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

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revision 1.4 by mocchiut, Fri Aug 4 10:31:29 2006 UTC revision 1.24 by mocchiut, Fri Sep 7 21:14:18 2007 UTC
# Line 13  Line 13 
13  #include <TClassEdit.h>  #include <TClassEdit.h>
14  #include <TObject.h>  #include <TObject.h>
15  #include <TList.h>  #include <TList.h>
16  #include <TArrayL.h>  #include <TArrayI.h>
17  #include <TSystem.h>  #include <TSystem.h>
18  #include <TSystemDirectory.h>  #include <TSystemDirectory.h>
19  #include <TString.h>  #include <TString.h>
# Line 23  Line 23 
23  #include <TSQLRow.h>  #include <TSQLRow.h>
24  #include <TSQLResult.h>  #include <TSQLResult.h>
25  //  //
26    // RunInfo header
27    //
28    #include <RunInfo.h>
29    #include <GLTables.h>
30    //
31  // YODA headers  // YODA headers
32  //  //
33  #include <PamelaRun.h>  #include <PamelaRun.h>
 #include <RegistryEvent.h>  
34  #include <PscuHeader.h>  #include <PscuHeader.h>
35  #include <PscuEvent.h>  #include <PscuEvent.h>
36  #include <EventHeader.h>  #include <EventHeader.h>
37  #include <RegistryEvent.h>  #include <mcmd/McmdEvent.h>
38  //  #include <mcmd/McmdRecord.h>
 // RunInfo header  
 //  
 #include <RunInfo.h>  
 #include <GLTables.h>  
39  //  //
40  // This program headers  // This program headers
41  //  //
42  #include <OrbitalInfo.h>  #include <OrbitalInfo.h>
 #include <OrbitalInfoCore.h>  
43  #include <OrbitalInfoVerl2.h>  #include <OrbitalInfoVerl2.h>
44    #include <OrbitalInfoCore.h>
45    #include <InclinationInfo.h>
46    
47  using namespace std;  using namespace std;
48    
# Line 49  using namespace std; Line 50  using namespace std;
50  // CORE ROUTINE  // CORE ROUTINE
51  //  //
52  //  //
53    int OrbitalInfoCore(UInt_t run, TFile *file, TSQLServer *dbc, Int_t OrbitalInfoargc, char *OrbitalInfoargv[]){
54  int OrbitalInfoCore(ULong64_t run, TFile *file, TSQLServer *dbc, Int_t OrbitalInfoargc, char *OrbitalInfoargv[]){    //
55    Int_t i = 0;    Int_t i = 0;
56    //    //
57    TString processFolder = "OrbitalInfoFolder";    TString processFolder = Form("OrbitalInfoFolder_%u",run);
58    //    //
59    // Set these to true to have a very verbose output.    // Set these to true to have a very verbose output.
60    //    //
# Line 73  int OrbitalInfoCore(ULong64_t run, TFile Line 74  int OrbitalInfoCore(ULong64_t run, TFile
74        };        };
75        if ( (!strcmp(OrbitalInfoargv[i],"--debug")) || (!strcmp(OrbitalInfoargv[i],"-g")) ) {        if ( (!strcmp(OrbitalInfoargv[i],"--debug")) || (!strcmp(OrbitalInfoargv[i],"-g")) ) {
76          verbose = true;          verbose = true;
77            debug = true;
78        };        };
79        if ( (!strcmp(OrbitalInfoargv[i],"--verbose")) || (!strcmp(OrbitalInfoargv[i],"-v")) ) {        if ( (!strcmp(OrbitalInfoargv[i],"--verbose")) || (!strcmp(OrbitalInfoargv[i],"-v")) ) {
80          verbose = true;          verbose = true;
# Line 84  int OrbitalInfoCore(ULong64_t run, TFile Line 86  int OrbitalInfoCore(ULong64_t run, TFile
86    const char* outDir = gSystem->DirName(gSystem->DirName(file->GetPath()));    const char* outDir = gSystem->DirName(gSystem->DirName(file->GetPath()));
87    //    //
88    TTree *OrbitalInfotr = 0;    TTree *OrbitalInfotr = 0;
89    Long64_t nevents = 0LL;    UInt_t nevents = 0;
90      UInt_t neventsm = 0;
91    //    //
92    // variables needed to reprocess data    // variables needed to reprocess data
93    //    //
94      Long64_t maxsize = 10000000000LL;  
95      TTree::SetMaxTreeSize(maxsize);
96      //
97    TString OrbitalInfoversion;    TString OrbitalInfoversion;
98    ItoRunInfo *runinfo = 0;    ItoRunInfo *runinfo = 0;
99    TArrayL *runlist = 0;    TArrayI *runlist = 0;
100    TTree *OrbitalInfotrclone = 0;    TTree *OrbitalInfotrclone = 0;
101    Bool_t reproc = false;    Bool_t reproc = false;
102    Bool_t reprocall = false;    Bool_t reprocall = false;
# Line 99  int OrbitalInfoCore(ULong64_t run, TFile Line 105  int OrbitalInfoCore(ULong64_t run, TFile
105    UInt_t numbofrun = 0;    UInt_t numbofrun = 0;
106    stringstream ftmpname;    stringstream ftmpname;
107    TString fname;    TString fname;
108    Long64_t totfileentries = 0ULL;    UInt_t totfileentries = 0;
109    Long64_t idRun = 0LL;    UInt_t idRun = 0;
110      //
111      // My variables. Vitaly.
112      //
113      //  UInt_t iev = 0;
114      //  UInt_t j3 = 0;
115      UInt_t oi = 0;
116      Int_t tmpSize = 0;
117    //    //
118    // variables needed to handle error signals    // variables needed to handle error signals
119    //    //
# Line 116  int OrbitalInfoCore(ULong64_t run, TFile Line 129  int OrbitalInfoCore(ULong64_t run, TFile
129    //    //
130    TFile *l0File = 0;    TFile *l0File = 0;
131    TTree *l0tr = 0;    TTree *l0tr = 0;
132    TBranch *l0registry = 0;    TTree *l0trm = 0;
   pamela::RegistryEvent *l0reg=0;  
133    // EM: open also header branch    // EM: open also header branch
134    TBranch *l0head = 0;    TBranch *l0head = 0;
135    pamela::EventHeader *eh = 0;    pamela::EventHeader *eh = 0;
136    pamela::PscuHeader *ph = 0;    pamela::PscuHeader *ph = 0;
137      pamela::McmdEvent *mcmdev = 0;
138      pamela::McmdRecord *mcmdrc = 0;
139    // end EM    // end EM
140      
141      //  pamela::RunHeaderEvent *reh = new pamela::RunHeaderEvent;
142      //  pamela::EventHeader    *eH  = new pamela::EventHeader;
143      
144    //    //
145    // Define other basic variables    // Define other basic variables
146    //    //
# Line 131  int OrbitalInfoCore(ULong64_t run, TFile Line 149  int OrbitalInfoCore(ULong64_t run, TFile
149    stringstream file3;    stringstream file3;
150    stringstream qy;    stringstream qy;
151    Int_t totevent = 0;    Int_t totevent = 0;
152    ULong64_t atime = 0ULL;    UInt_t atime = 0;
153    Int_t ei = 0;    UInt_t re = 0;
154    Int_t re = 0;    UInt_t ik = 0;
155    
156      // Position
157      Float_t lon, lat, alt;
158    
159      //
160      // IGRF stuff
161      //
162      float dimo = 0.0; // dipole moment (computed from dat files)
163      float bnorth, beast, bdown, babs;
164      float xl; // L value
165      float icode; // code value for L accuracy (see fortran code)
166      float bab1; // What's  the difference with babs?
167      float stps = 0.005; // step size for field line tracing
168      float bdel = 0.01; // required accuracy
169      float bequ;  // equatorial b value (also called b_0)
170      bool value = 0; // false if bequ is not the minimum b value
171      float rr0; // equatorial radius normalized to earth radius
172    
173    //    //
174    // Working filename    // Working filename
175    //    //
# Line 148  int OrbitalInfoCore(ULong64_t run, TFile Line 184  int OrbitalInfoCore(ULong64_t run, TFile
184    TTree *tempOrbitalInfo = 0;    TTree *tempOrbitalInfo = 0;
185    stringstream tempname;    stringstream tempname;
186    stringstream OrbitalInfofolder;    stringstream OrbitalInfofolder;
187      Bool_t myfold = false;
188    tempname.str("");    tempname.str("");
189    tempname << outDir;    tempname << outDir;
190    tempname << "/" << processFolder.Data();    tempname << "/" << processFolder.Data();
191    OrbitalInfofolder.str("");    OrbitalInfofolder.str("");
192    OrbitalInfofolder << tempname.str().c_str();    OrbitalInfofolder << tempname.str().c_str();
   gSystem->MakeDirectory(OrbitalInfofolder.str().c_str());  
193    tempname << "/OrbitalInfotree_run";    tempname << "/OrbitalInfotree_run";
194    tempname << run << ".root";      tempname << run << ".root";  
195    //    //
196    // DB classes    // DB classes
197    //    //
198    GL_ROOT *glroot = new GL_ROOT();    GL_ROOT *glroot = new GL_ROOT();
199      GL_TIMESYNC *dbtime = 0;
200      GL_TLE *gltle = new GL_TLE();
201      //
202      //Quaternions classes
203      //
204      Quaternions *L_QQ_Q_l_lower = new Quaternions();
205      InclinationInfo *RYPang_lower = new InclinationInfo();
206      Quaternions *L_QQ_Q_l_upper = new Quaternions();
207      InclinationInfo *RYPang_upper = new InclinationInfo();
208      
209      cEci eCi;
210      
211      // Initialize fortran routines!!!
212      Int_t ltp2 = 0;
213      Int_t ltp3 = 0;
214      Int_t uno = 1;
215      char *niente = " ";
216      GL_PARAM *glparam = new GL_PARAM();
217      GL_PARAM *glparam2 = new GL_PARAM();
218      Int_t parerror=glparam->Query_GL_PARAM(1,301,dbc); // parameters stored in DB in GL_PRAM table
219      
220      if ( parerror<0 ) {
221        code = parerror;
222        goto closeandexit;
223      };
224      ltp2 = (Int_t)(glparam->PATH+glparam->NAME).Length();
225      if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam->PATH+glparam->NAME).Data());
226      //
227      parerror=glparam2->Query_GL_PARAM(1,302,dbc); // parameters stored in DB in GL_PRAM table
228      if ( parerror<0 ) {
229        code = parerror;
230        goto closeandexit;
231      };
232      ltp3 = (Int_t)(glparam2->PATH+glparam2->NAME).Length();
233      if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam2->PATH+glparam2->NAME).Data());
234      //
235      initize_((char *)niente,&uno,(char *)(glparam->PATH+glparam->NAME).Data(),&ltp2,(char *)(glparam2->PATH+glparam2->NAME).Data(),&ltp3);
236      //
237      // End IGRF stuff//
238      //
239    
240    //    //
241    // Let's start!    // Let's start!
242    //    //
# Line 167  int OrbitalInfoCore(ULong64_t run, TFile Line 244  int OrbitalInfoCore(ULong64_t run, TFile
244    // if run != 0 we must process only that run but first we have to check if the tree MyDetector2 already exist in the file    // if run != 0 we must process only that run but first we have to check if the tree MyDetector2 already exist in the file
245    // if it exists we are reprocessing data and we must delete that entries, if not we must create it.    // if it exists we are reprocessing data and we must delete that entries, if not we must create it.
246    //    //
247    if ( run == 0ULL )  reproc = true;    if ( run == 0 )  reproc = true;
248    //    //
249    //    //
250    // Output file is "outputfile"    // Output file is "outputfile"
# Line 214  int OrbitalInfoCore(ULong64_t run, TFile Line 291  int OrbitalInfoCore(ULong64_t run, TFile
291    // number of run to be processed    // number of run to be processed
292    //    //
293    numbofrun = runinfo->GetNoRun();    numbofrun = runinfo->GetNoRun();
294      UInt_t totnorun = runinfo->GetRunEntries();
295    //    //
296    // 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
297    //    //
# Line 224  int OrbitalInfoCore(ULong64_t run, TFile Line 302  int OrbitalInfoCore(ULong64_t run, TFile
302      // tree does not exist, we are not reprocessing      // tree does not exist, we are not reprocessing
303      //      //
304      reproc = false;      reproc = false;
305      if ( run == 0ULL ){      if ( run == 0 ){
306        if (verbose) printf(" OrbitalInfo - WARNING: you are reprocessing data but OrbitalInfo tree does not exist!\n");        if (verbose) printf(" OrbitalInfo - WARNING: you are reprocessing data but OrbitalInfo tree does not exist!\n");
307      }      }
308      if ( runinfo->IsReprocessing() && run != 0ULL ) {      if ( runinfo->IsReprocessing() && run != 0 ) {
309        if (verbose) printf(" OrbitalInfo - WARNING: it seems you are not reprocessing data but OrbitalInfo\n versioning information already exists in RunInfo.\n");        if (verbose) printf(" OrbitalInfo - WARNING: it seems you are not reprocessing data but OrbitalInfo\n versioning information already exists in RunInfo.\n");
310      }      }
311    } else {    } else {
312      //      //
313      // tree exists, we are reprocessing data. Are we reprocessing a single run or all the file?      // tree exists, we are reprocessing data. Are we reprocessing a single run or all the file?
314      //      //
315        OrbitalInfotrclone->SetAutoSave(900000000000000LL);
316      reproc = true;      reproc = true;
317      //      //
318      //      //
319      if (verbose) printf("\n Preparing the pre-processing...\n");      if (verbose) printf("\n Preparing the pre-processing...\n");
320      //      //
321      if ( run == 0ULL ){      if ( run == 0 || totnorun == 1 ){
322        //        //
323        // we are reprocessing all the file        // we are reprocessing all the file
324        // if we are reprocessing everything we don't need to copy any old event and we can just work with the new tree and delete the old one immediately        // if we are reprocessing everything we don't need to copy any old event and we can just work with the new tree and delete the old one immediately
# Line 254  int OrbitalInfoCore(ULong64_t run, TFile Line 333  int OrbitalInfoCore(ULong64_t run, TFile
333        //        //
334        reprocall = false;        reprocall = false;
335        //        //
336        if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing run number %llu \n",run);        if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing run number %u \n",run);
337        //        //
338        // copying old tree to a new file        // copying old tree to a new file
339        //        //
340          gSystem->MakeDirectory(OrbitalInfofolder.str().c_str());
341          myfold = true;
342        tempfile = new TFile(tempname.str().c_str(),"RECREATE");        tempfile = new TFile(tempname.str().c_str(),"RECREATE");
343        tempOrbitalInfo = OrbitalInfotrclone->CloneTree(-1,"fast");        tempOrbitalInfo = OrbitalInfotrclone->CloneTree(-1,"fast");
344        tempOrbitalInfo->SetName("OrbitalInfo-old");        tempOrbitalInfo->SetName("OrbitalInfo-old");
# Line 277  int OrbitalInfoCore(ULong64_t run, TFile Line 358  int OrbitalInfoCore(ULong64_t run, TFile
358    //    //
359    file->cd();    file->cd();
360    OrbitalInfotr = new TTree("OrbitalInfo-new","PAMELA OrbitalInfo data");    OrbitalInfotr = new TTree("OrbitalInfo-new","PAMELA OrbitalInfo data");
361      OrbitalInfotr->SetAutoSave(900000000000000LL);
362    OrbitalInfotr->Branch("OrbitalInfo","OrbitalInfo",&orbitalinfo);    OrbitalInfotr->Branch("OrbitalInfo","OrbitalInfo",&orbitalinfo);
363    //    //
364    if ( reproc && !reprocall ){    if ( reproc && !reprocall ){
# Line 285  int OrbitalInfoCore(ULong64_t run, TFile Line 367  int OrbitalInfoCore(ULong64_t run, TFile
367      //      //
368      tempfile = new TFile(tempname.str().c_str(),"READ");      tempfile = new TFile(tempname.str().c_str(),"READ");
369      OrbitalInfotrclone = (TTree*)tempfile->Get("OrbitalInfo-old");      OrbitalInfotrclone = (TTree*)tempfile->Get("OrbitalInfo-old");
370        OrbitalInfotrclone->SetAutoSave(900000000000000LL);
371      OrbitalInfotrclone->SetBranchAddress("OrbitalInfo",&orbitalinfoclone);      OrbitalInfotrclone->SetBranchAddress("OrbitalInfo",&orbitalinfoclone);
372      //            //      
373      if ( nobefrun > 0 ){      if ( nobefrun > 0 ){
374        if (verbose){        if (verbose){
375        printf("\n Pre-processing: copying events from the old tree before the processed run\n");            printf("\n Pre-processing: copying events from the old tree before the processed run\n");  
376        printf(" Copying %u events in the file which are before the beginning of the run %llu \n",nobefrun,run);          printf(" Copying %u events in the file which are before the beginning of the run %u \n",nobefrun,run);
377        printf(" Start copying at event number 0, end copying at event number %u \n",nobefrun);          printf(" Start copying at event number 0, end copying at event number %u \n",nobefrun);
378        }        }
379        for (UInt_t j = 0; j < nobefrun; j++){        for (UInt_t j = 0; j < nobefrun; j++){
380          //          //
# Line 299  int OrbitalInfoCore(ULong64_t run, TFile Line 382  int OrbitalInfoCore(ULong64_t run, TFile
382          //          //
383          // copy orbitalinfoclone to mydec          // copy orbitalinfoclone to mydec
384          //          //
         //      orbitalinfo = new OrbitalInfo();  
385          orbitalinfo->Clear();          orbitalinfo->Clear();
386            //
387          memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone));          memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone));
388          //          //
389          // Fill entry in the new tree          // Fill entry in the new tree
# Line 322  int OrbitalInfoCore(ULong64_t run, TFile Line 405  int OrbitalInfoCore(ULong64_t run, TFile
405      //      //
406      // retrieve the first run ID to be processed using the RunInfo list      // retrieve the first run ID to be processed using the RunInfo list
407      //      //
408        
409      idRun = runlist->At(irun);      idRun = runlist->At(irun);
410      if (verbose){      if (verbose){
411        printf("\n\n\n ####################################################################### \n");        printf("\n\n\n ####################################################################### \n");
# Line 329  int OrbitalInfoCore(ULong64_t run, TFile Line 413  int OrbitalInfoCore(ULong64_t run, TFile
413        printf(" ####################################################################### \n\n\n");        printf(" ####################################################################### \n\n\n");
414      }      }
415      //      //
416      runinfo->ID_REG_RUN = 0ULL;      runinfo->ID_ROOT_L0 = 0;
417      //      //
418      // store in the runinfo class the GL_RUN variables for our run      // store in the runinfo class the GL_RUN variables for our run
419      //      //
420      sgnl = 0;      sgnl = 0;
421      sgnl = runinfo->GetRunInfo(idRun);      sgnl = runinfo->GetRunInfo(idRun);
422      if ( sgnl ){      if ( sgnl ){
423        //printf("\n OrbitalInfo - ERROR: RunInfo exited with non-zero status\n");        if ( debug ) printf("\n OrbitalInfo - ERROR: RunInfo exited with non-zero status\n");
424        code = sgnl;        code = sgnl;
425        goto closeandexit;        goto closeandexit;
426      } else {      } else {
# Line 345  int OrbitalInfoCore(ULong64_t run, TFile Line 429  int OrbitalInfoCore(ULong64_t run, TFile
429      //      //
430      // now you can access that variables using the RunInfo class this way runinfo->ID_REG_RUN      // now you can access that variables using the RunInfo class this way runinfo->ID_REG_RUN
431      //      //
432      if ( runinfo->ID_REG_RUN == 0 ){      if ( runinfo->ID_ROOT_L0 == 0 ){
433        //printf("\n OrbitalInfo - ERROR: no run with ID_RUN = %i \n\n Exiting... \n\n",(int)idRun);        if ( debug ) printf("\n OrbitalInfo - ERROR: no run with ID_RUN = %u \n\n Exiting... \n\n",idRun);
434        code = -5;        code = -5;
435        goto closeandexit;            goto closeandexit;    
436      };      };
437      //      //
438        // prepare the timesync for the db
439        //
440        dbtime = new GL_TIMESYNC(runinfo->ID_ROOT_L0,"ID",dbc);
441      
442        //
443      // Search in the DB the path and name of the LEVEL0 file to be processed.      // Search in the DB the path and name of the LEVEL0 file to be processed.
444      //      //
445      glroot->Query_GL_ROOT(runinfo->ID_REG_RUN,dbc);      glroot->Query_GL_ROOT(runinfo->ID_ROOT_L0,dbc);
446      //      //
447      ftmpname.str("");      ftmpname.str("");
448      ftmpname << glroot->PATH.Data() << "/";      ftmpname << glroot->PATH.Data() << "/";
449      ftmpname << glroot->NAME.Data();      ftmpname << glroot->NAME.Data();
450      fname = ftmpname.str().c_str();      fname = ftmpname.str().c_str();
451        ftmpname.str("");
452      //      //
453      // print out informations      // print out informations
454      //      //
455      totevent = runinfo->EV_REG_PHYS_TO - runinfo->EV_REG_PHYS_FROM + 1;      totevent = runinfo->NEVENTS;
456        //cout<<"totevents = "<<totevent<<"\n";
457      if (verbose){      if (verbose){
458        printf("\n LEVEL0 data file: %s \n",fname.Data());        printf("\n LEVEL0 data file: %s \n",fname.Data());
459        printf(" RUN HEADER absolute time is:  %llu \n",runinfo->RUNHEADER_TIME);        printf(" RUN HEADER absolute time is:  %u \n",runinfo->RUNHEADER_TIME);
460        printf(" RUN TRAILER absolute time is: %llu \n",runinfo->RUNTRAILER_TIME);        printf(" RUN TRAILER absolute time is: %u \n",runinfo->RUNTRAILER_TIME);
461        printf(" %i events to be processed for run %llu: from %i to %i (reg entries)\n\n",totevent,idRun,runinfo->EV_REG_PHYS_FROM,runinfo->EV_REG_PHYS_TO);        printf(" %i events to be processed for run %u: from %i to %i \n\n",totevent,idRun,runinfo->EV_FROM+1,runinfo->EV_FROM+totevent);
462      }//      }//
463      // Open Level0 file      // Open Level0 file
464      l0File = new TFile(fname.Data());      l0File = new TFile(fname.Data());
465      if ( !l0File ) {      if ( !l0File ) {
466        //printf(" OrbitalInfo - ERROR: problems opening Level0 file\n");        if ( debug ) printf(" OrbitalInfo - ERROR: problems opening Level0 file\n");
467        code = -6;        code = -6;
468        goto closeandexit;        goto closeandexit;
469      };      };
470      l0tr = (TTree*)l0File->Get("Physics");      l0tr = (TTree*)l0File->Get("Physics");
471      if ( !l0tr ) {      if ( !l0tr ) {
472        //printf(" OrbitalInfo - ERROR: no Physics tree in Level0 file\n");        if ( debug ) printf(" OrbitalInfo - ERROR: no Physics tree in Level0 file\n");
473        l0File->Close();        l0File->Close();
474        code = -7;        code = -7;
475        goto closeandexit;        goto closeandexit;
# Line 386  int OrbitalInfoCore(ULong64_t run, TFile Line 477  int OrbitalInfoCore(ULong64_t run, TFile
477      // EM: open header branch as well      // EM: open header branch as well
478      l0head = l0tr->GetBranch("Header");      l0head = l0tr->GetBranch("Header");
479      if ( !l0head ) {      if ( !l0head ) {
480        //if ( verbose ) printf(" CALORIMETER - ERROR: no Header branch in Level0 tree\n");        if ( debug ) printf(" OrbitalInfo - ERROR: no Header branch in Level0 tree\n");
481        l0File->Close();        l0File->Close();
482        code = -8;        code = -8;
483        goto closeandexit;            goto closeandexit;    
484      };      };
485      l0tr->SetBranchAddress("Header", &eh);      l0tr->SetBranchAddress("Header", &eh);
486      // end EM      // end EM
487      l0registry = l0tr->GetBranch("Registry");      nevents = l0head->GetEntries();
     if ( !l0registry ) {  
       //printf(" OrbitalInfo - ERROR: no Registry branch in Level0 tree\n");  
       l0File->Close();  
       code = -9;  
       goto closeandexit;      
     };  
     //  
     l0tr->SetBranchAddress("Registry", &l0reg);  
     //  
     nevents = l0registry->GetEntries();  
488      //      //
489      if ( nevents < 1 ) {      if ( nevents < 1 ) {
490        //printf(" OrbitalInfo - ERROR: Level0 file is empty\n\n");        if ( debug ) printf(" OrbitalInfo - ERROR: Level0 file is empty\n\n");
491        l0File->Close();        l0File->Close();
492        code = -11;        code = -11;
493        goto closeandexit;        goto closeandexit;
494      };      };
495      //      //
496      if ( runinfo->EV_REG_PHYS_TO > nevents-1 ) {      if ( runinfo->EV_TO > nevents-1 ) {
497        //printf(" OrbitalInfo - ERROR: too few entries in the registry tree\n");        if ( debug ) printf(" OrbitalInfo - ERROR: too few entries in the registry tree\n");
498        l0File->Close();        l0File->Close();
499        code = -12;        code = -12;
500        goto closeandexit;        goto closeandexit;
501      };      };
502      //      //
503    //     TTree *tp = (TTree*)l0File->Get("RunHeader");
504    //     tp->SetBranchAddress("Header", &eH);
505    //     tp->SetBranchAddress("RunHeader", &reh);
506    //     tp->GetEntry(0);
507    //     ph = eH->GetPscuHeader();
508    //     ULong_t TimeSync = reh->LAST_TIME_SYNC_INFO;
509    //     ULong_t ObtSync = reh->OBT_TIME_SYNC;    
510    //     if ( debug ) printf(" 1 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",TimeSync,ObtSync,TimeSync-ObtSync);
511    //
512        ULong_t TimeSync = (ULong_t)dbtime->GetTimesync();
513        ULong_t ObtSync = (ULong_t)(dbtime->GetObt0()/1000);
514        ULong_t DeltaOBT = TimeSync - ObtSync;
515    
516        if ( debug ) printf(" 2 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",(ULong_t)(dbtime->GetTimesync()/1000),(ULong_t)dbtime->GetObt0(),TimeSync-ObtSync);
517        
518        l0trm = (TTree*)l0File->Get("Mcmd");
519        neventsm = l0trm->GetEntries();
520        //    neventsm = 0;
521        //
522        if (neventsm == 0){
523          if ( debug ) printf("InclinationInfo - WARNING: No quaternions in this File");
524          //      l0File->Close();
525          code = 900;
526          //      goto closeandexit;
527        }
528        //
529        
530        l0trm->SetBranchAddress("Mcmd", &mcmdev);
531        //    l0trm->SetBranchAddress("Header", &eh);
532        //
533        //
534        //
535        UInt_t mctren = 0;    
536        UInt_t mcreen = 0;  
537        UInt_t numrec = 0;
538        //
539        Double_t upperqtime = 0;
540        Double_t lowerqtime = 0;
541        
542        Double_t incli = 0;
543        oi = 0;
544        UInt_t ooi = 0;
545        //
546        // init quaternions sync
547        //
548        Bool_t isf = true;
549        Int_t fgh = 0;
550        //
551      // run over all the events of the run      // run over all the events of the run
552      //      //
553      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");
554      //      //
555      for ( re = runinfo->EV_REG_PHYS_FROM; re <= runinfo->EV_REG_PHYS_TO; re++){      //    if ( dbc ){
556        //      dbc->Close();
557          //      delete dbc;
558        //};
559        //
560        for ( re = runinfo->EV_FROM; re < (runinfo->EV_FROM+runinfo->NEVENTS); re++){
561        
562        //        //
563        if ( procev%1000 == 0 && procev > 0 && verbose) printf(" %iK \n",procev/1000);            if ( procev%1000 == 0 && procev > 0 && verbose ) printf(" %iK \n",procev/1000);  
564          if ( debug ) printf(" %i \n",procev);      
565        //        //
566        l0registry->GetEntry(re);        l0head->GetEntry(re);
567        //        //
568        // absolute time of this event        // absolute time of this event
569        //        //
570        atime = l0reg->absTime;        ph = eh->GetPscuHeader();
571        //        atime = dbtime->DBabsTime(ph->GetOrbitalTime());
       // physics events is at entry number ei where  
       //  
       ei = l0reg->event;  
572        //        //
573        // paranoid check        // paranoid check
574        //        //
575        if ( (atime > runinfo->RUNTRAILER_TIME) || (atime < runinfo->RUNHEADER_TIME)  ) {        if ( (atime > runinfo->RUNTRAILER_TIME) || (atime < runinfo->RUNHEADER_TIME)  ) {
576          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");
577          goto jumpev;  //      debug = true;
578        };          continue;
579          }
580        //        //
581        procev++;        procev++;
582        //        //
583        // start processing        // start processing
584        //        //
585        orbitalinfo->Clear();        orbitalinfo->Clear();
586        //orbitalinfo = new OrbitalInfo();        //
587        orbitalinfo->absTime = l0reg->absTime;        // Fill OBT, pkt_num and absTime
588        // EM: add OBT and plt_num infos from the header        //      
589        l0head->GetEntry(ei);        //      ph = eh->GetPscuHeader();
       ph = eh->GetPscuHeader();  
590        orbitalinfo->pkt_num = ph->GetCounter();        orbitalinfo->pkt_num = ph->GetCounter();
591        orbitalinfo->OBT = ph->GetOrbitalTime();        orbitalinfo->OBT = ph->GetOrbitalTime();
592        // end EM        orbitalinfo->absTime = atime;
       OrbitalInfotr->Fill();  
       //      
593        //        //
594      jumpev:        // Propagate the orbit from the tle time to atime, using SGP(D)4.
       debug = false;  
595        //        //
596      };        cCoordGeo coo;
597          float jyear=0;    
598          //
599          if(atime >= gltle->GetToTime()) {
600            if ( !gltle->Query(atime, dbc) ){
601              //      
602              // Compute the magnetic dipole moment.
603              //
604              UInt_t year, month, day, hour, min, sec;
605              //
606              TTimeStamp t = TTimeStamp(atime, kTRUE);
607              t.GetDate(kTRUE, 0, &year, &month, &day);
608              t.GetTime(kTRUE, 0, &hour, &min, &sec);
609              jyear = (float) year
610                + (month*31.+ (float) day)/365.
611                + (hour*3600.+min*60.+(float)sec)/(24*3600*365.);
612              //
613              feldcof_(&jyear, &dimo); // get dipole moment for year
614            } else {
615              code = -56;
616              goto closeandexit;
617            };
618          }
619          coo = getCoo(atime, gltle->GetFromTime(), gltle->GetTle());
620          //
621          cOrbit orbits(*gltle->GetTle());
622          //
623          if ( debug ) printf(" I am Here \n");
624          //
625          // synchronize with quaternions data
626          //
627          if ( isf && neventsm>0 ){
628            if ( debug ) printf(" I am here \n");
629            //
630            // First event
631            //
632            isf = false;
633            upperqtime = atime;
634            lowerqtime = runinfo->RUNHEADER_TIME;
635            for ( ik = 0; ik < neventsm; ik++){
636              l0trm->GetEntry(ik);
637              tmpSize = mcmdev->Records->GetEntries();
638              numrec = tmpSize;
639              for (Int_t j3 = 0;j3<tmpSize;j3++){
640                mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(j3);
641                if ((int)mcmdrc->ID1 == 226){
642                  L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
643                  for (UInt_t ui = 0; ui < 6; ui++){
644                    if (ui>0){
645                      if (L_QQ_Q_l_upper->time[ui]>L_QQ_Q_l_upper->time[0]){
646                        if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000))<atime){
647                          upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));
648                          orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
649                          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]);
650                        }else {
651                          lowerqtime = upperqtime;
652                          upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));
653                          orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
654                          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]);
655                          mcreen = j3;
656                          mctren = ik;
657                          if(fgh==0){
658                            CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
659                            CopyAng(RYPang_lower,RYPang_upper);
660                          }
661                          oi=ui;
662                          goto closethisloop;
663                        }
664                        fgh++;
665                        CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
666                        CopyAng(RYPang_lower,RYPang_upper);
667                      }
668                    }else{
669                      if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))<atime){
670                        upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
671                        orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
672                        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]);
673                      }
674                      else {
675                        lowerqtime = upperqtime;
676                        upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
677                        orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
678                        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]);
679                        mcreen = j3;
680                        mctren = ik;
681                        if(fgh==0){
682                          CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
683                          CopyAng(RYPang_lower,RYPang_upper);
684                          lowerqtime = atime-1;
685                        }
686                        oi=ui;
687                        goto closethisloop;
688                        //_0 = true;
689                      }
690                      fgh++;
691                      CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
692                      CopyAng(RYPang_lower,RYPang_upper);
693                      //_0 = true;
694                    };
695                    //cin>>grib;
696                  };
697                };
698              };
699            };
700          };
701        closethisloop:
702          //
703          if ( debug ) printf(" I am There \n");
704          //
705          if (((atime>(UInt_t)upperqtime)||(atime<(UInt_t)lowerqtime)) && neventsm>0 ){
706            if ( debug ) printf(" I am there \n");
707            //
708            lowerqtime = upperqtime;
709            Long64_t maxloop = 100000000LL;
710            Long64_t mn = 0;
711            bool gh=false;
712            ooi=oi;
713            if ( verbose ) printf(" OrbitalInfoCore: sync with quaternions data upperqtime %u lowerqtime %u atime %u \n",(UInt_t)upperqtime,(UInt_t)lowerqtime,atime);
714            while (!gh){      
715              if ( mn > maxloop ){
716                if ( verbose ) printf(" OrbitalInfoCore: quaternions sync out of range! exiting\n");
717                gh = true;
718                neventsm = 0;
719              };
720              mn++;
721              if (oi<5) oi++;
722              else oi=0;
723              if (oi==0){
724                mcreen++;
725                if (mcreen == numrec){
726                  mctren++;
727                  mcreen = 0;
728                  l0trm->GetEntry(mctren);
729                  numrec = mcmdev->Records->GetEntries();
730                }
731                CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
732                CopyAng(RYPang_lower,RYPang_upper);
733                mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(mcreen);
734                if ((int)mcmdrc->ID1 == 226){
735                  L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
736                  upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
737                  if (upperqtime<lowerqtime){
738                    upperqtime=runinfo->RUNTRAILER_TIME;
739                    CopyQ(L_QQ_Q_l_upper,L_QQ_Q_l_lower);
740                    CopyAng(RYPang_upper,RYPang_lower);
741                  }else{
742                    orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
743                    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]);
744                  }
745                  //              re--;
746                  gh=true;
747                }
748              }else{
749                if ((Int_t)L_QQ_Q_l_upper->time[oi]>(Int_t)L_QQ_Q_l_upper->time[0]){
750                  upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
751                  orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
752                  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]);
753                  orbits.getPosition((double) (lowerqtime - gltle->GetFromTime())/60., &eCi);
754                  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]);
755                  //              re--;
756                  gh=true;
757                };
758              };
759            };
760            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);
761          };
762          //
763          if ( debug ) printf(" I am THIS \n");
764          //
765          // Fill in quaternions and angles
766          //
767          if ((atime<=(UInt_t)upperqtime)&&(atime>=(UInt_t)lowerqtime)&& neventsm>0){      
768            if ( debug ) printf(" I am this \n");
769            UInt_t tut = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi);
770            if (oi == 0){
771              if ((tut!=5)||(tut!=6)){
772                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)));
773                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));
774                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)));
775                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));
776                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)));
777                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));
778                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)));
779                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));
780            
781                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)));
782                orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
783                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)));
784                orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
785                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)));
786                orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
787              }
788              if (tut==6){
789                if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){
790                  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)));
791                  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));
792                  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)));
793                  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));
794                  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)));
795                  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));
796                  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)));
797                  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));
798            
799                  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)));
800                  orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
801                  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)));
802                  orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
803                  //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";
804                  //cin>>grib;
805                  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)));
806                  orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
807                }
808              }
809            } else {
810              if((tut!=6)||(tut!=7)||(tut!=9)){
811                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)));
812                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));
813                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)));
814                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));
815                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)));
816                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));
817                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)));
818                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));
819            
820                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)));
821                orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
822                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)));
823                orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
824                //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";
825                //cin>>grib;
826                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)));
827                orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
828              }
829              if (tut==6){
830                if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){
831                  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)));
832                  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));
833                  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)));
834                  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));
835                  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)));
836                  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));
837                  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)));
838                  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));
839            
840                  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)));
841                  orbitalinfo->theta =  incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
842                  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)));
843                  orbitalinfo->phi =  incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
844                  //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";
845                  //cin>>grib;
846                  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)));
847                  orbitalinfo->etha =  incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
848                }
849              }            
850            }
851            //
852            orbitalinfo->mode = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi);
853            //
854          } else {
855            if ( debug ) printf(" ops no incl! \n");
856            orbitalinfo->mode = -1;
857          };
858      
859          //
860          // fill orbital positions
861          //        
862          // Build coordinates in the right range.  We want to convert,
863          // longitude from (0, 2*pi) to (-180deg, 180deg).  Altitude is
864          // in meters.
865          lon = (coo.m_Lon > M_PI) ? rad2deg(coo.m_Lon - 2*M_PI) : rad2deg(coo.m_Lon);
866          lat = rad2deg(coo.m_Lat);
867          alt = coo.m_Alt;
868          //
869          if( lon<180 && lon>-180 && lat<90 && lat>-90 && alt>0 ){  
870            //      
871            orbitalinfo->lon = lon;
872            orbitalinfo->lat = lat;
873            orbitalinfo->alt = alt ;
874            //
875            // compute mag field components and L shell.
876            //
877            feldg_(&lat, &lon, &alt, &bnorth, &beast, &bdown, &babs);
878            shellg_(&lat, &lon, &alt, &dimo, &xl, &icode, &bab1);
879            findb0_(&stps, &bdel, &value, &bequ, &rr0);
880            //
881            orbitalinfo->Bnorth = bnorth;
882            orbitalinfo->Beast = beast;
883            orbitalinfo->Bdown = bdown;
884            orbitalinfo->Babs = babs;
885            orbitalinfo->BB0 = babs/bequ;
886            orbitalinfo->L = xl;      
887            // Set Stormer vertical cutoff using L shell.
888            orbitalinfo->cutoff[0] = 14.9/(xl*xl);
889            //
890          };      
891          //
892          // Fill the class
893          //
894          OrbitalInfotr->Fill();
895          //
896        }; // loop over the events in the run
897      //      //
898      // Here you may want to clear some variables before processing another run        // Here you may want to clear some variables before processing another run  
899      //      //
900      ei = 0;      delete dbtime;
901        if ( L_QQ_Q_l_upper ) delete L_QQ_Q_l_upper;
902        if ( L_QQ_Q_l_lower ) delete L_QQ_Q_l_lower;
903        if ( RYPang_upper ) delete RYPang_upper;
904        if ( RYPang_lower ) delete RYPang_lower;
905    }; // process all the runs    }; // process all the runs
906    //    
907    if (verbose) printf("\n Finished processing data \n");    if (verbose) printf("\n Finished processing data \n");
908    //    //
909   closeandexit:   closeandexit:
# Line 492  int OrbitalInfoCore(ULong64_t run, TFile Line 926  int OrbitalInfoCore(ULong64_t run, TFile
926          // copy orbitalinfoclone to OrbitalInfo          // copy orbitalinfoclone to OrbitalInfo
927          //          //
928          orbitalinfo->Clear();          orbitalinfo->Clear();
929          //      orbitalinfo = new OrbitalInfo();          //
930          memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone));          memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone));
931          //          //
932          // Fill entry in the new tree          // Fill entry in the new tree
# Line 507  int OrbitalInfoCore(ULong64_t run, TFile Line 941  int OrbitalInfoCore(ULong64_t run, TFile
941    //    //
942    if ( l0File ) l0File->Close();    if ( l0File ) l0File->Close();
943    if ( tempfile ) tempfile->Close();                if ( tempfile ) tempfile->Close();            
944    gSystem->Unlink(tempname.str().c_str());    if ( myfold ) gSystem->Unlink(tempname.str().c_str());
945      //
   //if ( code < 0 ) printf("\n OrbitalInfo - ERROR: an error occurred, try to save anyway...\n");  
   //printf("\n Writing and closing rootple\n");  
946    if ( runinfo ) runinfo->Close();        if ( runinfo ) runinfo->Close();    
947    if ( OrbitalInfotr ) OrbitalInfotr->SetName("OrbitalInfo");        if ( OrbitalInfotr ) OrbitalInfotr->SetName("OrbitalInfo");    
948    if ( file ){    if ( file ){
# Line 518  int OrbitalInfoCore(ULong64_t run, TFile Line 950  int OrbitalInfoCore(ULong64_t run, TFile
950      file->Write();      file->Write();
951    };    };
952    //    //
953    gSystem->Unlink(OrbitalInfofolder.str().c_str());    if ( myfold ) gSystem->Unlink(OrbitalInfofolder.str().c_str());
954    //    //
955    // the end    // the end
956    //    //
# Line 534  int OrbitalInfoCore(ULong64_t run, TFile Line 966  int OrbitalInfoCore(ULong64_t run, TFile
966    return(code);    return(code);
967  }  }
968    
969    
970    //
971    // Returns the cCoordGeo structure holding the geographical
972    // coordinates for the event (see sgp4.h).
973    //
974    // atime is the abstime of the event in UTC unix time.
975    // tletime is the time of the tle in UTC unix time.
976    // tle is the previous and nearest tle (compared to atime).
977    cCoordGeo getCoo(UInt_t atime, UInt_t tletime, cTle *tle)
978    {
979      cEci eci;
980      cOrbit orbit(*tle);
981      orbit.getPosition((double) (atime - tletime)/60., &eci);
982      
983      return eci.toGeo();
984    }
985    
986    // function of copyng of quatrnions classes
987    
988    void CopyQ(Quaternions *Q1, Quaternions *Q2){
989      for(UInt_t i = 0; i < 6; i++){
990        Q1->time[i]=Q2->time[i];
991        for (UInt_t j = 0; j < 4; j++)Q1->quat[i][j]=Q2->quat[i][j];
992      }
993      return;
994    }
995    
996    // functions of copyng InclinationInfo classes
997    
998    void CopyAng(InclinationInfo *A1, InclinationInfo *A2){
999      A1->Tangazh = A2->Tangazh;
1000      A1->Ryskanie = A2->Ryskanie;
1001      A1->Kren = A2->Kren;
1002      return;
1003    }
1004    
1005    UInt_t holeq(Double_t lower,Double_t upper,Quaternions *Qlower, Quaternions *Qupper, UInt_t f){
1006      
1007      UInt_t hole = 10;
1008      bool R10l = false;     // Sign of R10 mode in lower quaternions array
1009      bool R10u = false;     // Sign of R10 mode in upper quaternions array
1010      bool insm = false;     // Sign that we inside quaternions array
1011      bool mxtml = false;    // Sign of mixt mode in lower quaternions array
1012      bool mxtmu = false;    // Sign of mixt mode in upper quaternions array
1013      bool npasm = false;     // Sign of normall pass between R10 and non R10 or between non R10 and R10
1014      UInt_t NCQl = 6;       // Number of correct quaternions in lower array
1015      UInt_t NCQu = 6;       // Number of correct quaternions in upper array
1016      if (f>0){
1017        insm = true;
1018        if(Qupper->time[f]-Qupper->time[f-1]==30) R10u = false;
1019        if(Qupper->time[f]-Qupper->time[f-1]<1) R10u = true;
1020      }else{
1021        insm = false;
1022        if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]<2)) R10l = true;
1023        if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]<2)) R10u = true;
1024        if((Qlower->time[5]-Qlower->time[0]==150)&&(Qlower->time[1]-Qlower->time[0]==30)) R10l = false;
1025        if((Qupper->time[5]-Qupper->time[0]==150)&&(Qupper->time[1]-Qupper->time[0]==30)) R10u = false;
1026        if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]==30)){
1027          mxtml = true;
1028          for(UInt_t i = 1; i < 6; i++){
1029            if(Qlower->time[i]-Qlower->time[0]==30*i) NCQl=i;
1030          }
1031        }
1032        if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]==30)){
1033          mxtmu = true;
1034          for(UInt_t i = 1; i < 6; i++){
1035            if(Qupper->time[i]-Qupper->time[0]==30*i) NCQu=i;
1036          }
1037        }
1038      }
1039      
1040      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;
1041      
1042      
1043      if (R10u&&insm) hole=0; // best event R10
1044      if ((upper-lower<=5)&&(!insm)&&R10l&&R10u) hole = 1; // when first of 6 quaternions in array is correct
1045      if (((!R10u)&&insm)||((!insm)&&(!R10u)&&(!R10l)&&((upper-lower==210+(6-NCQl)*30)||(upper-lower==30)))) hole = 2; //non R10
1046      if (npasm&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 3; //normall pass from R10 to non R10 or from non R10 to R10
1047      if ((!npasm)&&(upper-lower<=300)&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 4; // eliminable hole between R10 and non R10 or between non R10 and R10
1048      if ((upper-lower>=300)&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 5; //uneliminable hole between R10 and non R10 or between non R10 and R10
1049      if ((upper-lower>5)&&(upper-lower<=300)&&R10u&&R10l) hole = 6; // eliminable hole inside R10
1050      if ((upper-lower>300)&&R10u&&R10l) hole = 7; //uneliminable hole inside R10
1051      if ((upper-lower>210)&&(upper-lower<=1200)&&(!R10u)&&(!R10l)) hole = 8; //eliminable hole inside non R10
1052      if ((upper-lower>1200)&&!R10u&&!R10l) hole = 9; // uneliminable hole inside non R10
1053      return hole;
1054    }
1055    
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