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

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Revision 1.20 - (show annotations) (download)
Sat May 5 12:50:29 2007 UTC (18 years, 7 months ago) by mocchiut
Branch: MAIN
Changes since 1.19: +1 -1 lines
Wrong debug setting when outside time window fixed

1 //
2 // C/C++ headers
3 //
4 #include <fstream>
5 #include <string.h>
6 #include <iostream>
7 #include <cstring>
8 #include <stdio.h>
9 //
10 // ROOT headers
11 //
12 #include <TTree.h>
13 #include <TClassEdit.h>
14 #include <TObject.h>
15 #include <TList.h>
16 #include <TArrayI.h>
17 #include <TSystem.h>
18 #include <TSystemDirectory.h>
19 #include <TString.h>
20 #include <TFile.h>
21 #include <TClass.h>
22 #include <TSQLServer.h>
23 #include <TSQLRow.h>
24 #include <TSQLResult.h>
25 //
26 // RunInfo header
27 //
28 #include <RunInfo.h>
29 #include <GLTables.h>
30 //
31 // YODA headers
32 //
33 #include <PamelaRun.h>
34 #include <PscuHeader.h>
35 #include <PscuEvent.h>
36 #include <EventHeader.h>
37 #include <mcmd/McmdEvent.h>
38 #include <mcmd/McmdRecord.h>
39 //
40 // This program headers
41 //
42 #include <OrbitalInfo.h>
43 #include <OrbitalInfoVerl2.h>
44 #include <OrbitalInfoCore.h>
45 #include <InclinationInfo.h>
46
47 using namespace std;
48
49 //
50 // CORE ROUTINE
51 //
52 //
53 int OrbitalInfoCore(UInt_t run, TFile *file, TSQLServer *dbc, Int_t OrbitalInfoargc, char *OrbitalInfoargv[]){
54 //
55 Int_t i = 0;
56 //
57 TString processFolder = Form("OrbitalInfoFolder_%u",run);
58 //
59 // Set these to true to have a very verbose output.
60 //
61 Bool_t debug = false;
62 //
63 Bool_t verbose = false;
64
65 if ( OrbitalInfoargc > 0 ){
66 i = 0;
67 while ( i < OrbitalInfoargc ){
68 if ( !strcmp(OrbitalInfoargv[i],"-processFolder") ) {
69 if ( OrbitalInfoargc < i+1 ){
70 throw -3;
71 };
72 processFolder = (TString)OrbitalInfoargv[i+1];
73 i++;
74 };
75 if ( (!strcmp(OrbitalInfoargv[i],"--debug")) || (!strcmp(OrbitalInfoargv[i],"-g")) ) {
76 verbose = true;
77 debug = true;
78 };
79 if ( (!strcmp(OrbitalInfoargv[i],"--verbose")) || (!strcmp(OrbitalInfoargv[i],"-v")) ) {
80 verbose = true;
81 };
82 i++;
83 };
84 };
85 //
86 const char* outDir = gSystem->DirName(gSystem->DirName(file->GetPath()));
87 //
88 TTree *OrbitalInfotr = 0;
89 UInt_t nevents = 0;
90 UInt_t neventsm = 0;
91 //
92 // variables needed to reprocess data
93 //
94 Long64_t maxsize = 10000000000LL;
95 TTree::SetMaxTreeSize(maxsize);
96 //
97 TString OrbitalInfoversion;
98 ItoRunInfo *runinfo = 0;
99 TArrayI *runlist = 0;
100 TTree *OrbitalInfotrclone = 0;
101 Bool_t reproc = false;
102 Bool_t reprocall = false;
103 UInt_t nobefrun = 0;
104 UInt_t noaftrun = 0;
105 UInt_t numbofrun = 0;
106 stringstream ftmpname;
107 TString fname;
108 UInt_t totfileentries = 0;
109 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
119 //
120 Int_t code = 0;
121 Int_t sgnl;
122 //
123 // OrbitalInfo classes
124 //
125 OrbitalInfo *orbitalinfo = new OrbitalInfo();
126 OrbitalInfo *orbitalinfoclone = new OrbitalInfo();
127 //
128 // define variables for opening and reading level0 file
129 //
130 TFile *l0File = 0;
131 TTree *l0tr = 0;
132 TTree *l0trm = 0;
133 // EM: open also header branch
134 TBranch *l0head = 0;
135 pamela::EventHeader *eh = 0;
136 pamela::PscuHeader *ph = 0;
137 pamela::McmdEvent *mcmdev = 0;
138 pamela::McmdRecord *mcmdrc = 0;
139 // end EM
140
141 // pamela::RunHeaderEvent *reh = new pamela::RunHeaderEvent;
142 // pamela::EventHeader *eH = new pamela::EventHeader;
143
144 //
145 // Define other basic variables
146 //
147 UInt_t procev = 0;
148 stringstream file2;
149 stringstream file3;
150 stringstream qy;
151 Int_t totevent = 0;
152 UInt_t atime = 0;
153 UInt_t re = 0;
154 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
175 //
176 TString outputfile;
177 stringstream name;
178 name.str("");
179 name << outDir << "/";
180 //
181 // temporary file and folder
182 //
183 TFile *tempfile = 0;
184 TTree *tempOrbitalInfo = 0;
185 stringstream tempname;
186 stringstream OrbitalInfofolder;
187 tempname.str("");
188 tempname << outDir;
189 tempname << "/" << processFolder.Data();
190 OrbitalInfofolder.str("");
191 OrbitalInfofolder << tempname.str().c_str();
192 gSystem->MakeDirectory(OrbitalInfofolder.str().c_str());
193 tempname << "/OrbitalInfotree_run";
194 tempname << run << ".root";
195 //
196 // DB classes
197 //
198 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!
242 //
243 // As a first thing we must check what we have to do: if run = 0 we must process all events in the file has been passed
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
245 // if it exists we are reprocessing data and we must delete that entries, if not we must create it.
246 //
247 if ( run == 0 ) reproc = true;
248 //
249 //
250 // Output file is "outputfile"
251 //
252 if ( !file->IsOpen() ){
253 //printf(" OrbitalInfo - ERROR: cannot open file for writing\n");
254 throw -901;
255 };
256 //
257 // Retrieve GL_RUN variables from the level2 file
258 //
259 OrbitalInfoversion = OrbitalInfoInfo(false); // we should decide how to handle versioning system
260 //
261 // create an interface to RunInfo called "runinfo"
262 //
263 runinfo = new ItoRunInfo(file);
264 //
265 // open "Run" tree in level2 file, if not existing return an error (sngl != 0)
266 //
267 sgnl = 0;
268 sgnl = runinfo->Update(run, "ORB", OrbitalInfoversion);
269 //sgnl = runinfo->Read(run);
270
271 if ( sgnl ){
272 //printf("OrbitalInfo - ERROR: RunInfo exited with non-zero status\n");
273 code = sgnl;
274 goto closeandexit;
275 } else {
276 sgnl = 0;
277 };
278 //
279 // number of events in the file BEFORE the first event of our run
280 //
281 nobefrun = runinfo->GetFirstEntry();
282 //
283 // total number of events in the file
284 //
285 totfileentries = runinfo->GetFileEntries();
286 //
287 // first file entry AFTER the last event of our run
288 //
289 noaftrun = runinfo->GetLastEntry() + 1;
290 //
291 // number of run to be processed
292 //
293 numbofrun = runinfo->GetNoRun();
294 //
295 // Try to access the OrbitalInfo tree in the file, if it exists we are reprocessing data if not we are processing a new run
296 //
297 OrbitalInfotrclone = (TTree*)file->Get("OrbitalInfo");
298 //
299 if ( !OrbitalInfotrclone ){
300 //
301 // tree does not exist, we are not reprocessing
302 //
303 reproc = false;
304 if ( run == 0 ){
305 if (verbose) printf(" OrbitalInfo - WARNING: you are reprocessing data but OrbitalInfo tree does not exist!\n");
306 }
307 if ( runinfo->IsReprocessing() && run != 0 ) {
308 if (verbose) printf(" OrbitalInfo - WARNING: it seems you are not reprocessing data but OrbitalInfo\n versioning information already exists in RunInfo.\n");
309 }
310 } else {
311 //
312 // tree exists, we are reprocessing data. Are we reprocessing a single run or all the file?
313 //
314 OrbitalInfotrclone->SetAutoSave(900000000000000LL);
315 reproc = true;
316 //
317 //
318 if (verbose) printf("\n Preparing the pre-processing...\n");
319 //
320 if ( run == 0 ){
321 //
322 // we are reprocessing all the file
323 // 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
324 //
325 reprocall = true;
326 //
327 if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing all runs\n");
328 //
329 } else {
330 //
331 // we are reprocessing a single run, we must copy to the new tree the events in the file which preceed the first event of the run
332 //
333 reprocall = false;
334 //
335 if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing run number %u \n",run);
336 //
337 // copying old tree to a new file
338 //
339 tempfile = new TFile(tempname.str().c_str(),"RECREATE");
340 tempOrbitalInfo = OrbitalInfotrclone->CloneTree(-1,"fast");
341 tempOrbitalInfo->SetName("OrbitalInfo-old");
342 tempfile->Write();
343 tempfile->Close();
344 }
345 //
346 // Delete the old tree from old file and memory
347 //
348 OrbitalInfotrclone->Delete("all");
349 //
350 if (verbose) printf(" ...done!\n");
351 //
352 };
353 //
354 // create mydetector tree mydect
355 //
356 file->cd();
357 OrbitalInfotr = new TTree("OrbitalInfo-new","PAMELA OrbitalInfo data");
358 OrbitalInfotr->SetAutoSave(900000000000000LL);
359 OrbitalInfotr->Branch("OrbitalInfo","OrbitalInfo",&orbitalinfo);
360 //
361 if ( reproc && !reprocall ){
362 //
363 // open new file and retrieve also tree informations
364 //
365 tempfile = new TFile(tempname.str().c_str(),"READ");
366 OrbitalInfotrclone = (TTree*)tempfile->Get("OrbitalInfo-old");
367 OrbitalInfotrclone->SetAutoSave(900000000000000LL);
368 OrbitalInfotrclone->SetBranchAddress("OrbitalInfo",&orbitalinfoclone);
369 //
370 if ( nobefrun > 0 ){
371 if (verbose){
372 printf("\n Pre-processing: copying events from the old tree before the processed run\n");
373 printf(" Copying %u events in the file which are before the beginning of the run %u \n",nobefrun,run);
374 printf(" Start copying at event number 0, end copying at event number %u \n",nobefrun);
375 }
376 for (UInt_t j = 0; j < nobefrun; j++){
377 //
378 OrbitalInfotrclone->GetEntry(j);
379 //
380 // copy orbitalinfoclone to mydec
381 //
382 orbitalinfo->Clear();
383 //
384 memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone));
385 //
386 // Fill entry in the new tree
387 //
388 OrbitalInfotr->Fill();
389 //
390 };
391 if (verbose) printf(" Finished successful copying!\n");
392 };
393 };
394 //
395 // Get the list of run to be processed, if only one run has to be processed the list will contain one entry only.
396 //
397 runlist = runinfo->GetRunList();
398 //
399 // Loop over the run to be processed
400 //
401
402 for (UInt_t irun=0; irun < numbofrun; irun++){
403 //
404 // retrieve the first run ID to be processed using the RunInfo list
405 //
406
407 idRun = runlist->At(irun);
408 if (verbose){
409 printf("\n\n\n ####################################################################### \n");
410 printf(" PROCESSING RUN NUMBER %i \n",(int)idRun);
411 printf(" ####################################################################### \n\n\n");
412 }
413 //
414 runinfo->ID_ROOT_L0 = 0;
415 //
416 // store in the runinfo class the GL_RUN variables for our run
417 //
418 sgnl = 0;
419 sgnl = runinfo->GetRunInfo(idRun);
420 if ( sgnl ){
421 if ( debug ) printf("\n OrbitalInfo - ERROR: RunInfo exited with non-zero status\n");
422 code = sgnl;
423 goto closeandexit;
424 } else {
425 sgnl = 0;
426 };
427 //
428 // now you can access that variables using the RunInfo class this way runinfo->ID_REG_RUN
429 //
430 if ( runinfo->ID_ROOT_L0 == 0 ){
431 if ( debug ) printf("\n OrbitalInfo - ERROR: no run with ID_RUN = %u \n\n Exiting... \n\n",idRun);
432 code = -5;
433 goto closeandexit;
434 };
435 //
436 // prepare the timesync for the db
437 //
438 dbtime = new GL_TIMESYNC(runinfo->ID_ROOT_L0,"ID",dbc);
439
440 //
441 // Search in the DB the path and name of the LEVEL0 file to be processed.
442 //
443 glroot->Query_GL_ROOT(runinfo->ID_ROOT_L0,dbc);
444 //
445 ftmpname.str("");
446 ftmpname << glroot->PATH.Data() << "/";
447 ftmpname << glroot->NAME.Data();
448 fname = ftmpname.str().c_str();
449 ftmpname.str("");
450 //
451 // print out informations
452 //
453 totevent = runinfo->NEVENTS;
454 //cout<<"totevents = "<<totevent<<"\n";
455 if (verbose){
456 printf("\n LEVEL0 data file: %s \n",fname.Data());
457 printf(" RUN HEADER absolute time is: %u \n",runinfo->RUNHEADER_TIME);
458 printf(" RUN TRAILER absolute time is: %u \n",runinfo->RUNTRAILER_TIME);
459 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);
460 }//
461 // Open Level0 file
462 l0File = new TFile(fname.Data());
463 if ( !l0File ) {
464 if ( debug ) printf(" OrbitalInfo - ERROR: problems opening Level0 file\n");
465 code = -6;
466 goto closeandexit;
467 };
468 l0tr = (TTree*)l0File->Get("Physics");
469 if ( !l0tr ) {
470 if ( debug ) printf(" OrbitalInfo - ERROR: no Physics tree in Level0 file\n");
471 l0File->Close();
472 code = -7;
473 goto closeandexit;
474 };
475 // EM: open header branch as well
476 l0head = l0tr->GetBranch("Header");
477 if ( !l0head ) {
478 if ( debug ) printf(" OrbitalInfo - ERROR: no Header branch in Level0 tree\n");
479 l0File->Close();
480 code = -8;
481 goto closeandexit;
482 };
483 l0tr->SetBranchAddress("Header", &eh);
484 // end EM
485 nevents = l0head->GetEntries();
486 //
487 if ( nevents < 1 ) {
488 if ( debug ) printf(" OrbitalInfo - ERROR: Level0 file is empty\n\n");
489 l0File->Close();
490 code = -11;
491 goto closeandexit;
492 };
493 //
494 if ( runinfo->EV_TO > nevents-1 ) {
495 if ( debug ) printf(" OrbitalInfo - ERROR: too few entries in the registry tree\n");
496 l0File->Close();
497 code = -12;
498 goto closeandexit;
499 };
500 //
501 // TTree *tp = (TTree*)l0File->Get("RunHeader");
502 // tp->SetBranchAddress("Header", &eH);
503 // tp->SetBranchAddress("RunHeader", &reh);
504 // tp->GetEntry(0);
505 // ph = eH->GetPscuHeader();
506 // ULong_t TimeSync = reh->LAST_TIME_SYNC_INFO;
507 // ULong_t ObtSync = reh->OBT_TIME_SYNC;
508 // if ( debug ) printf(" 1 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",TimeSync,ObtSync,TimeSync-ObtSync);
509 //
510 ULong_t TimeSync = (ULong_t)dbtime->GetTimesync();
511 ULong_t ObtSync = (ULong_t)(dbtime->GetObt0()/1000);
512 ULong_t DeltaOBT = TimeSync - ObtSync;
513
514 if ( debug ) printf(" 2 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",(ULong_t)(dbtime->GetTimesync()/1000),(ULong_t)dbtime->GetObt0(),TimeSync-ObtSync);
515
516 l0trm = (TTree*)l0File->Get("Mcmd");
517 neventsm = l0trm->GetEntries();
518 // neventsm = 0;
519 //
520 if (neventsm == 0){
521 if ( debug ) printf("InclinationInfo - WARNING: No quaternions in this File");
522 // l0File->Close();
523 code = 900;
524 // goto closeandexit;
525 }
526 //
527
528 l0trm->SetBranchAddress("Mcmd", &mcmdev);
529 // l0trm->SetBranchAddress("Header", &eh);
530 //
531 //
532 //
533 UInt_t mctren = 0;
534 UInt_t mcreen = 0;
535 UInt_t numrec = 0;
536 //
537 Double_t upperqtime = 0;
538 Double_t lowerqtime = 0;
539
540 Double_t incli = 0;
541 oi = 0;
542 UInt_t ooi = 0;
543 //
544 // init quaternions sync
545 //
546 Bool_t isf = true;
547 Int_t fgh = 0;
548 //
549 // run over all the events of the run
550 //
551 if (verbose) printf("\n Ready to start! \n\n Processed events: \n\n");
552 //
553 for ( re = runinfo->EV_FROM; re < (runinfo->EV_FROM+runinfo->NEVENTS); re++){
554
555 //
556 if ( procev%1000 == 0 && procev > 0 && verbose ) printf(" %iK \n",procev/1000);
557 if ( debug ) printf(" %i \n",procev);
558 //
559 l0head->GetEntry(re);
560 //
561 // absolute time of this event
562 //
563 ph = eh->GetPscuHeader();
564 atime = dbtime->DBabsTime(ph->GetOrbitalTime());
565 //
566 // paranoid check
567 //
568 if ( (atime > runinfo->RUNTRAILER_TIME) || (atime < runinfo->RUNHEADER_TIME) ) {
569 if (verbose) printf(" OrbitalInfo - WARNING: event at time outside the run time window, skipping it\n");
570 // debug = true;
571 continue;
572 }
573 //
574 procev++;
575 //
576 // start processing
577 //
578 orbitalinfo->Clear();
579 //
580 // Fill OBT, pkt_num and absTime
581 //
582 // ph = eh->GetPscuHeader();
583 orbitalinfo->pkt_num = ph->GetCounter();
584 orbitalinfo->OBT = ph->GetOrbitalTime();
585 orbitalinfo->absTime = atime;
586 //
587 // Propagate the orbit from the tle time to atime, using SGP(D)4.
588 //
589 cCoordGeo coo;
590 float jyear=0;
591 //
592 if(atime >= gltle->GetToTime()) {
593 if ( !gltle->Query(atime, dbc) ){
594 //
595 // Compute the magnetic dipole moment.
596 //
597 UInt_t year, month, day, hour, min, sec;
598 //
599 TTimeStamp t = TTimeStamp(atime, kTRUE);
600 t.GetDate(kTRUE, 0, &year, &month, &day);
601 t.GetTime(kTRUE, 0, &hour, &min, &sec);
602 jyear = (float) year
603 + (month*31.+ (float) day)/365.
604 + (hour*3600.+min*60.+(float)sec)/(24*3600*365.);
605 //
606 feldcof_(&jyear, &dimo); // get dipole moment for year
607 } else {
608 code = -56;
609 goto closeandexit;
610 };
611 }
612 coo = getCoo(atime, gltle->GetFromTime(), gltle->GetTle());
613 //
614 cOrbit orbits(*gltle->GetTle());
615 //
616 if ( debug ) printf(" I am Here \n");
617 //
618 // synchronize with quaternions data
619 //
620 if ( isf && neventsm>0 ){
621 if ( debug ) printf(" I am here \n");
622 //
623 // First event
624 //
625 isf = false;
626 upperqtime = atime;
627 lowerqtime = runinfo->RUNHEADER_TIME;
628 for ( ik = 0; ik < neventsm; ik++){
629 l0trm->GetEntry(ik);
630 tmpSize = mcmdev->Records->GetEntries();
631 numrec = tmpSize;
632 for (Int_t j3 = 0;j3<tmpSize;j3++){
633 mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(j3);
634 if ((int)mcmdrc->ID1 == 226){
635 L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
636 for (UInt_t ui = 0; ui < 6; ui++){
637 if (ui>0){
638 if (L_QQ_Q_l_upper->time[ui]>L_QQ_Q_l_upper->time[0]){
639 if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000))<atime){
640 upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));
641 orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
642 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]);
643 }else {
644 lowerqtime = upperqtime;
645 upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000));
646 orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
647 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]);
648 mcreen = j3;
649 mctren = ik;
650 if(fgh==0){
651 CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
652 CopyAng(RYPang_lower,RYPang_upper);
653 }
654 oi=ui;
655 goto closethisloop;
656 }
657 fgh++;
658 CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
659 CopyAng(RYPang_lower,RYPang_upper);
660 }
661 }else{
662 if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))<atime){
663 upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
664 orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
665 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]);
666 }
667 else {
668 lowerqtime = upperqtime;
669 upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
670 orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
671 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]);
672 mcreen = j3;
673 mctren = ik;
674 if(fgh==0){
675 CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
676 CopyAng(RYPang_lower,RYPang_upper);
677 lowerqtime = atime-1;
678 }
679 oi=ui;
680 goto closethisloop;
681 //_0 = true;
682 }
683 fgh++;
684 CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
685 CopyAng(RYPang_lower,RYPang_upper);
686 //_0 = true;
687 };
688 //cin>>grib;
689 };
690 };
691 };
692 };
693 };
694 closethisloop:
695 //
696 if ( debug ) printf(" I am There \n");
697 //
698 if (((atime>(UInt_t)upperqtime)||(atime<(UInt_t)lowerqtime)) && neventsm>0 ){
699 if ( debug ) printf(" I am there \n");
700 //
701 lowerqtime = upperqtime;
702 UInt_t maxloop = 100000000;
703 UInt_t mn = 0;
704 bool gh=false;
705 ooi=oi;
706 if ( verbose ) printf(" OrbitalInfoCore: sync with quaternions data upperqtime %u lowerqtime %u atime %u \n",(UInt_t)upperqtime,(UInt_t)lowerqtime,atime);
707 while (!gh){
708 if ( mn > maxloop ){
709 if ( verbose ) printf(" OrbitalInfoCore: quaternions sync out of range! exiting\n");
710 gh = true;
711 };
712 mn++;
713 if (oi<5) oi++;
714 else oi=0;
715 if (oi==0){
716 mcreen++;
717 if (mcreen == numrec){
718 mctren++;
719 mcreen = 0;
720 l0trm->GetEntry(mctren);
721 numrec = mcmdev->Records->GetEntries();
722 }
723 CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper);
724 CopyAng(RYPang_lower,RYPang_upper);
725 mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(mcreen);
726 if ((int)mcmdrc->ID1 == 226){
727 L_QQ_Q_l_upper->fill(mcmdrc->McmdData);
728 upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
729 if (upperqtime<lowerqtime){
730 upperqtime=runinfo->RUNTRAILER_TIME;
731 CopyQ(L_QQ_Q_l_upper,L_QQ_Q_l_lower);
732 CopyAng(RYPang_upper,RYPang_lower);
733 }else{
734 orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
735 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]);
736 }
737 // re--;
738 gh=true;
739 }
740 }else{
741 if ((Int_t)L_QQ_Q_l_upper->time[oi]>(Int_t)L_QQ_Q_l_upper->time[0]){
742 upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
743 orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi);
744 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]);
745 orbits.getPosition((double) (lowerqtime - gltle->GetFromTime())/60., &eCi);
746 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]);
747 // re--;
748 gh=true;
749 };
750 };
751 };
752 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);
753 };
754 //
755 if ( debug ) printf(" I am THIS \n");
756 //
757 // Fill in quaternions and angles
758 //
759 if ((atime<=(UInt_t)upperqtime)&&(atime>=(UInt_t)lowerqtime)&& neventsm>0){
760 if ( debug ) printf(" I am this \n");
761 UInt_t tut = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi);
762 if (oi == 0){
763 if ((tut!=5)||(tut!=6)){
764 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)));
765 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));
766 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)));
767 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));
768 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)));
769 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));
770 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)));
771 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));
772
773 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)));
774 orbitalinfo->theta = incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
775 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)));
776 orbitalinfo->phi = incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
777 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)));
778 orbitalinfo->etha = incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
779 }
780 if (tut==6){
781 if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){
782 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)));
783 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));
784 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)));
785 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));
786 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)));
787 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));
788 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)));
789 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));
790
791 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)));
792 orbitalinfo->theta = incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
793 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)));
794 orbitalinfo->phi = incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
795 //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";
796 //cin>>grib;
797 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)));
798 orbitalinfo->etha = incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000));
799 }
800 }
801 } else {
802 if((tut!=6)||(tut!=7)||(tut!=9)){
803 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)));
804 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));
805 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)));
806 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));
807 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)));
808 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));
809 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)));
810 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));
811
812 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)));
813 orbitalinfo->theta = incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
814 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)));
815 orbitalinfo->phi = incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
816 //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";
817 //cin>>grib;
818 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)));
819 orbitalinfo->etha = incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
820 }
821 if (tut==6){
822 if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){
823 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)));
824 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));
825 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)));
826 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));
827 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)));
828 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));
829 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)));
830 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));
831
832 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)));
833 orbitalinfo->theta = incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
834 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)));
835 orbitalinfo->phi = incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
836 //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";
837 //cin>>grib;
838 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)));
839 orbitalinfo->etha = incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000));
840 }
841 }
842 }
843 //
844 orbitalinfo->mode = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi);
845 //
846 } else {
847 if ( debug ) printf(" ops no incl! \n");
848 orbitalinfo->mode = -1;
849 };
850
851 //
852 // fill orbital positions
853 //
854 // Build coordinates in the right range. We want to convert,
855 // longitude from (0, 2*pi) to (-180deg, 180deg). Altitude is
856 // in meters.
857 lon = (coo.m_Lon > M_PI) ? rad2deg(coo.m_Lon - 2*M_PI) : rad2deg(coo.m_Lon);
858 lat = rad2deg(coo.m_Lat);
859 alt = coo.m_Alt;
860 //
861 if( lon<180 && lon>-180 && lat<90 && lat>-90 && alt>0 ){
862 //
863 orbitalinfo->lon = lon;
864 orbitalinfo->lat = lat;
865 orbitalinfo->alt = alt ;
866 //
867 // compute mag field components and L shell.
868 //
869 feldg_(&lat, &lon, &alt, &bnorth, &beast, &bdown, &babs);
870 shellg_(&lat, &lon, &alt, &dimo, &xl, &icode, &bab1);
871 findb0_(&stps, &bdel, &value, &bequ, &rr0);
872 //
873 orbitalinfo->Bnorth = bnorth;
874 orbitalinfo->Beast = beast;
875 orbitalinfo->Bdown = bdown;
876 orbitalinfo->Babs = babs;
877 orbitalinfo->BB0 = babs/bequ;
878 orbitalinfo->L = xl;
879 // Set Stormer vertical cutoff using L shell.
880 orbitalinfo->cutoff[0] = 14.9/(xl*xl);
881 //
882 };
883 //
884 // Fill the class
885 //
886 OrbitalInfotr->Fill();
887 //
888 }; // loop over the events in the run
889 //
890 // Here you may want to clear some variables before processing another run
891 //
892 delete dbtime;
893 if ( L_QQ_Q_l_upper ) delete L_QQ_Q_l_upper;
894 if ( L_QQ_Q_l_lower ) delete L_QQ_Q_l_lower;
895 if ( RYPang_upper ) delete RYPang_upper;
896 if ( RYPang_lower ) delete RYPang_lower;
897 }; // process all the runs
898
899 if (verbose) printf("\n Finished processing data \n");
900 //
901 closeandexit:
902 //
903 // we have finished processing the run(s). If we processed a single run now we must copy all the events after our run from the old tree to the new one and delete the old tree.
904 //
905 if ( !reprocall && reproc && code >= 0 ){
906 if ( totfileentries > noaftrun ){
907 if (verbose){
908 printf("\n Post-processing: copying events from the old tree after the processed run\n");
909 printf(" Copying %i events in the file which are after the end of the run %i \n",(int)(totfileentries-noaftrun),(int)run);
910 printf(" Start copying at event number %i end copying at event number %i \n",(int)noaftrun,(int)totfileentries);
911 }
912 for (UInt_t j = noaftrun; j < totfileentries; j++ ){
913 //
914 // Get entry from old tree
915 //
916 OrbitalInfotrclone->GetEntry(j);
917 //
918 // copy orbitalinfoclone to OrbitalInfo
919 //
920 orbitalinfo->Clear();
921 //
922 memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone));
923 //
924 // Fill entry in the new tree
925 //
926 OrbitalInfotr->Fill();
927 };
928 if (verbose) printf(" Finished successful copying!\n");
929 };
930 };
931 //
932 // Close files, delete old tree(s), write and close level2 file
933 //
934 if ( l0File ) l0File->Close();
935 if ( tempfile ) tempfile->Close();
936 gSystem->Unlink(tempname.str().c_str());
937 //
938 if ( runinfo ) runinfo->Close();
939 if ( OrbitalInfotr ) OrbitalInfotr->SetName("OrbitalInfo");
940 if ( file ){
941 file->cd();
942 file->Write();
943 };
944 //
945 gSystem->Unlink(OrbitalInfofolder.str().c_str());
946 //
947 // the end
948 //
949 if (verbose) printf("\n Exiting...\n");
950 if(OrbitalInfotr)OrbitalInfotr->Delete();
951 //
952 if ( orbitalinfo ) delete orbitalinfo;
953 if ( orbitalinfoclone ) delete orbitalinfoclone;
954 if ( glroot ) delete glroot;
955 if ( runinfo ) delete runinfo;
956 //
957 if(code < 0) throw code;
958 return(code);
959 }
960
961
962 //
963 // Returns the cCoordGeo structure holding the geographical
964 // coordinates for the event (see sgp4.h).
965 //
966 // atime is the abstime of the event in UTC unix time.
967 // tletime is the time of the tle in UTC unix time.
968 // tle is the previous and nearest tle (compared to atime).
969 cCoordGeo getCoo(UInt_t atime, UInt_t tletime, cTle *tle)
970 {
971 cEci eci;
972 cOrbit orbit(*tle);
973 orbit.getPosition((double) (atime - tletime)/60., &eci);
974
975 return eci.toGeo();
976 }
977
978 // function of copyng of quatrnions classes
979
980 void CopyQ(Quaternions *Q1, Quaternions *Q2){
981 for(UInt_t i = 0; i < 6; i++){
982 Q1->time[i]=Q2->time[i];
983 for (UInt_t j = 0; j < 4; j++)Q1->quat[i][j]=Q2->quat[i][j];
984 }
985 return;
986 }
987
988 // functions of copyng InclinationInfo classes
989
990 void CopyAng(InclinationInfo *A1, InclinationInfo *A2){
991 A1->Tangazh = A2->Tangazh;
992 A1->Ryskanie = A2->Ryskanie;
993 A1->Kren = A2->Kren;
994 return;
995 }
996
997 UInt_t holeq(Double_t lower,Double_t upper,Quaternions *Qlower, Quaternions *Qupper, UInt_t f){
998
999 UInt_t hole = 10;
1000 bool R10l = false; // Sign of R10 mode in lower quaternions array
1001 bool R10u = false; // Sign of R10 mode in upper quaternions array
1002 bool insm = false; // Sign that we inside quaternions array
1003 bool mxtml = false; // Sign of mixt mode in lower quaternions array
1004 bool mxtmu = false; // Sign of mixt mode in upper quaternions array
1005 bool npasm = false; // Sign of normall pass between R10 and non R10 or between non R10 and R10
1006 UInt_t NCQl = 6; // Number of correct quaternions in lower array
1007 UInt_t NCQu = 6; // Number of correct quaternions in upper array
1008 if (f>0){
1009 insm = true;
1010 if(Qupper->time[f]-Qupper->time[f-1]==30) R10u = false;
1011 if(Qupper->time[f]-Qupper->time[f-1]<1) R10u = true;
1012 }else{
1013 insm = false;
1014 if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]<2)) R10l = true;
1015 if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]<2)) R10u = true;
1016 if((Qlower->time[5]-Qlower->time[0]==150)&&(Qlower->time[1]-Qlower->time[0]==30)) R10l = false;
1017 if((Qupper->time[5]-Qupper->time[0]==150)&&(Qupper->time[1]-Qupper->time[0]==30)) R10u = false;
1018 if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]==30)){
1019 mxtml = true;
1020 for(UInt_t i = 1; i < 6; i++){
1021 if(Qlower->time[i]-Qlower->time[0]==30*i) NCQl=i;
1022 }
1023 }
1024 if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]==30)){
1025 mxtmu = true;
1026 for(UInt_t i = 1; i < 6; i++){
1027 if(Qupper->time[i]-Qupper->time[0]==30*i) NCQu=i;
1028 }
1029 }
1030 }
1031
1032 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;
1033
1034
1035 if (R10u&&insm) hole=0; // best event R10
1036 if ((upper-lower<=5)&&(!insm)&&R10l&&R10u) hole = 1; // when first of 6 quaternions in array is correct
1037 if (((!R10u)&&insm)||((!insm)&&(!R10u)&&(!R10l)&&((upper-lower==210+(6-NCQl)*30)||(upper-lower==30)))) hole = 2; //non R10
1038 if (npasm&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 3; //normall pass from R10 to non R10 or from non R10 to R10
1039 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
1040 if ((upper-lower>=300)&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 5; //uneliminable hole between R10 and non R10 or between non R10 and R10
1041 if ((upper-lower>5)&&(upper-lower<=300)&&R10u&&R10l) hole = 6; // eliminable hole inside R10
1042 if ((upper-lower>300)&&R10u&&R10l) hole = 7; //uneliminable hole inside R10
1043 if ((upper-lower>210)&&(upper-lower<=1200)&&(!R10u)&&(!R10l)) hole = 8; //eliminable hole inside non R10
1044 if ((upper-lower>1200)&&!R10u&&!R10l) hole = 9; // uneliminable hole inside non R10
1045 return hole;
1046 }
1047

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