| 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 = "OrbitalInfoFolder_"+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(),<p2,(char *)(glparam2->PATH+glparam2->NAME).Data(),<p3); |
| 236 |
|
| 237 |
// |
| 238 |
// End IGRF stuff// |
| 239 |
// |
| 240 |
|
| 241 |
// |
| 242 |
// Let's start! |
| 243 |
// |
| 244 |
// 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 |
| 245 |
// if run != 0 we must process only that run but first we have to check if the tree MyDetector2 already exist in the file |
| 246 |
// if it exists we are reprocessing data and we must delete that entries, if not we must create it. |
| 247 |
// |
| 248 |
if ( run == 0 ) reproc = true; |
| 249 |
// |
| 250 |
// |
| 251 |
// Output file is "outputfile" |
| 252 |
// |
| 253 |
if ( !file->IsOpen() ){ |
| 254 |
//printf(" OrbitalInfo - ERROR: cannot open file for writing\n"); |
| 255 |
throw -901; |
| 256 |
}; |
| 257 |
// |
| 258 |
// Retrieve GL_RUN variables from the level2 file |
| 259 |
// |
| 260 |
OrbitalInfoversion = OrbitalInfoInfo(false); // we should decide how to handle versioning system |
| 261 |
// |
| 262 |
// create an interface to RunInfo called "runinfo" |
| 263 |
// |
| 264 |
runinfo = new ItoRunInfo(file); |
| 265 |
// |
| 266 |
// open "Run" tree in level2 file, if not existing return an error (sngl != 0) |
| 267 |
// |
| 268 |
sgnl = 0; |
| 269 |
sgnl = runinfo->Update(run, "ORB", OrbitalInfoversion); |
| 270 |
//sgnl = runinfo->Read(run); |
| 271 |
|
| 272 |
if ( sgnl ){ |
| 273 |
//printf("OrbitalInfo - ERROR: RunInfo exited with non-zero status\n"); |
| 274 |
code = sgnl; |
| 275 |
goto closeandexit; |
| 276 |
} else { |
| 277 |
sgnl = 0; |
| 278 |
}; |
| 279 |
// |
| 280 |
// number of events in the file BEFORE the first event of our run |
| 281 |
// |
| 282 |
nobefrun = runinfo->GetFirstEntry(); |
| 283 |
// |
| 284 |
// total number of events in the file |
| 285 |
// |
| 286 |
totfileentries = runinfo->GetFileEntries(); |
| 287 |
// |
| 288 |
// first file entry AFTER the last event of our run |
| 289 |
// |
| 290 |
noaftrun = runinfo->GetLastEntry() + 1; |
| 291 |
// |
| 292 |
// number of run to be processed |
| 293 |
// |
| 294 |
numbofrun = runinfo->GetNoRun(); |
| 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 |
| 297 |
// |
| 298 |
OrbitalInfotrclone = (TTree*)file->Get("OrbitalInfo"); |
| 299 |
// |
| 300 |
if ( !OrbitalInfotrclone ){ |
| 301 |
// |
| 302 |
// tree does not exist, we are not reprocessing |
| 303 |
// |
| 304 |
reproc = false; |
| 305 |
if ( run == 0 ){ |
| 306 |
if (verbose) printf(" OrbitalInfo - WARNING: you are reprocessing data but OrbitalInfo tree does not exist!\n"); |
| 307 |
} |
| 308 |
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"); |
| 310 |
} |
| 311 |
} else { |
| 312 |
// |
| 313 |
// tree exists, we are reprocessing data. Are we reprocessing a single run or all the file? |
| 314 |
// |
| 315 |
OrbitalInfotrclone->SetAutoSave(900000000000000LL); |
| 316 |
reproc = true; |
| 317 |
// |
| 318 |
// |
| 319 |
if (verbose) printf("\n Preparing the pre-processing...\n"); |
| 320 |
// |
| 321 |
if ( run == 0 ){ |
| 322 |
// |
| 323 |
// 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 |
| 325 |
// |
| 326 |
reprocall = true; |
| 327 |
// |
| 328 |
if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing all runs\n"); |
| 329 |
// |
| 330 |
} else { |
| 331 |
// |
| 332 |
// 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 |
| 333 |
// |
| 334 |
reprocall = false; |
| 335 |
// |
| 336 |
if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing run number %u \n",run); |
| 337 |
// |
| 338 |
// copying old tree to a new file |
| 339 |
// |
| 340 |
tempfile = new TFile(tempname.str().c_str(),"RECREATE"); |
| 341 |
tempOrbitalInfo = OrbitalInfotrclone->CloneTree(-1,"fast"); |
| 342 |
tempOrbitalInfo->SetName("OrbitalInfo-old"); |
| 343 |
tempfile->Write(); |
| 344 |
tempfile->Close(); |
| 345 |
} |
| 346 |
// |
| 347 |
// Delete the old tree from old file and memory |
| 348 |
// |
| 349 |
OrbitalInfotrclone->Delete("all"); |
| 350 |
// |
| 351 |
if (verbose) printf(" ...done!\n"); |
| 352 |
// |
| 353 |
}; |
| 354 |
// |
| 355 |
// create mydetector tree mydect |
| 356 |
// |
| 357 |
file->cd(); |
| 358 |
OrbitalInfotr = new TTree("OrbitalInfo-new","PAMELA OrbitalInfo data"); |
| 359 |
OrbitalInfotr->SetAutoSave(900000000000000LL); |
| 360 |
OrbitalInfotr->Branch("OrbitalInfo","OrbitalInfo",&orbitalinfo); |
| 361 |
// |
| 362 |
if ( reproc && !reprocall ){ |
| 363 |
// |
| 364 |
// open new file and retrieve also tree informations |
| 365 |
// |
| 366 |
tempfile = new TFile(tempname.str().c_str(),"READ"); |
| 367 |
OrbitalInfotrclone = (TTree*)tempfile->Get("OrbitalInfo-old"); |
| 368 |
OrbitalInfotrclone->SetAutoSave(900000000000000LL); |
| 369 |
OrbitalInfotrclone->SetBranchAddress("OrbitalInfo",&orbitalinfoclone); |
| 370 |
// |
| 371 |
if ( nobefrun > 0 ){ |
| 372 |
if (verbose){ |
| 373 |
printf("\n Pre-processing: copying events from the old tree before the processed run\n"); |
| 374 |
printf(" Copying %u events in the file which are before the beginning of the run %u \n",nobefrun,run); |
| 375 |
printf(" Start copying at event number 0, end copying at event number %u \n",nobefrun); |
| 376 |
} |
| 377 |
for (UInt_t j = 0; j < nobefrun; j++){ |
| 378 |
// |
| 379 |
OrbitalInfotrclone->GetEntry(j); |
| 380 |
// |
| 381 |
// copy orbitalinfoclone to mydec |
| 382 |
// |
| 383 |
orbitalinfo->Clear(); |
| 384 |
// |
| 385 |
memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone)); |
| 386 |
// |
| 387 |
// Fill entry in the new tree |
| 388 |
// |
| 389 |
OrbitalInfotr->Fill(); |
| 390 |
// |
| 391 |
}; |
| 392 |
if (verbose) printf(" Finished successful copying!\n"); |
| 393 |
}; |
| 394 |
}; |
| 395 |
// |
| 396 |
// Get the list of run to be processed, if only one run has to be processed the list will contain one entry only. |
| 397 |
// |
| 398 |
runlist = runinfo->GetRunList(); |
| 399 |
// |
| 400 |
// Loop over the run to be processed |
| 401 |
// |
| 402 |
|
| 403 |
for (UInt_t irun=0; irun < numbofrun; irun++){ |
| 404 |
// |
| 405 |
// retrieve the first run ID to be processed using the RunInfo list |
| 406 |
// |
| 407 |
|
| 408 |
idRun = runlist->At(irun); |
| 409 |
if (verbose){ |
| 410 |
printf("\n\n\n ####################################################################### \n"); |
| 411 |
printf(" PROCESSING RUN NUMBER %i \n",(int)idRun); |
| 412 |
printf(" ####################################################################### \n\n\n"); |
| 413 |
} |
| 414 |
// |
| 415 |
runinfo->ID_ROOT_L0 = 0; |
| 416 |
// |
| 417 |
// store in the runinfo class the GL_RUN variables for our run |
| 418 |
// |
| 419 |
sgnl = 0; |
| 420 |
sgnl = runinfo->GetRunInfo(idRun); |
| 421 |
if ( sgnl ){ |
| 422 |
if ( debug ) printf("\n OrbitalInfo - ERROR: RunInfo exited with non-zero status\n"); |
| 423 |
code = sgnl; |
| 424 |
goto closeandexit; |
| 425 |
} else { |
| 426 |
sgnl = 0; |
| 427 |
}; |
| 428 |
// |
| 429 |
// now you can access that variables using the RunInfo class this way runinfo->ID_REG_RUN |
| 430 |
// |
| 431 |
if ( runinfo->ID_ROOT_L0 == 0 ){ |
| 432 |
if ( debug ) printf("\n OrbitalInfo - ERROR: no run with ID_RUN = %u \n\n Exiting... \n\n",idRun); |
| 433 |
code = -5; |
| 434 |
goto closeandexit; |
| 435 |
}; |
| 436 |
// |
| 437 |
// prepare the timesync for the db |
| 438 |
// |
| 439 |
dbtime = new GL_TIMESYNC(runinfo->ID_ROOT_L0,"ID",dbc); |
| 440 |
|
| 441 |
// |
| 442 |
// Search in the DB the path and name of the LEVEL0 file to be processed. |
| 443 |
// |
| 444 |
glroot->Query_GL_ROOT(runinfo->ID_ROOT_L0,dbc); |
| 445 |
// |
| 446 |
ftmpname.str(""); |
| 447 |
ftmpname << glroot->PATH.Data() << "/"; |
| 448 |
ftmpname << glroot->NAME.Data(); |
| 449 |
fname = ftmpname.str().c_str(); |
| 450 |
ftmpname.str(""); |
| 451 |
// |
| 452 |
// print out informations |
| 453 |
// |
| 454 |
totevent = runinfo->NEVENTS; |
| 455 |
//cout<<"totevents = "<<totevent<<"\n"; |
| 456 |
if (verbose){ |
| 457 |
printf("\n LEVEL0 data file: %s \n",fname.Data()); |
| 458 |
printf(" RUN HEADER absolute time is: %u \n",runinfo->RUNHEADER_TIME); |
| 459 |
printf(" RUN TRAILER absolute time is: %u \n",runinfo->RUNTRAILER_TIME); |
| 460 |
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); |
| 461 |
}// |
| 462 |
// Open Level0 file |
| 463 |
l0File = new TFile(fname.Data()); |
| 464 |
if ( !l0File ) { |
| 465 |
if ( debug ) printf(" OrbitalInfo - ERROR: problems opening Level0 file\n"); |
| 466 |
code = -6; |
| 467 |
goto closeandexit; |
| 468 |
}; |
| 469 |
l0tr = (TTree*)l0File->Get("Physics"); |
| 470 |
if ( !l0tr ) { |
| 471 |
if ( debug ) printf(" OrbitalInfo - ERROR: no Physics tree in Level0 file\n"); |
| 472 |
l0File->Close(); |
| 473 |
code = -7; |
| 474 |
goto closeandexit; |
| 475 |
}; |
| 476 |
// EM: open header branch as well |
| 477 |
l0head = l0tr->GetBranch("Header"); |
| 478 |
if ( !l0head ) { |
| 479 |
if ( debug ) printf(" OrbitalInfo - ERROR: no Header branch in Level0 tree\n"); |
| 480 |
l0File->Close(); |
| 481 |
code = -8; |
| 482 |
goto closeandexit; |
| 483 |
}; |
| 484 |
l0tr->SetBranchAddress("Header", &eh); |
| 485 |
// end EM |
| 486 |
nevents = l0head->GetEntries(); |
| 487 |
// |
| 488 |
if ( nevents < 1 ) { |
| 489 |
if ( debug ) printf(" OrbitalInfo - ERROR: Level0 file is empty\n\n"); |
| 490 |
l0File->Close(); |
| 491 |
code = -11; |
| 492 |
goto closeandexit; |
| 493 |
}; |
| 494 |
// |
| 495 |
if ( runinfo->EV_TO > nevents-1 ) { |
| 496 |
if ( debug ) printf(" OrbitalInfo - ERROR: too few entries in the registry tree\n"); |
| 497 |
l0File->Close(); |
| 498 |
code = -12; |
| 499 |
goto closeandexit; |
| 500 |
}; |
| 501 |
// |
| 502 |
// TTree *tp = (TTree*)l0File->Get("RunHeader"); |
| 503 |
// tp->SetBranchAddress("Header", &eH); |
| 504 |
// tp->SetBranchAddress("RunHeader", &reh); |
| 505 |
// tp->GetEntry(0); |
| 506 |
// ph = eH->GetPscuHeader(); |
| 507 |
// ULong_t TimeSync = reh->LAST_TIME_SYNC_INFO; |
| 508 |
// ULong_t ObtSync = reh->OBT_TIME_SYNC; |
| 509 |
// if ( debug ) printf(" 1 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",TimeSync,ObtSync,TimeSync-ObtSync); |
| 510 |
// |
| 511 |
ULong_t TimeSync = (ULong_t)dbtime->GetTimesync(); |
| 512 |
ULong_t ObtSync = (ULong_t)(dbtime->GetObt0()/1000); |
| 513 |
ULong_t DeltaOBT = TimeSync - ObtSync; |
| 514 |
|
| 515 |
if ( debug ) printf(" 2 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",(ULong_t)(dbtime->GetTimesync()/1000),(ULong_t)dbtime->GetObt0(),TimeSync-ObtSync); |
| 516 |
|
| 517 |
l0trm = (TTree*)l0File->Get("Mcmd"); |
| 518 |
neventsm = l0trm->GetEntries(); |
| 519 |
// |
| 520 |
if (neventsm == 0){ |
| 521 |
if ( debug ) printf("InclinationInfo - ERROR: No quaternions in this File"); |
| 522 |
l0File->Close(); |
| 523 |
code = -13; |
| 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 |
// synchronize with quaternions data |
| 617 |
// |
| 618 |
if ( isf ){ |
| 619 |
// |
| 620 |
// First event |
| 621 |
// |
| 622 |
isf = false; |
| 623 |
upperqtime = atime; |
| 624 |
lowerqtime = runinfo->RUNHEADER_TIME; |
| 625 |
for ( ik = 0; ik < neventsm; ik++){ |
| 626 |
l0trm->GetEntry(ik); |
| 627 |
tmpSize = mcmdev->Records->GetEntries(); |
| 628 |
numrec = tmpSize; |
| 629 |
for (Int_t j3 = 0;j3<tmpSize;j3++){ |
| 630 |
mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(j3); |
| 631 |
if ((int)mcmdrc->ID1 == 226){ |
| 632 |
L_QQ_Q_l_upper->fill(mcmdrc->McmdData); |
| 633 |
for (UInt_t ui = 0; ui < 6; ui++){ |
| 634 |
if (ui>0){ |
| 635 |
if (L_QQ_Q_l_upper->time[ui]>L_QQ_Q_l_upper->time[0]){ |
| 636 |
if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000))<atime){ |
| 637 |
upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000)); |
| 638 |
orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi); |
| 639 |
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]); |
| 640 |
}else { |
| 641 |
lowerqtime = upperqtime; |
| 642 |
upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000)); |
| 643 |
orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi); |
| 644 |
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]); |
| 645 |
mcreen = j3; |
| 646 |
mctren = ik; |
| 647 |
if(fgh==0){ |
| 648 |
CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper); |
| 649 |
CopyAng(RYPang_lower,RYPang_upper); |
| 650 |
} |
| 651 |
oi=ui; |
| 652 |
goto closethisloop; |
| 653 |
} |
| 654 |
fgh++; |
| 655 |
CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper); |
| 656 |
CopyAng(RYPang_lower,RYPang_upper); |
| 657 |
} |
| 658 |
}else{ |
| 659 |
if (dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000))<atime){ |
| 660 |
upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 661 |
orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi); |
| 662 |
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]); |
| 663 |
} |
| 664 |
else { |
| 665 |
lowerqtime = upperqtime; |
| 666 |
upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 667 |
orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi); |
| 668 |
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]); |
| 669 |
mcreen = j3; |
| 670 |
mctren = ik; |
| 671 |
if(fgh==0){ |
| 672 |
CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper); |
| 673 |
CopyAng(RYPang_lower,RYPang_upper); |
| 674 |
lowerqtime = atime-1; |
| 675 |
} |
| 676 |
oi=ui; |
| 677 |
goto closethisloop; |
| 678 |
//_0 = true; |
| 679 |
} |
| 680 |
fgh++; |
| 681 |
CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper); |
| 682 |
CopyAng(RYPang_lower,RYPang_upper); |
| 683 |
//_0 = true; |
| 684 |
}; |
| 685 |
//cin>>grib; |
| 686 |
}; |
| 687 |
}; |
| 688 |
}; |
| 689 |
}; |
| 690 |
}; |
| 691 |
closethisloop: |
| 692 |
// |
| 693 |
if ((atime>(UInt_t)upperqtime)||(atime<(UInt_t)lowerqtime)){ |
| 694 |
// |
| 695 |
lowerqtime = upperqtime; |
| 696 |
UInt_t maxloop = 100000000; |
| 697 |
UInt_t mn = 0; |
| 698 |
bool gh=false; |
| 699 |
ooi=oi; |
| 700 |
if ( verbose ) printf(" OrbitalInfoCore: sync with quaternions data upperqtime %u lowerqtime %u atime %u \n",(UInt_t)upperqtime,(UInt_t)lowerqtime,atime); |
| 701 |
while (!gh){ |
| 702 |
if ( mn > maxloop ){ |
| 703 |
if ( verbose ) printf(" OrbitalInfoCore: quaternions sync out of range! exiting\n"); |
| 704 |
gh = true; |
| 705 |
}; |
| 706 |
mn++; |
| 707 |
if (oi<5) oi++; |
| 708 |
else oi=0; |
| 709 |
if (oi==0){ |
| 710 |
mcreen++; |
| 711 |
if (mcreen == numrec){ |
| 712 |
mctren++; |
| 713 |
mcreen = 0; |
| 714 |
l0trm->GetEntry(mctren); |
| 715 |
numrec = mcmdev->Records->GetEntries(); |
| 716 |
} |
| 717 |
CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper); |
| 718 |
CopyAng(RYPang_lower,RYPang_upper); |
| 719 |
mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(mcreen); |
| 720 |
if ((int)mcmdrc->ID1 == 226){ |
| 721 |
L_QQ_Q_l_upper->fill(mcmdrc->McmdData); |
| 722 |
upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 723 |
if (upperqtime<lowerqtime){ |
| 724 |
upperqtime=runinfo->RUNTRAILER_TIME; |
| 725 |
CopyQ(L_QQ_Q_l_upper,L_QQ_Q_l_lower); |
| 726 |
CopyAng(RYPang_upper,RYPang_lower); |
| 727 |
}else{ |
| 728 |
orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi); |
| 729 |
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]); |
| 730 |
} |
| 731 |
// re--; |
| 732 |
gh=true; |
| 733 |
} |
| 734 |
}else{ |
| 735 |
if ((Int_t)L_QQ_Q_l_upper->time[oi]>(Int_t)L_QQ_Q_l_upper->time[0]){ |
| 736 |
upperqtime = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)); |
| 737 |
orbits.getPosition((double) (upperqtime - gltle->GetFromTime())/60., &eCi); |
| 738 |
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]); |
| 739 |
orbits.getPosition((double) (lowerqtime - gltle->GetFromTime())/60., &eCi); |
| 740 |
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]); |
| 741 |
// re--; |
| 742 |
gh=true; |
| 743 |
}; |
| 744 |
}; |
| 745 |
}; |
| 746 |
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); |
| 747 |
}; |
| 748 |
// |
| 749 |
// Fill in quaternions and angles |
| 750 |
// |
| 751 |
if ((atime<=(UInt_t)upperqtime)&&(atime>=(UInt_t)lowerqtime)){ |
| 752 |
UInt_t tut = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi); |
| 753 |
if (oi == 0){ |
| 754 |
if ((tut!=5)||(tut!=6)){ |
| 755 |
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))); |
| 756 |
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)); |
| 757 |
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))); |
| 758 |
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)); |
| 759 |
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))); |
| 760 |
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)); |
| 761 |
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))); |
| 762 |
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)); |
| 763 |
|
| 764 |
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))); |
| 765 |
orbitalinfo->theta = incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 766 |
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))); |
| 767 |
orbitalinfo->phi = incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 768 |
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))); |
| 769 |
orbitalinfo->etha = incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 770 |
} |
| 771 |
if (tut==6){ |
| 772 |
if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){ |
| 773 |
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))); |
| 774 |
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)); |
| 775 |
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))); |
| 776 |
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)); |
| 777 |
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))); |
| 778 |
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)); |
| 779 |
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))); |
| 780 |
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)); |
| 781 |
|
| 782 |
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))); |
| 783 |
orbitalinfo->theta = incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 784 |
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))); |
| 785 |
orbitalinfo->phi = incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 786 |
//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"; |
| 787 |
//cin>>grib; |
| 788 |
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))); |
| 789 |
orbitalinfo->etha = incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 790 |
} |
| 791 |
} |
| 792 |
} else { |
| 793 |
if((tut!=6)||(tut!=7)||(tut!=9)){ |
| 794 |
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))); |
| 795 |
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)); |
| 796 |
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))); |
| 797 |
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)); |
| 798 |
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))); |
| 799 |
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)); |
| 800 |
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))); |
| 801 |
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)); |
| 802 |
|
| 803 |
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))); |
| 804 |
orbitalinfo->theta = incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)); |
| 805 |
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))); |
| 806 |
orbitalinfo->phi = incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)); |
| 807 |
//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"; |
| 808 |
//cin>>grib; |
| 809 |
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))); |
| 810 |
orbitalinfo->etha = incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)); |
| 811 |
} |
| 812 |
if (tut==6){ |
| 813 |
if (fabs(RYPang_lower->Kren-RYPang_upper->Kren)<0.1){ |
| 814 |
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))); |
| 815 |
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)); |
| 816 |
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))); |
| 817 |
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)); |
| 818 |
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))); |
| 819 |
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)); |
| 820 |
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))); |
| 821 |
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)); |
| 822 |
|
| 823 |
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))); |
| 824 |
orbitalinfo->theta = incli*atime+RYPang_upper->Tangazh-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)); |
| 825 |
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))); |
| 826 |
orbitalinfo->phi = incli*atime+RYPang_upper->Ryskanie-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)); |
| 827 |
//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"; |
| 828 |
//cin>>grib; |
| 829 |
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))); |
| 830 |
orbitalinfo->etha = incli*atime+RYPang_upper->Kren-incli*dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[oi]*1000-DeltaOBT*1000)); |
| 831 |
} |
| 832 |
} |
| 833 |
} |
| 834 |
orbitalinfo->mode = holeq(lowerqtime, upperqtime, L_QQ_Q_l_lower, L_QQ_Q_l_upper, oi); |
| 835 |
|
| 836 |
} else { |
| 837 |
orbitalinfo->mode = -1; |
| 838 |
}; |
| 839 |
|
| 840 |
// |
| 841 |
// fill orbital positions |
| 842 |
// |
| 843 |
// Build coordinates in the right range. We want to convert, |
| 844 |
// longitude from (0, 2*pi) to (-180deg, 180deg). Altitude is |
| 845 |
// in meters. |
| 846 |
lon = (coo.m_Lon > M_PI) ? rad2deg(coo.m_Lon - 2*M_PI) : rad2deg(coo.m_Lon); |
| 847 |
lat = rad2deg(coo.m_Lat); |
| 848 |
alt = coo.m_Alt; |
| 849 |
// |
| 850 |
if( lon<180 && lon>-180 && lat<90 && lat>-90 && alt>0 ){ |
| 851 |
// |
| 852 |
orbitalinfo->lon = lon; |
| 853 |
orbitalinfo->lat = lat; |
| 854 |
orbitalinfo->alt = alt ; |
| 855 |
// |
| 856 |
// compute mag field components and L shell. |
| 857 |
// |
| 858 |
feldg_(&lat, &lon, &alt, &bnorth, &beast, &bdown, &babs); |
| 859 |
shellg_(&lat, &lon, &alt, &dimo, &xl, &icode, &bab1); |
| 860 |
findb0_(&stps, &bdel, &value, &bequ, &rr0); |
| 861 |
// |
| 862 |
orbitalinfo->Bnorth = bnorth; |
| 863 |
orbitalinfo->Beast = beast; |
| 864 |
orbitalinfo->Bdown = bdown; |
| 865 |
orbitalinfo->Babs = babs; |
| 866 |
orbitalinfo->BB0 = babs/bequ; |
| 867 |
orbitalinfo->L = xl; |
| 868 |
// Set Stormer vertical cutoff using L shell. |
| 869 |
orbitalinfo->cutoff[0] = 14.9/(xl*xl); |
| 870 |
// |
| 871 |
}; |
| 872 |
// |
| 873 |
// Fill the class |
| 874 |
// |
| 875 |
OrbitalInfotr->Fill(); |
| 876 |
// |
| 877 |
}; // loop over the events in the run |
| 878 |
// |
| 879 |
// Here you may want to clear some variables before processing another run |
| 880 |
// |
| 881 |
delete dbtime; |
| 882 |
delete L_QQ_Q_l_upper; |
| 883 |
delete L_QQ_Q_l_lower; |
| 884 |
delete RYPang_upper; |
| 885 |
delete RYPang_lower; |
| 886 |
}; // process all the runs |
| 887 |
|
| 888 |
if (verbose) printf("\n Finished processing data \n"); |
| 889 |
// |
| 890 |
closeandexit: |
| 891 |
// |
| 892 |
// 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. |
| 893 |
// |
| 894 |
if ( !reprocall && reproc && code >= 0 ){ |
| 895 |
if ( totfileentries > noaftrun ){ |
| 896 |
if (verbose){ |
| 897 |
printf("\n Post-processing: copying events from the old tree after the processed run\n"); |
| 898 |
printf(" Copying %i events in the file which are after the end of the run %i \n",(int)(totfileentries-noaftrun),(int)run); |
| 899 |
printf(" Start copying at event number %i end copying at event number %i \n",(int)noaftrun,(int)totfileentries); |
| 900 |
} |
| 901 |
for (UInt_t j = noaftrun; j < totfileentries; j++ ){ |
| 902 |
// |
| 903 |
// Get entry from old tree |
| 904 |
// |
| 905 |
OrbitalInfotrclone->GetEntry(j); |
| 906 |
// |
| 907 |
// copy orbitalinfoclone to OrbitalInfo |
| 908 |
// |
| 909 |
orbitalinfo->Clear(); |
| 910 |
// |
| 911 |
memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone)); |
| 912 |
// |
| 913 |
// Fill entry in the new tree |
| 914 |
// |
| 915 |
OrbitalInfotr->Fill(); |
| 916 |
}; |
| 917 |
if (verbose) printf(" Finished successful copying!\n"); |
| 918 |
}; |
| 919 |
}; |
| 920 |
// |
| 921 |
// Close files, delete old tree(s), write and close level2 file |
| 922 |
// |
| 923 |
if ( l0File ) l0File->Close(); |
| 924 |
if ( tempfile ) tempfile->Close(); |
| 925 |
gSystem->Unlink(tempname.str().c_str()); |
| 926 |
// |
| 927 |
if ( runinfo ) runinfo->Close(); |
| 928 |
if ( OrbitalInfotr ) OrbitalInfotr->SetName("OrbitalInfo"); |
| 929 |
if ( file ){ |
| 930 |
file->cd(); |
| 931 |
file->Write(); |
| 932 |
}; |
| 933 |
// |
| 934 |
gSystem->Unlink(OrbitalInfofolder.str().c_str()); |
| 935 |
// |
| 936 |
// the end |
| 937 |
// |
| 938 |
if (verbose) printf("\n Exiting...\n"); |
| 939 |
if(OrbitalInfotr)OrbitalInfotr->Delete(); |
| 940 |
// |
| 941 |
if ( orbitalinfo ) delete orbitalinfo; |
| 942 |
if ( orbitalinfoclone ) delete orbitalinfoclone; |
| 943 |
if ( glroot ) delete glroot; |
| 944 |
if ( runinfo ) delete runinfo; |
| 945 |
// |
| 946 |
if(code < 0) throw code; |
| 947 |
return(code); |
| 948 |
} |
| 949 |
|
| 950 |
|
| 951 |
// |
| 952 |
// Returns the cCoordGeo structure holding the geographical |
| 953 |
// coordinates for the event (see sgp4.h). |
| 954 |
// |
| 955 |
// atime is the abstime of the event in UTC unix time. |
| 956 |
// tletime is the time of the tle in UTC unix time. |
| 957 |
// tle is the previous and nearest tle (compared to atime). |
| 958 |
cCoordGeo getCoo(UInt_t atime, UInt_t tletime, cTle *tle) |
| 959 |
{ |
| 960 |
cEci eci; |
| 961 |
cOrbit orbit(*tle); |
| 962 |
orbit.getPosition((double) (atime - tletime)/60., &eci); |
| 963 |
|
| 964 |
return eci.toGeo(); |
| 965 |
} |
| 966 |
|
| 967 |
// function of copyng of quatrnions classes |
| 968 |
|
| 969 |
void CopyQ(Quaternions *Q1, Quaternions *Q2){ |
| 970 |
for(UInt_t i = 0; i < 6; i++){ |
| 971 |
Q1->time[i]=Q2->time[i]; |
| 972 |
for (UInt_t j = 0; j < 4; j++)Q1->quat[i][j]=Q2->quat[i][j]; |
| 973 |
} |
| 974 |
return; |
| 975 |
} |
| 976 |
|
| 977 |
// functions of copyng InclinationInfo classes |
| 978 |
|
| 979 |
void CopyAng(InclinationInfo *A1, InclinationInfo *A2){ |
| 980 |
A1->Tangazh = A2->Tangazh; |
| 981 |
A1->Ryskanie = A2->Ryskanie; |
| 982 |
A1->Kren = A2->Kren; |
| 983 |
return; |
| 984 |
} |
| 985 |
|
| 986 |
UInt_t holeq(Double_t lower,Double_t upper,Quaternions *Qlower, Quaternions *Qupper, UInt_t f){ |
| 987 |
|
| 988 |
UInt_t hole = 10; |
| 989 |
bool R10l = false; // Sign of R10 mode in lower quaternions array |
| 990 |
bool R10u = false; // Sign of R10 mode in upper quaternions array |
| 991 |
bool insm = false; // Sign that we inside quaternions array |
| 992 |
bool mxtml = false; // Sign of mixt mode in lower quaternions array |
| 993 |
bool mxtmu = false; // Sign of mixt mode in upper quaternions array |
| 994 |
bool npasm = false; // Sign of normall pass between R10 and non R10 or between non R10 and R10 |
| 995 |
UInt_t NCQl = 6; // Number of correct quaternions in lower array |
| 996 |
UInt_t NCQu = 6; // Number of correct quaternions in upper array |
| 997 |
if (f>0){ |
| 998 |
insm = true; |
| 999 |
if(Qupper->time[f]-Qupper->time[f-1]==30) R10u = false; |
| 1000 |
if(Qupper->time[f]-Qupper->time[f-1]<1) R10u = true; |
| 1001 |
}else{ |
| 1002 |
insm = false; |
| 1003 |
if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]<2)) R10l = true; |
| 1004 |
if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]<2)) R10u = true; |
| 1005 |
if((Qlower->time[5]-Qlower->time[0]==150)&&(Qlower->time[1]-Qlower->time[0]==30)) R10l = false; |
| 1006 |
if((Qupper->time[5]-Qupper->time[0]==150)&&(Qupper->time[1]-Qupper->time[0]==30)) R10u = false; |
| 1007 |
if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]==30)){ |
| 1008 |
mxtml = true; |
| 1009 |
for(UInt_t i = 1; i < 6; i++){ |
| 1010 |
if(Qlower->time[i]-Qlower->time[0]==30*i) NCQl=i; |
| 1011 |
} |
| 1012 |
} |
| 1013 |
if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]==30)){ |
| 1014 |
mxtmu = true; |
| 1015 |
for(UInt_t i = 1; i < 6; i++){ |
| 1016 |
if(Qupper->time[i]-Qupper->time[0]==30*i) NCQu=i; |
| 1017 |
} |
| 1018 |
} |
| 1019 |
} |
| 1020 |
|
| 1021 |
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; |
| 1022 |
|
| 1023 |
|
| 1024 |
if (R10u&&insm) hole=0; // best event R10 |
| 1025 |
if ((upper-lower<=5)&&(!insm)&&R10l&&R10u) hole = 1; // when first of 6 quaternions in array is correct |
| 1026 |
if (((!R10u)&&insm)||((!insm)&&(!R10u)&&(!R10l)&&((upper-lower==210+(6-NCQl)*30)||(upper-lower==30)))) hole = 2; //non R10 |
| 1027 |
if (npasm&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 3; //normall pass from R10 to non R10 or from non R10 to R10 |
| 1028 |
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 |
| 1029 |
if ((upper-lower>=300)&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 5; //uneliminable hole between R10 and non R10 or between non R10 and R10 |
| 1030 |
if ((upper-lower>5)&&(upper-lower<=300)&&R10u&&R10l) hole = 6; // eliminable hole inside R10 |
| 1031 |
if ((upper-lower>300)&&R10u&&R10l) hole = 7; //uneliminable hole inside R10 |
| 1032 |
if ((upper-lower>210)&&(upper-lower<=1200)&&(!R10u)&&(!R10l)) hole = 8; //eliminable hole inside non R10 |
| 1033 |
if ((upper-lower>1200)&&!R10u&&!R10l) hole = 9; // uneliminable hole inside non R10 |
| 1034 |
return hole; |
| 1035 |
} |
| 1036 |
|
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