int_t nfi = 0;
1611      for(UInt_t mu = 0;mu<qtime.size();mu++){
1612        //cout<<"Roll["<<mu<<"] = "<<Roll[mu]<<endl;
1613        if(TMath::Abs(Roll[mu])<1. && TMath::Abs(Pitch[mu])<1. && TMath::Abs(q[mu])<limsin){
1614        //cout<<"q["<<mu<<endl<<"] = "<<q[mu]<<endl;
1615        if(mulast!=0 && munow!=0 && munext!=0){mulast=munow;munow=munext;munext=mu;}
1616        if(munext==0 && munow!=0)munext=mu;
1617        if(munow==0 && mulast!=0)munow=mu;
1618        if(mulast==0)mulast=mu;
1619        
1620        //cout<<"mulast = "<<mulast<<"\tmunow = "<<munow<<"\tmunext = "<<munext<<endl;
1621        //Int_t ref;
1622        //cin>>ref;
1623        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;
1624        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;
1625        //if(normal_way)cout<<"Normal_Way"<<endl;
1626        if(Large_gap || small_gap_on_ridge){
1627          //cout<<"Large gap..."<<endl;
1628          //if(small_gap_on_ridge)cout<<"small gap..."<<endl;
1629          //cout<<"q["<<mulast<<"] = "<<q[mulast]<<"\tq["<<munow<<"] = "<<q[munow]<<"\tq["<<munext<<"] = "<<q[munext]<<endl;
1630          //cout<<"qtime["<<mulast<<"] = "<<qtime[mulast]<<"\tqtime["<<munow<<"] = "<<qtime[munow]<<"\tqtime["<<munext<<"] = "<<qtime[munext]<<endl;
1631          increase = false;
1632          decrease = false;
1633          if(nfi>0){
1634            qsine.resize(qsine.size()-1);
1635            sinesize = qsine.size();
1636            //cout<<"nfi was larger then zero"<<endl;
1637          }else{
1638            //cout<<"nfi was not larger then zero :( nfi = "<<nfi<<endl;
1639            //cout<<"qsine.size = "<<qsine.size()<<endl;
1640            if(!Period_is_defined){
1641              //cout<<"Period was defined"<<endl;
1642              if(qsine.size()>1){
1643                qsine[sinesize-1].b = qsine[sinesize-2].b;
1644                qsine[sinesize-1].c = qsine[sinesize-2].c;
1645              }else{
1646                qsine[sinesize-1].b = TMath::Pi()/1591.54;
1647                qsine[sinesize-1].c = qsine[sinesize-1].startPoint;
1648              }
1649            }
1650            if(!Max_is_defined){
1651              //cout<<"Max was already defined"<<endl;
1652              if(qsine.size()>1)qsine[sinesize-1].A = qsine[sinesize-2].A;else qsine[sinesize-1].A = limsin;
1653            }
1654            qsine[sinesize-1].NeedFit = true;
1655          }
1656          qsine[sinesize-1].finishPoint = qtime[munow];
1657          //cout<<"finish point before large gap = "<<qtime[munow]<<endl;
1658          nfi = 0;
1659          Max_is_defined = false;
1660          Start_point_is_defined = false;
1661          Period_is_defined = false;
1662          small_gap_on_ridge = false;
1663        }
1664        //cout<<"Slope "<<increase<<"\t"<<decrease<<endl;
1665        //cout<<"mulast = "<<mulast<<"\tmunow = "<<munow<<"\tmunext = "<<munext<<endl;
1666        if((munext>munow) && (munow>mulast) && normal_way){
1667          if(!increase && !decrease){
1668            //cout<<"Normal way have started"<<endl;
1669            qsine.resize(qsine.size()+1);
1670            sinesize = qsine.size();
1671            qsine[sinesize-1].startPoint=qtime[mulast];
1672            if(q[munext]>q[munow] && q[munow]>q[mulast]) increase = true;
1673            if(q[munext]<q[munow] && q[munow]<q[mulast]) decrease = true;
1674          }
1675          //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;}
1676          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){
1677            //cout<<"Max point is qtime = "<<qtime[munow]<<"\tq = "<<q[munow]<<endl;
1678            if(q[munow]>q[mulast]){
1679              increase = false;
1680              decrease = true;
1681            }
1682            if(q[munow]<q[mulast]){
1683              increase = true;
1684              decrease = false;
1685            }
1686            if(Max_is_defined && !Start_point_is_defined){
1687              Double_t qPer = qtime[munow]-t1A;
1688              if(qPer>1000){
1689                //cout<<"qsine["<<sinesize-1<<"] = "<<qPer<<" = "<<qtime[munow]<<" - "<<t1A<<"\tlim = "<<limsin<<endl;
1690                qsine[sinesize-1].b=TMath::Pi()/qPer;
1691                if(decrease)qsine[sinesize-1].c=-qsine[sinesize-1].b*t1A;
1692                if(increase)qsine[sinesize-1].c=-qsine[sinesize-1].b*(t1A-qPer);
1693                Period_is_defined = true;
1694              }
1695            }
1696            Max_is_defined = true;
1697            qsine[sinesize-1].A = TMath::Abs(q[munow]);
1698            if(Start_point_is_defined && Period_is_defined){
1699              qsine[sinesize-1].finishPoint = qtime[munow];
1700              nfi++;
1701              qsine[sinesize-1].NeedFit = false;
1702              Max_is_defined = false;
1703              Start_point_is_defined = false;
1704              Period_is_defined = false;
1705              qsine.resize(qsine.size()+1);
1706              sinesize = qsine.size();
1707              qsine[sinesize-1].startPoint = qtime[munow];
1708            }
1709            if(!Start_point_is_defined) t1A=qtime[munow];
1710          }
1711          //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;
1712          if(((q[munow]>=0 && q[mulast]<=0) || (q[munow]<=0 && q[mulast]>=0)) && qtime[munow]-qtime[mulast]<2000 && qtime[munext]-qtime[munow]<2000){
1713            Double_t tcrosszero = 0;
1714            //cout<<"cross zero point...qtime = "<<qtime[munow]<<endl;
1715            if(q[munow]==0.) tcrosszero = qtime[munow];else
1716              if(q[mulast]==0.)tcrosszero = qtime[mulast];else{
1717                Double_t k_ = (q[munow]-q[mulast])/(qtime[munow]-qtime[mulast]);
1718                Double_t b_ = q[munow]-k_*qtime[munow];
1719                tcrosszero = -b_/k_;
1720              }
1721            if(Start_point_is_defined){
1722              //cout<<"Start Point allready defined"<<endl;
1723              Double_t qPer = tcrosszero - t1;
1724              qsine[sinesize-1].b = TMath::Pi()/qPer;
1725              //cout<<"qsine["<<sinesize-1<<"].b = "<<TMath::Pi()/qPer<<endl;
1726              Period_is_defined = true;
1727              Float_t x0 = 0;
1728              if(decrease)x0 = t1;
1729              if(increase)x0 = tcrosszero;
1730              qsine[sinesize-1].c = -qsine[sinesize-1].b*x0;
1731              if(Max_is_defined){
1732                //cout<<"Max was previous defined"<<endl;
1733                qsine[sinesize-1].finishPoint = qtime[munow];
1734                nfi++;
1735                qsine[sinesize-1].NeedFit = false;
1736                Max_is_defined = false;
1737                t1 = tcrosszero;
1738                Start_point_is_defined = true;
1739                Period_is_defined = false;
1740                qsine.resize(qsine.size()+1);
1741                sinesize = qsine.size();
1742                qsine[sinesize-1].startPoint = qtime[munow];
1743              }
1744            }else{
1745              t1 = tcrosszero;
1746              Start_point_is_defined = true;
1747            }
1748          }
1749        }
1750        }
1751      }
1752    
1753      //cout<<"FINISH SINE INTERPOLATION FUNCTION..."<<endl<<endl;
1754    }
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