| 1 |
// C/C++ headers |
| 2 |
// |
| 3 |
#include <fstream> |
| 4 |
#include <string.h> |
| 5 |
#include <iostream> |
| 6 |
#include <cstring> |
| 7 |
#include <stdio.h> |
| 8 |
// |
| 9 |
// ROOT headers |
| 10 |
// |
| 11 |
//#include <TCanvas.h> |
| 12 |
#include <TH2F.h> //for test only. Vitaly. |
| 13 |
#include <TVector3.h> |
| 14 |
//#include <TF1.h> |
| 15 |
|
| 16 |
#include <TTree.h> |
| 17 |
#include <TClassEdit.h> |
| 18 |
#include <TObject.h> |
| 19 |
#include <TList.h> |
| 20 |
#include <TArrayI.h> |
| 21 |
#include <TSystem.h> |
| 22 |
#include <TSystemDirectory.h> |
| 23 |
#include <TString.h> |
| 24 |
#include <TFile.h> |
| 25 |
#include <TClass.h> |
| 26 |
#include <TSQLServer.h> |
| 27 |
#include <TSQLRow.h> |
| 28 |
#include <TSQLResult.h> |
| 29 |
// |
| 30 |
// RunInfo header |
| 31 |
// |
| 32 |
#include <RunInfo.h> |
| 33 |
#include <GLTables.h> |
| 34 |
// |
| 35 |
// YODA headers |
| 36 |
// |
| 37 |
#include <PamelaRun.h> |
| 38 |
#include <PscuHeader.h> |
| 39 |
#include <PscuEvent.h> |
| 40 |
#include <EventHeader.h> |
| 41 |
#include <mcmd/McmdEvent.h> |
| 42 |
#include <mcmd/McmdRecord.h> |
| 43 |
// |
| 44 |
// This program headers |
| 45 |
// |
| 46 |
#include <OrbitalInfo.h> |
| 47 |
#include <OrbitalInfoVerl2.h> |
| 48 |
#include <OrbitalInfoCore.h> |
| 49 |
#include <InclinationInfo.h> |
| 50 |
|
| 51 |
// |
| 52 |
// Tracker and ToF classes headers and definitions |
| 53 |
// |
| 54 |
#include <ToFLevel2.h> |
| 55 |
#include <TrkLevel2.h> |
| 56 |
#include <ExtTrack.h> // new tracking code |
| 57 |
|
| 58 |
using namespace std; |
| 59 |
|
| 60 |
// |
| 61 |
// CORE ROUTINE |
| 62 |
// |
| 63 |
// |
| 64 |
int OrbitalInfoCore(UInt_t run, TFile *file, GL_TABLES *glt, Int_t OrbitalInfoargc, char *OrbitalInfoargv[]){ |
| 65 |
// |
| 66 |
Int_t i = 0; |
| 67 |
TString host = glt->CGetHost(); |
| 68 |
TString user = glt->CGetUser(); |
| 69 |
TString psw = glt->CGetPsw(); |
| 70 |
TSQLServer *dbc = TSQLServer::Connect(host.Data(),user.Data(),psw.Data()); |
| 71 |
// |
| 72 |
stringstream myquery; |
| 73 |
myquery.str(""); |
| 74 |
myquery << "SET time_zone='+0:00'; SET sql_mode = 'NO_UNSIGNED_SUBTRACTION';"; |
| 75 |
delete dbc->Query(myquery.str().c_str()); |
| 76 |
// |
| 77 |
TString processFolder = Form("OrbitalInfoFolder_%u",run); |
| 78 |
// |
| 79 |
// Set these to true to have a very verbose output. |
| 80 |
// |
| 81 |
Bool_t debug = false; |
| 82 |
// |
| 83 |
Bool_t verbose = false; |
| 84 |
// |
| 85 |
Bool_t standalone = false; |
| 86 |
// |
| 87 |
if ( OrbitalInfoargc > 0 ){ |
| 88 |
i = 0; |
| 89 |
while ( i < OrbitalInfoargc ){ |
| 90 |
if ( !strcmp(OrbitalInfoargv[i],"-processFolder") ) { |
| 91 |
if ( OrbitalInfoargc < i+1 ){ |
| 92 |
throw -3; |
| 93 |
}; |
| 94 |
processFolder = (TString)OrbitalInfoargv[i+1]; |
| 95 |
i++; |
| 96 |
}; |
| 97 |
if ( (!strcmp(OrbitalInfoargv[i],"--debug")) || (!strcmp(OrbitalInfoargv[i],"-g")) ) { |
| 98 |
verbose = true; |
| 99 |
debug = true; |
| 100 |
}; |
| 101 |
if ( (!strcmp(OrbitalInfoargv[i],"--verbose")) || (!strcmp(OrbitalInfoargv[i],"-v")) ) { |
| 102 |
verbose = true; |
| 103 |
}; |
| 104 |
if ( (!strcmp(OrbitalInfoargv[i],"--standalone")) ) { |
| 105 |
standalone = true; |
| 106 |
}; |
| 107 |
if ( (!strcmp(OrbitalInfoargv[i],"--calculate-pitch")) ) { |
| 108 |
standalone = false; |
| 109 |
}; |
| 110 |
i++; |
| 111 |
}; |
| 112 |
}; |
| 113 |
// |
| 114 |
const char* outDir = gSystem->DirName(gSystem->DirName(file->GetPath())); |
| 115 |
// |
| 116 |
TTree *OrbitalInfotr = 0; |
| 117 |
UInt_t nevents = 0; |
| 118 |
UInt_t neventsm = 0; |
| 119 |
// |
| 120 |
// variables needed to reprocess data |
| 121 |
// |
| 122 |
Long64_t maxsize = 10000000000LL; |
| 123 |
TTree::SetMaxTreeSize(maxsize); |
| 124 |
// |
| 125 |
TString OrbitalInfoversion; |
| 126 |
ItoRunInfo *runinfo = 0; |
| 127 |
TArrayI *runlist = 0; |
| 128 |
TTree *OrbitalInfotrclone = 0; |
| 129 |
Bool_t reproc = false; |
| 130 |
Bool_t reprocall = false; |
| 131 |
Bool_t igrfloaded = false; |
| 132 |
UInt_t nobefrun = 0; |
| 133 |
UInt_t noaftrun = 0; |
| 134 |
UInt_t numbofrun = 0; |
| 135 |
stringstream ftmpname; |
| 136 |
TString fname; |
| 137 |
UInt_t totfileentries = 0; |
| 138 |
UInt_t idRun = 0; |
| 139 |
UInt_t anni5 = 60 * 60 * 24 * 365 * 5 ;//1576800 |
| 140 |
// |
| 141 |
// My variables. Vitaly. |
| 142 |
// |
| 143 |
// UInt_t oi = 0; |
| 144 |
Int_t tmpSize = 0; |
| 145 |
// |
| 146 |
// variables needed to handle error signals |
| 147 |
// |
| 148 |
Int_t code = 0; |
| 149 |
Int_t sgnl; |
| 150 |
// |
| 151 |
// OrbitalInfo classes |
| 152 |
// |
| 153 |
OrbitalInfo *orbitalinfo = new OrbitalInfo(); |
| 154 |
OrbitalInfo *orbitalinfoclone = new OrbitalInfo(); |
| 155 |
|
| 156 |
// |
| 157 |
// define variables for opening and reading level0 file |
| 158 |
// |
| 159 |
TFile *l0File = 0; |
| 160 |
TTree *l0tr = 0; |
| 161 |
// TTree *l0trm = 0; |
| 162 |
TChain *ch = 0; |
| 163 |
// EM: open also header branch |
| 164 |
TBranch *l0head = 0; |
| 165 |
pamela::EventHeader *eh = 0; |
| 166 |
pamela::PscuHeader *ph = 0; |
| 167 |
pamela::McmdEvent *mcmdev = 0; |
| 168 |
pamela::McmdRecord *mcmdrc = 0; |
| 169 |
// end EM |
| 170 |
|
| 171 |
// pamela::RunHeaderEvent *reh = new pamela::RunHeaderEvent; |
| 172 |
// pamela::EventHeader *eH = new pamela::EventHeader; |
| 173 |
|
| 174 |
// |
| 175 |
// Define other basic variables |
| 176 |
// |
| 177 |
UInt_t procev = 0; |
| 178 |
stringstream file2; |
| 179 |
stringstream file3; |
| 180 |
stringstream qy; |
| 181 |
Int_t totevent = 0; |
| 182 |
UInt_t atime = 0; |
| 183 |
UInt_t re = 0; |
| 184 |
UInt_t ik = 0; |
| 185 |
|
| 186 |
// Position |
| 187 |
Float_t lon, lat, alt; |
| 188 |
|
| 189 |
// |
| 190 |
// IGRF stuff |
| 191 |
// |
| 192 |
Double_t dimo = 0.0; // dipole moment (computed from dat files) // EM GCC 4.7 |
| 193 |
Float_t bnorth, beast, bdown, babs; |
| 194 |
Float_t xl; // L value |
| 195 |
Float_t icode; // code value for L accuracy (see fortran code) |
| 196 |
Float_t bab1; // What's the difference with babs? |
| 197 |
Float_t stps = 0.005; // step size for field line tracing |
| 198 |
Float_t bdel = 0.01; // required accuracy |
| 199 |
Float_t bequ; // equatorial b value (also called b_0) |
| 200 |
Bool_t value = 0; // false if bequ is not the minimum b value |
| 201 |
Float_t rr0; // equatorial radius normalized to earth radius |
| 202 |
|
| 203 |
// |
| 204 |
// Working filename |
| 205 |
// |
| 206 |
TString outputfile; |
| 207 |
stringstream name; |
| 208 |
name.str(""); |
| 209 |
name << outDir << "/"; |
| 210 |
// |
| 211 |
// temporary file and folder |
| 212 |
// |
| 213 |
TFile *tempfile = 0; |
| 214 |
TTree *tempOrbitalInfo = 0; |
| 215 |
stringstream tempname; |
| 216 |
stringstream OrbitalInfofolder; |
| 217 |
Bool_t myfold = false; |
| 218 |
tempname.str(""); |
| 219 |
tempname << outDir; |
| 220 |
tempname << "/" << processFolder.Data(); |
| 221 |
OrbitalInfofolder.str(""); |
| 222 |
OrbitalInfofolder << tempname.str().c_str(); |
| 223 |
tempname << "/OrbitalInfotree_run"; |
| 224 |
tempname << run << ".root"; |
| 225 |
UInt_t totnorun = 0; |
| 226 |
// |
| 227 |
// DB classes |
| 228 |
// |
| 229 |
GL_ROOT *glroot = new GL_ROOT(); |
| 230 |
GL_TIMESYNC *dbtime = 0; |
| 231 |
GL_TLE *gltle = new GL_TLE(); |
| 232 |
// |
| 233 |
//Quaternions classes |
| 234 |
// |
| 235 |
Quaternions *L_QQ_Q_l_lower = 0; |
| 236 |
InclinationInfo *RYPang_lower = 0; |
| 237 |
Quaternions *L_QQ_Q_l_upper = 0; |
| 238 |
InclinationInfo *RYPang_upper = 0; |
| 239 |
|
| 240 |
cEci eCi; |
| 241 |
|
| 242 |
// Initialize fortran routines!!! |
| 243 |
Int_t ltp1 = 0; |
| 244 |
Int_t ltp2 = 0; |
| 245 |
Int_t ltp3 = 0; |
| 246 |
// Int_t uno = 1; |
| 247 |
// const char *niente = " "; |
| 248 |
GL_PARAM *glparam0 = new GL_PARAM(); |
| 249 |
GL_PARAM *glparam = new GL_PARAM(); |
| 250 |
GL_PARAM *glparam2 = new GL_PARAM(); |
| 251 |
GL_PARAM *glparam3 = new GL_PARAM(); |
| 252 |
|
| 253 |
// |
| 254 |
// Orientation variables. Vitaly |
| 255 |
// |
| 256 |
|
| 257 |
UInt_t evfrom = 0; |
| 258 |
UInt_t jumped = 0; |
| 259 |
Int_t itr = -1; |
| 260 |
// Double_t A1; |
| 261 |
// Double_t A2; |
| 262 |
// Double_t A3; |
| 263 |
Double_t Px = 0; |
| 264 |
Double_t Py = 0; |
| 265 |
Double_t Pz = 0; |
| 266 |
TTree *ttof = 0; |
| 267 |
ToFLevel2 *tof = new ToFLevel2(); |
| 268 |
TTree *ttrke = 0; |
| 269 |
TrkLevel2 *trke = new TrkLevel2(); |
| 270 |
OrientationInfo *PO = new OrientationInfo(); |
| 271 |
Int_t nz = 6; |
| 272 |
Float_t zin[6]; |
| 273 |
Int_t nevtofl2 = 0; |
| 274 |
Int_t nevtrkl2 = 0; |
| 275 |
if ( verbose ) cout<<"Reading quaternions external file"<<endl; |
| 276 |
cout.setf(ios::fixed,ios::floatfield); |
| 277 |
/******Reading recovered quaternions...*********/ |
| 278 |
vector<Double_t> recqtime; |
| 279 |
vector<Float_t> recq0; |
| 280 |
vector<Float_t> recq1; |
| 281 |
vector<Float_t> recq2; |
| 282 |
vector<Float_t> recq3; |
| 283 |
Float_t Norm = 1; |
| 284 |
|
| 285 |
vector<UInt_t> RTtime1; |
| 286 |
vector<UInt_t> RTtime2; |
| 287 |
vector<Double_t> RTbank1; |
| 288 |
vector<Double_t> RTbank2; |
| 289 |
vector<Double_t> RTbpluto1; |
| 290 |
vector<Double_t> RTbpluto2; |
| 291 |
vector<Int_t> RTazim; |
| 292 |
vector<UInt_t> RTstart; |
| 293 |
vector<UInt_t> RTpluto2; |
| 294 |
vector<UInt_t> RTpluto1; |
| 295 |
vector<Int_t> RTerrq; |
| 296 |
|
| 297 |
TClonesArray *tcNucleiTrk = NULL; |
| 298 |
TClonesArray *tcExtNucleiTrk = NULL; |
| 299 |
TClonesArray *tcExtTrk = NULL; |
| 300 |
TClonesArray *tcNucleiTof = NULL; |
| 301 |
TClonesArray *tcExtNucleiTof = NULL; |
| 302 |
TClonesArray *tcExtTof = NULL; |
| 303 |
TClonesArray *torbNucleiTrk = NULL; |
| 304 |
TClonesArray *torbExtNucleiTrk = NULL; |
| 305 |
TClonesArray *torbExtTrk = NULL; |
| 306 |
Bool_t hasNucleiTrk = false; |
| 307 |
Bool_t hasExtNucleiTrk = false; |
| 308 |
Bool_t hasExtTrk = false; |
| 309 |
Bool_t hasNucleiTof = false; |
| 310 |
Bool_t hasExtNucleiTof = false; |
| 311 |
Bool_t hasExtTof = false; |
| 312 |
|
| 313 |
ifstream in; |
| 314 |
ifstream an; |
| 315 |
// ofstream mc; |
| 316 |
// TString gr; |
| 317 |
Int_t parerror2=0; |
| 318 |
|
| 319 |
Int_t parerror=glparam0->Query_GL_PARAM(1,303,dbc); // parameters stored in DB in GL_PRAM table |
| 320 |
if ( verbose ) cout<<parerror<<"\t"<<(char*)(glparam0->PATH+glparam0->NAME).Data()<<endl; |
| 321 |
if ( parerror<0 ) { |
| 322 |
code = parerror; |
| 323 |
goto closeandexit; |
| 324 |
} |
| 325 |
in.open((char*)(glparam0->PATH+glparam0->NAME).Data(),ios::in); |
| 326 |
while(!in.eof()){ |
| 327 |
recqtime.resize(recqtime.size()+1); |
| 328 |
Int_t sizee = recqtime.size(); |
| 329 |
recq0.resize(sizee); |
| 330 |
recq1.resize(sizee); |
| 331 |
recq2.resize(sizee); |
| 332 |
recq3.resize(sizee); |
| 333 |
in>>recqtime[sizee-1]; |
| 334 |
in>>recq0[sizee-1]; |
| 335 |
in>>recq1[sizee-1]; |
| 336 |
in>>recq2[sizee-1]; |
| 337 |
in>>recq3[sizee-1]; |
| 338 |
in>>Norm; |
| 339 |
} |
| 340 |
in.close(); |
| 341 |
if ( verbose ) cout<<"We have read recovered data"<<endl; |
| 342 |
if (debug) cout << "size of recovered quaterions data set is " << recqtime.size() << endl; |
| 343 |
|
| 344 |
if ( verbose ) cout<<"read Rotation Table"<<endl; |
| 345 |
|
| 346 |
parerror2=glparam0->Query_GL_PARAM(1,305,dbc); |
| 347 |
|
| 348 |
if ( verbose ) cout<<parerror2<<"\t"<<(char*)(glparam0->PATH+glparam0->NAME).Data()<<endl; |
| 349 |
if ( parerror2<0 ) { |
| 350 |
code = parerror; |
| 351 |
goto closeandexit; |
| 352 |
} |
| 353 |
an.open((char*)(glparam0->PATH+glparam0->NAME).Data(),ios::in); |
| 354 |
while(!an.eof()){ |
| 355 |
RTtime1.resize(RTtime1.size()+1); |
| 356 |
Int_t sizee = RTtime1.size(); |
| 357 |
RTbank1.resize(sizee+1); |
| 358 |
RTazim.resize(sizee+1); |
| 359 |
RTerrq.resize(sizee+1); |
| 360 |
RTstart.resize(sizee+1); |
| 361 |
RTpluto1.resize(sizee+1); |
| 362 |
RTbpluto1.resize(sizee+1); |
| 363 |
an>>RTtime1[sizee-1]; |
| 364 |
an>>RTbank1[sizee-1]; |
| 365 |
an>>RTstart[sizee-1]; |
| 366 |
an>>RTpluto1[sizee-1]; |
| 367 |
an>>RTbpluto1[sizee-1]; |
| 368 |
an>>RTazim[sizee-1]; |
| 369 |
an>>RTerrq[sizee-1]; |
| 370 |
if(sizee>1) { |
| 371 |
RTtime2.resize(sizee+1); |
| 372 |
RTbank2.resize(sizee+1); |
| 373 |
RTpluto2.resize(sizee+1); |
| 374 |
RTbpluto2.resize(sizee+1); |
| 375 |
RTtime2[sizee-2]=RTtime1[sizee-1]; |
| 376 |
RTpluto2[sizee-2]=RTpluto1[sizee-1]; |
| 377 |
RTbank2[sizee-2]=RTbank1[sizee-1]; |
| 378 |
RTbpluto2[sizee-2]=RTbpluto1[sizee-1]; |
| 379 |
} |
| 380 |
} |
| 381 |
an.close(); |
| 382 |
//cout<<"put some number here"<<endl; |
| 383 |
//Int_t yupi; |
| 384 |
//cin>>yupi; |
| 385 |
|
| 386 |
if ( verbose ) cout<<"We have read Rotation Table"<<endl; |
| 387 |
//Geomagnetic coordinates calculations staff |
| 388 |
|
| 389 |
GMtype_CoordGeodetic location; |
| 390 |
// GMtype_CoordDipole GMlocation; |
| 391 |
GMtype_Ellipsoid Ellip; |
| 392 |
GMtype_Data G0, G1, H1; |
| 393 |
|
| 394 |
// { // this braces is necessary to avoid jump to label 'closeandexit' error // but it is wrong since the variable "igpath" will not exist outside. To overcome the "jump to label 'closeandexit' error" it is necessary to set the "igpath" before line 276 |
| 395 |
// TString igpath="/data03/Malakhov/pam9Malakhov/installed10/calib/orb-param/"; |
| 396 |
// } |
| 397 |
|
| 398 |
// GM_ScanIGRF(glparam->PATH, &G0, &G1, &H1); |
| 399 |
GM_ScanIGRF(dbc, &G0, &G1, &H1); |
| 400 |
|
| 401 |
//cout << G0.element[0] << "\t" << G1.element[0] << "\t" << H1.element[0] << endl; |
| 402 |
//cout << G0.element[5] << "\t" << G1.element[5] << "\t" << H1.element[5] << endl; |
| 403 |
|
| 404 |
GM_SetEllipsoid(&Ellip); |
| 405 |
|
| 406 |
// IGRF stuff moved inside run loop! |
| 407 |
|
| 408 |
for (Int_t ip=0;ip<nz;ip++){ |
| 409 |
zin[ip] = tof->GetZTOF(tof->GetToFPlaneID(ip)); |
| 410 |
}; |
| 411 |
// |
| 412 |
if ( !standalone ){ |
| 413 |
// |
| 414 |
// Does it contain the Tracker and ToF trees? |
| 415 |
// |
| 416 |
ttof = (TTree*)file->Get("ToF"); |
| 417 |
if ( !ttof ) { |
| 418 |
if ( verbose ) printf(" OrbitalInfo - ERROR: no tof tree\n"); |
| 419 |
code = -900; |
| 420 |
goto closeandexit; |
| 421 |
} |
| 422 |
ttof->SetBranchAddress("ToFLevel2",&tof); |
| 423 |
nevtofl2 = ttof->GetEntries(); |
| 424 |
|
| 425 |
// |
| 426 |
// Look for extended tracking algorithm |
| 427 |
// |
| 428 |
if ( verbose ) printf("Look for extended and nuclei tracking algorithms in ToF\n"); |
| 429 |
// Nuclei tracking algorithm |
| 430 |
Int_t checkAlgo = 0; |
| 431 |
tcNucleiTof = new TClonesArray("ToFTrkVar"); |
| 432 |
checkAlgo = ttof->SetBranchAddress("TrackNuclei",&tcNucleiTof); |
| 433 |
if ( !checkAlgo ){ |
| 434 |
if ( verbose ) printf(" Nuclei tracking algorithm ToF branch found! :D \n"); |
| 435 |
hasNucleiTof = true; |
| 436 |
} else { |
| 437 |
if ( verbose ) printf(" Nuclei tracking algorithm ToF branch not found :( !\n"); |
| 438 |
printf(" ok, this is not a problem (it depends on tracker settings) \n"); |
| 439 |
delete tcNucleiTof; |
| 440 |
tcNucleiTof=NULL; // 10RED reprocessing bug |
| 441 |
} |
| 442 |
// Nuclei tracking algorithm using calorimeter points |
| 443 |
tcExtNucleiTof = new TClonesArray("ToFTrkVar"); |
| 444 |
checkAlgo = ttof->SetBranchAddress("RecoveredTrackNuclei",&tcExtNucleiTof); |
| 445 |
if ( !checkAlgo ){ |
| 446 |
if ( verbose ) printf(" Recovered nuclei tracking algorithm ToF branch found! :D \n"); |
| 447 |
hasExtNucleiTof = true; |
| 448 |
} else { |
| 449 |
if ( verbose ) printf(" Recovered nuclei tracking algorithm ToF branch not found :( !\n"); |
| 450 |
printf(" ok, this is not a problem (it depends on tracker settings) \n"); |
| 451 |
delete tcExtNucleiTof; |
| 452 |
tcExtNucleiTof=NULL; // 10RED reprocessing bug |
| 453 |
} |
| 454 |
// Tracking algorithm using calorimeter points |
| 455 |
tcExtTof = new TClonesArray("ToFTrkVar"); |
| 456 |
checkAlgo = ttof->SetBranchAddress("RecoveredTrack",&tcExtTof); |
| 457 |
if ( !checkAlgo ){ |
| 458 |
if ( verbose ) printf(" Recovered track algorithm ToF branch found! :D \n"); |
| 459 |
hasExtTof = true; |
| 460 |
} else { |
| 461 |
if ( verbose ) printf(" Recovered track algorithm ToF branch not found :( !\n"); |
| 462 |
printf(" ok, this is not a problem (it depends on tracker settings) \n"); |
| 463 |
delete tcExtTof; |
| 464 |
tcExtTof=NULL; // 10RED reprocessing bug |
| 465 |
} |
| 466 |
|
| 467 |
ttrke = (TTree*)file->Get("Tracker"); |
| 468 |
if ( !ttrke ) { |
| 469 |
if ( verbose ) printf(" OrbitalInfo - ERROR: no trk tree\n"); |
| 470 |
code = -903; |
| 471 |
goto closeandexit; |
| 472 |
} |
| 473 |
ttrke->SetBranchAddress("TrkLevel2",&trke); |
| 474 |
nevtrkl2 = ttrke->GetEntries(); |
| 475 |
|
| 476 |
// |
| 477 |
// Look for extended tracking algorithm |
| 478 |
// |
| 479 |
if ( verbose ) printf("Look for extended and nuclei tracking algorithms\n"); |
| 480 |
// Nuclei tracking algorithm |
| 481 |
checkAlgo = 0; |
| 482 |
tcNucleiTrk = new TClonesArray("TrkTrack"); |
| 483 |
checkAlgo = ttrke->SetBranchAddress("TrackNuclei",&tcNucleiTrk); |
| 484 |
if ( !checkAlgo ){ |
| 485 |
if ( verbose ) printf(" Nuclei tracking algorithm branch found! :D \n"); |
| 486 |
hasNucleiTrk = true; |
| 487 |
} else { |
| 488 |
if ( verbose ) printf(" Nuclei tracking algorithm branch not found :( !\n"); |
| 489 |
printf(" ok, this is not a problem (it depends on tracker settings) \n"); |
| 490 |
delete tcNucleiTrk; |
| 491 |
tcNucleiTrk=NULL; // 10RED reprocessing bug |
| 492 |
} |
| 493 |
// Nuclei tracking algorithm using calorimeter points |
| 494 |
tcExtNucleiTrk = new TClonesArray("ExtTrack"); |
| 495 |
checkAlgo = ttrke->SetBranchAddress("RecoveredTrackNuclei",&tcExtNucleiTrk); |
| 496 |
if ( !checkAlgo ){ |
| 497 |
if ( verbose ) printf(" Recovered nuclei tracking algorithm branch found! :D \n"); |
| 498 |
hasExtNucleiTrk = true; |
| 499 |
} else { |
| 500 |
if ( verbose ) printf(" Recovered nuclei tracking algorithm branch not found :( !\n"); |
| 501 |
printf(" ok, this is not a problem (it depends on tracker settings) \n"); |
| 502 |
delete tcExtNucleiTrk; |
| 503 |
tcExtNucleiTrk=NULL; // 10RED reprocessing bug |
| 504 |
} |
| 505 |
// Tracking algorithm using calorimeter points |
| 506 |
tcExtTrk = new TClonesArray("ExtTrack"); |
| 507 |
checkAlgo = ttrke->SetBranchAddress("RecoveredTrack",&tcExtTrk); |
| 508 |
if ( !checkAlgo ){ |
| 509 |
if ( verbose ) printf(" Recovered track algorithm branch found! :D \n"); |
| 510 |
hasExtTrk = true; |
| 511 |
} else { |
| 512 |
if ( verbose ) printf(" Recovered track algorithm branch not found :( !\n"); |
| 513 |
printf(" ok, this is not a problem (it depends on tracker settings) \n"); |
| 514 |
delete tcExtTrk; |
| 515 |
tcExtTrk=NULL; // 10RED reprocessing bug |
| 516 |
} |
| 517 |
|
| 518 |
if ( (hasNucleiTrk && !hasNucleiTof) || (!hasNucleiTrk && hasNucleiTof) || |
| 519 |
(hasExtNucleiTrk && !hasExtNucleiTof) || (!hasExtNucleiTrk && hasExtNucleiTof) || |
| 520 |
(hasExtTrk && !hasExtTof) || (!hasExtTrk && hasExtTof) |
| 521 |
){ |
| 522 |
if ( verbose ) printf(" ERROR: Mismatch between tracker and tof tree branches concerning extended tracking algorithm(s)\n"); |
| 523 |
if ( debug ) printf("hasNucleiTrk %i hasExtNucleiTrk %i hasExtTrk %i \n",hasNucleiTrk,hasExtNucleiTrk,hasExtTrk); |
| 524 |
if ( debug ) printf("hasNucleiTof %i hasExtNucleiTof %i hasExtTof %i \n",hasNucleiTof,hasExtNucleiTof,hasExtTof); |
| 525 |
throw -901; |
| 526 |
} |
| 527 |
|
| 528 |
} |
| 529 |
// |
| 530 |
// Let's start! |
| 531 |
// |
| 532 |
// 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 |
| 533 |
// if run != 0 we must process only that run but first we have to check if the tree MyDetector2 already exist in the file |
| 534 |
// if it exists we are reprocessing data and we must delete that entries, if not we must create it. |
| 535 |
// |
| 536 |
if ( run == 0 ) reproc = true; |
| 537 |
// |
| 538 |
// |
| 539 |
// Output file is "outputfile" |
| 540 |
// |
| 541 |
if ( !file->IsOpen() ){ |
| 542 |
//printf(" OrbitalInfo - ERROR: cannot open file for writing\n"); |
| 543 |
throw -901; |
| 544 |
}; |
| 545 |
// |
| 546 |
// Retrieve GL_RUN variables from the level2 file |
| 547 |
// |
| 548 |
OrbitalInfoversion = OrbitalInfoInfo(false); // we should decide how to handle versioning system |
| 549 |
// |
| 550 |
// create an interface to RunInfo called "runinfo" |
| 551 |
// |
| 552 |
runinfo = new ItoRunInfo(file); |
| 553 |
// |
| 554 |
// open "Run" tree in level2 file, if not existing return an error (sngl != 0) |
| 555 |
// |
| 556 |
sgnl = 0; |
| 557 |
sgnl = runinfo->Update(run, "ORB", OrbitalInfoversion); |
| 558 |
//sgnl = runinfo->Read(run); |
| 559 |
|
| 560 |
if ( sgnl ){ |
| 561 |
//printf("OrbitalInfo - ERROR: RunInfo exited with non-zero status\n"); |
| 562 |
code = sgnl; |
| 563 |
goto closeandexit; |
| 564 |
} else { |
| 565 |
sgnl = 0; |
| 566 |
}; |
| 567 |
// |
| 568 |
// number of events in the file BEFORE the first event of our run |
| 569 |
// |
| 570 |
nobefrun = runinfo->GetFirstEntry(); |
| 571 |
// |
| 572 |
// total number of events in the file |
| 573 |
// |
| 574 |
totfileentries = runinfo->GetFileEntries(); |
| 575 |
// |
| 576 |
// first file entry AFTER the last event of our run |
| 577 |
// |
| 578 |
noaftrun = runinfo->GetLastEntry() + 1; |
| 579 |
// |
| 580 |
// number of run to be processed |
| 581 |
// |
| 582 |
numbofrun = runinfo->GetNoRun(); |
| 583 |
totnorun = runinfo->GetRunEntries(); |
| 584 |
// |
| 585 |
// Try to access the OrbitalInfo tree in the file, if it exists we are reprocessing data if not we are processing a new run |
| 586 |
// |
| 587 |
OrbitalInfotrclone = (TTree*)file->Get("OrbitalInfo"); |
| 588 |
// |
| 589 |
if ( !OrbitalInfotrclone ){ |
| 590 |
// |
| 591 |
// tree does not exist, we are not reprocessing |
| 592 |
// |
| 593 |
reproc = false; |
| 594 |
if ( run == 0 ){ |
| 595 |
if (verbose) printf(" OrbitalInfo - WARNING: you are reprocessing data but OrbitalInfo tree does not exist!\n"); |
| 596 |
} |
| 597 |
if ( runinfo->IsReprocessing() && run != 0 ) { |
| 598 |
if (verbose) printf(" OrbitalInfo - WARNING: it seems you are not reprocessing data but OrbitalInfo\n versioning information already exists in RunInfo.\n"); |
| 599 |
} |
| 600 |
} else { |
| 601 |
// |
| 602 |
// tree exists, we are reprocessing data. Are we reprocessing a single run or all the file? |
| 603 |
// |
| 604 |
OrbitalInfotrclone->SetAutoSave(900000000000000LL); |
| 605 |
reproc = true; |
| 606 |
// |
| 607 |
// |
| 608 |
if (verbose) printf("\n Preparing the pre-processing...\n"); |
| 609 |
// |
| 610 |
if ( run == 0 || totnorun == 1 ){ |
| 611 |
// |
| 612 |
// we are reprocessing all the file |
| 613 |
// 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 |
| 614 |
// |
| 615 |
reprocall = true; |
| 616 |
// |
| 617 |
if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing all runs\n Deleting old tree...\n"); |
| 618 |
// |
| 619 |
} else { |
| 620 |
// |
| 621 |
// 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 |
| 622 |
// |
| 623 |
reprocall = false; |
| 624 |
// |
| 625 |
if (verbose) printf("\n OrbitalInfo - WARNING: Reprocessing run number %u \n",run); |
| 626 |
// |
| 627 |
// copying old tree to a new file |
| 628 |
// |
| 629 |
gSystem->MakeDirectory(OrbitalInfofolder.str().c_str()); |
| 630 |
myfold = true; |
| 631 |
tempfile = new TFile(tempname.str().c_str(),"RECREATE"); |
| 632 |
tempOrbitalInfo = OrbitalInfotrclone->CloneTree(-1,"fast"); |
| 633 |
tempOrbitalInfo->SetName("OrbitalInfo-old"); |
| 634 |
tempfile->Write(); |
| 635 |
tempOrbitalInfo->Delete(); |
| 636 |
tempfile->Close(); |
| 637 |
} |
| 638 |
// |
| 639 |
// Delete the old tree from old file and memory |
| 640 |
// |
| 641 |
OrbitalInfotrclone->Clear(); |
| 642 |
OrbitalInfotrclone->Delete("all"); |
| 643 |
// |
| 644 |
if (verbose) printf(" ...done!\n"); |
| 645 |
// |
| 646 |
}; |
| 647 |
// |
| 648 |
// create mydetector tree mydect |
| 649 |
// |
| 650 |
file->cd(); |
| 651 |
OrbitalInfotr = new TTree("OrbitalInfo-new","PAMELA OrbitalInfo data"); |
| 652 |
OrbitalInfotr->SetAutoSave(900000000000000LL); |
| 653 |
orbitalinfo->Set();//ELENA **TEMPORANEO?** |
| 654 |
OrbitalInfotr->Branch("OrbitalInfo","OrbitalInfo",&orbitalinfo); |
| 655 |
// |
| 656 |
// create new branches for new tracking algorithms |
| 657 |
// |
| 658 |
if ( hasNucleiTrk ){ |
| 659 |
torbNucleiTrk = new TClonesArray("OrbitalInfoTrkVar",1); |
| 660 |
OrbitalInfotr->Branch("TrackNuclei",&torbNucleiTrk); |
| 661 |
} |
| 662 |
if ( hasExtNucleiTrk ){ |
| 663 |
torbExtNucleiTrk = new TClonesArray("OrbitalInfoTrkVar",1); |
| 664 |
OrbitalInfotr->Branch("RecoveredTrackNuclei",&torbExtNucleiTrk); |
| 665 |
} |
| 666 |
if ( hasExtTrk ){ |
| 667 |
torbExtTrk = new TClonesArray("OrbitalInfoTrkVar",1); |
| 668 |
OrbitalInfotr->Branch("RecoveredTrack",&torbExtTrk); |
| 669 |
} |
| 670 |
|
| 671 |
// |
| 672 |
if ( reproc && !reprocall ){ |
| 673 |
// |
| 674 |
// open new file and retrieve also tree informations |
| 675 |
// |
| 676 |
tempfile = new TFile(tempname.str().c_str(),"READ"); |
| 677 |
OrbitalInfotrclone = (TTree*)tempfile->Get("OrbitalInfo-old"); |
| 678 |
OrbitalInfotrclone->SetAutoSave(900000000000000LL); |
| 679 |
OrbitalInfotrclone->SetBranchAddress("OrbitalInfo",&orbitalinfoclone); |
| 680 |
// |
| 681 |
if ( nobefrun > 0 ){ |
| 682 |
if (verbose){ |
| 683 |
printf("\n Pre-processing: copying events from the old tree before the processed run\n"); |
| 684 |
printf(" Copying %u events in the file which are before the beginning of the run %u \n",nobefrun,run); |
| 685 |
printf(" Start copying at event number 0, end copying at event number %u \n",nobefrun); |
| 686 |
} |
| 687 |
for (UInt_t j = 0; j < nobefrun; j++){ |
| 688 |
// |
| 689 |
if ( OrbitalInfotrclone->GetEntry(j) <= 0 ) throw -36; |
| 690 |
// |
| 691 |
// copy orbitalinfoclone to mydec |
| 692 |
// |
| 693 |
// orbitalinfo->Clear(); |
| 694 |
// |
| 695 |
memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone)); |
| 696 |
// |
| 697 |
// Fill entry in the new tree |
| 698 |
// |
| 699 |
OrbitalInfotr->Fill(); |
| 700 |
// |
| 701 |
}; |
| 702 |
if (verbose) printf(" Finished successful copying!\n"); |
| 703 |
}; |
| 704 |
}; |
| 705 |
// |
| 706 |
// |
| 707 |
// Get the list of run to be processed, if only one run has to be processed the list will contain one entry only. |
| 708 |
// |
| 709 |
runlist = runinfo->GetRunList(); |
| 710 |
// |
| 711 |
// Loop over the run to be processed |
| 712 |
// |
| 713 |
for (UInt_t irun=0; irun < numbofrun; irun++){ |
| 714 |
|
| 715 |
L_QQ_Q_l_lower = new Quaternions(); |
| 716 |
RYPang_lower = new InclinationInfo(); |
| 717 |
L_QQ_Q_l_upper = new Quaternions(); |
| 718 |
RYPang_upper = new InclinationInfo(); |
| 719 |
|
| 720 |
// |
| 721 |
// retrieve the first run ID to be processed using the RunInfo list |
| 722 |
// |
| 723 |
|
| 724 |
idRun = runlist->At(irun); |
| 725 |
if (verbose){ |
| 726 |
printf("\n\n\n ####################################################################### \n"); |
| 727 |
printf(" PROCESSING RUN NUMBER %i \n",(int)idRun); |
| 728 |
printf(" ####################################################################### \n\n\n"); |
| 729 |
} |
| 730 |
// |
| 731 |
runinfo->ID_ROOT_L0 = 0; |
| 732 |
// |
| 733 |
// store in the runinfo class the GL_RUN variables for our run |
| 734 |
// |
| 735 |
sgnl = 0; |
| 736 |
sgnl = runinfo->GetRunInfo(idRun); |
| 737 |
if ( sgnl ){ |
| 738 |
if ( debug ) printf("\n OrbitalInfo - ERROR: RunInfo exited with non-zero status\n"); |
| 739 |
code = sgnl; |
| 740 |
goto closeandexit; |
| 741 |
} else { |
| 742 |
sgnl = 0; |
| 743 |
}; |
| 744 |
// |
| 745 |
// now you can access that variables using the RunInfo class this way runinfo->ID_REG_RUN |
| 746 |
// |
| 747 |
if ( runinfo->ID_ROOT_L0 == 0 ){ |
| 748 |
if ( debug ) printf("\n OrbitalInfo - ERROR: no run with ID_RUN = %u \n\n Exiting... \n\n",idRun); |
| 749 |
code = -5; |
| 750 |
goto closeandexit; |
| 751 |
}; |
| 752 |
// |
| 753 |
// prepare the timesync for the db |
| 754 |
// |
| 755 |
dbtime = new GL_TIMESYNC(runinfo->ID_ROOT_L0,"ID",dbc); |
| 756 |
|
| 757 |
// |
| 758 |
// Search in the DB the path and name of the LEVEL0 file to be processed. |
| 759 |
// |
| 760 |
glroot->Query_GL_ROOT(runinfo->ID_ROOT_L0,dbc); |
| 761 |
// |
| 762 |
ftmpname.str(""); |
| 763 |
ftmpname << glroot->PATH.Data() << "/"; |
| 764 |
ftmpname << glroot->NAME.Data(); |
| 765 |
fname = ftmpname.str().c_str(); |
| 766 |
ftmpname.str(""); |
| 767 |
// |
| 768 |
// print nout informations |
| 769 |
// |
| 770 |
totevent = runinfo->NEVENTS; |
| 771 |
evfrom = runinfo->EV_FROM; |
| 772 |
//cout<<"totevents = "<<totevent<<"\n"; |
| 773 |
if (verbose){ |
| 774 |
printf("\n LEVEL0 data file: %s \n",fname.Data()); |
| 775 |
printf(" RUN HEADER absolute time is: %u \n",runinfo->RUNHEADER_TIME); |
| 776 |
printf(" RUN TRAILER absolute time is: %u \n",runinfo->RUNTRAILER_TIME); |
| 777 |
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); |
| 778 |
}// |
| 779 |
// |
| 780 |
// if ( !totevent ) goto closeandexit; |
| 781 |
// Open Level0 file |
| 782 |
if ( l0File ) l0File->Close(); |
| 783 |
l0File = new TFile(fname.Data()); |
| 784 |
if ( !l0File ) { |
| 785 |
if ( debug ) printf(" OrbitalInfo - ERROR: problems opening Level0 file\n"); |
| 786 |
code = -6; |
| 787 |
goto closeandexit; |
| 788 |
}; |
| 789 |
l0tr = (TTree*)l0File->Get("Physics"); |
| 790 |
if ( !l0tr ) { |
| 791 |
if ( debug ) printf(" OrbitalInfo - ERROR: no Physics tree in Level0 file\n"); |
| 792 |
l0File->Close(); |
| 793 |
code = -7; |
| 794 |
goto closeandexit; |
| 795 |
}; |
| 796 |
// EM: open header branch as well |
| 797 |
l0head = l0tr->GetBranch("Header"); |
| 798 |
if ( !l0head ) { |
| 799 |
if ( debug ) printf(" OrbitalInfo - ERROR: no Header branch in Level0 tree\n"); |
| 800 |
l0File->Close(); |
| 801 |
code = -8; |
| 802 |
goto closeandexit; |
| 803 |
}; |
| 804 |
l0tr->SetBranchAddress("Header", &eh); |
| 805 |
// end EM |
| 806 |
nevents = l0head->GetEntries(); |
| 807 |
// |
| 808 |
if ( nevents < 1 && totevent ) { |
| 809 |
if ( debug ) printf(" OrbitalInfo - ERROR: Level0 file is empty\n\n"); |
| 810 |
l0File->Close(); |
| 811 |
code = -11; |
| 812 |
goto closeandexit; |
| 813 |
}; |
| 814 |
// |
| 815 |
if ( runinfo->EV_TO > nevents-1 && totevent ) { |
| 816 |
if ( debug ) printf(" OrbitalInfo - ERROR: too few entries in the registry tree\n"); |
| 817 |
l0File->Close(); |
| 818 |
code = -12; |
| 819 |
goto closeandexit; |
| 820 |
}; |
| 821 |
|
| 822 |
// |
| 823 |
// open IGRF files and do it only once if we are processing a full level2 file |
| 824 |
// |
| 825 |
if ( !igrfloaded ){ |
| 826 |
|
| 827 |
if ( l0head->GetEntry(runinfo->EV_FROM) > 0 ){ |
| 828 |
igrfloaded = true; |
| 829 |
// |
| 830 |
// absolute time of first event of the run (it should not matter a lot) |
| 831 |
// |
| 832 |
ph = eh->GetPscuHeader(); |
| 833 |
atime = dbtime->DBabsTime(ph->GetOrbitalTime()); |
| 834 |
|
| 835 |
parerror=glparam->Query_GL_PARAM(atime-anni5,301,dbc); // parameters stored in DB in GL_PRAM table |
| 836 |
if ( parerror<0 ) { |
| 837 |
code = parerror; |
| 838 |
goto closeandexit; |
| 839 |
} |
| 840 |
ltp1 = (Int_t)(glparam->PATH+glparam->NAME).Length(); |
| 841 |
if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam->PATH+glparam->NAME).Data()); |
| 842 |
// |
| 843 |
parerror=glparam2->Query_GL_PARAM(atime,301,dbc); // parameters stored in DB in GL_PRAM table |
| 844 |
if ( parerror<0 ) { |
| 845 |
code = parerror; |
| 846 |
goto closeandexit; |
| 847 |
} |
| 848 |
ltp2 = (Int_t)(glparam2->PATH+glparam2->NAME).Length(); |
| 849 |
if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam2->PATH+glparam2->NAME).Data()); |
| 850 |
// |
| 851 |
parerror=glparam3->Query_GL_PARAM(atime,302,dbc); // parameters stored in DB in GL_PRAM table |
| 852 |
if ( parerror<0 ) { |
| 853 |
code = parerror; |
| 854 |
goto closeandexit; |
| 855 |
} |
| 856 |
ltp3 = (Int_t)(glparam3->PATH+glparam3->NAME).Length(); |
| 857 |
if ( verbose ) printf(" Reading Earth's Magnetic Field parameter file: %s \n",(glparam3->PATH+glparam3->NAME).Data()); |
| 858 |
// |
| 859 |
initize_((char *)(glparam->PATH+glparam->NAME).Data(),<p1,(char *)(glparam2->PATH+glparam2->NAME).Data(),<p2,(char *)(glparam3->PATH+glparam3->NAME).Data(),<p3); |
| 860 |
// |
| 861 |
if (debug) cout<<"initize: "<<(char *)(glparam->PATH+glparam->NAME).Data()<<"\t"<<(char *)(glparam2->PATH+glparam2->NAME).Data()<<"\t"<<(char *)(glparam3->PATH+glparam3->NAME).Data()<<endl; |
| 862 |
} |
| 863 |
} |
| 864 |
// |
| 865 |
// End IGRF stuff// |
| 866 |
// |
| 867 |
|
| 868 |
ULong_t TimeSync = (ULong_t)dbtime->GetTimesync(); |
| 869 |
ULong_t ObtSync = (ULong_t)(dbtime->GetObt0()/1000); |
| 870 |
ULong_t DeltaOBT = TimeSync - ObtSync; |
| 871 |
|
| 872 |
if ( debug ) printf(" 2 TimeSync %lu ObtSync %lu DeltaOBT %lu\n",(ULong_t)(dbtime->GetTimesync()/1000),(ULong_t)dbtime->GetObt0(),TimeSync-ObtSync); |
| 873 |
// |
| 874 |
// Read MCMDs from up to 11 files, 5 before and 5 after the present one in order to have some kind of inclination information |
| 875 |
// |
| 876 |
ch = new TChain("Mcmd","Mcmd"); |
| 877 |
// |
| 878 |
// look in the DB to find the closest files to this run |
| 879 |
// |
| 880 |
TSQLResult *pResult = 0; |
| 881 |
TSQLRow *Row = 0; |
| 882 |
stringstream myquery; |
| 883 |
UInt_t l0fid[10]; |
| 884 |
Int_t i = 0; |
| 885 |
memset(l0fid,0,10*sizeof(Int_t)); |
| 886 |
// |
| 887 |
myquery.str(""); |
| 888 |
myquery << "select ID_ROOT_L0 from GL_RUN where RUNHEADER_TIME<=" << runinfo->RUNHEADER_TIME << " group by ID_ROOT_L0 order by RUNHEADER_TIME desc limit 5;"; |
| 889 |
// |
| 890 |
pResult = dbc->Query(myquery.str().c_str()); |
| 891 |
// |
| 892 |
i = 9; |
| 893 |
if( pResult ){ |
| 894 |
// |
| 895 |
Row = pResult->Next(); |
| 896 |
// |
| 897 |
while ( Row ){ |
| 898 |
// |
| 899 |
// store infos and exit |
| 900 |
// |
| 901 |
l0fid[i] = (UInt_t)atoll(Row->GetField(0)); |
| 902 |
i--; |
| 903 |
Row = pResult->Next(); |
| 904 |
// |
| 905 |
}; |
| 906 |
pResult->Delete(); |
| 907 |
}; |
| 908 |
// |
| 909 |
myquery.str(""); |
| 910 |
myquery << "select ID_ROOT_L0 from GL_RUN where RUNHEADER_TIME>" << runinfo->RUNHEADER_TIME << " group by ID_ROOT_L0 order by RUNHEADER_TIME asc limit 5;"; |
| 911 |
// |
| 912 |
pResult = dbc->Query(myquery.str().c_str()); |
| 913 |
// |
| 914 |
i = 0; |
| 915 |
if( pResult ){ |
| 916 |
// |
| 917 |
Row = pResult->Next(); |
| 918 |
// |
| 919 |
while ( Row ){ |
| 920 |
// |
| 921 |
// store infos and exit |
| 922 |
// |
| 923 |
l0fid[i] = (UInt_t)atoll(Row->GetField(0)); |
| 924 |
i++; |
| 925 |
Row = pResult->Next(); |
| 926 |
// |
| 927 |
}; |
| 928 |
pResult->Delete(); |
| 929 |
}; |
| 930 |
// |
| 931 |
i = 0; |
| 932 |
UInt_t previd = 0; |
| 933 |
while ( i < 10 ){ |
| 934 |
if ( l0fid[i] && previd != l0fid[i] ){ |
| 935 |
previd = l0fid[i]; |
| 936 |
myquery.str(""); |
| 937 |
myquery << "select PATH,NAME from GL_ROOT where ID=" << l0fid[i] << " ;"; |
| 938 |
// |
| 939 |
pResult = dbc->Query(myquery.str().c_str()); |
| 940 |
// |
| 941 |
if( pResult ){ |
| 942 |
// |
| 943 |
Row = pResult->Next(); |
| 944 |
// |
| 945 |
if ( debug ) printf(" Using inclination informations from file: %s \n",(((TString)gSystem->ExpandPathName(Row->GetField(0)))+"/"+(TString)Row->GetField(1)).Data()); |
| 946 |
ch->Add(((TString)gSystem->ExpandPathName(Row->GetField(0)))+"/"+(TString)Row->GetField(1)); |
| 947 |
// |
| 948 |
pResult->Delete(); |
| 949 |
}; |
| 950 |
}; |
| 951 |
i++; |
| 952 |
}; |
| 953 |
// |
| 954 |
ch->SetBranchAddress("Mcmd",&mcmdev); |
| 955 |
neventsm = ch->GetEntries(); |
| 956 |
if ( debug ) printf(" entries %u \n", neventsm); |
| 957 |
// |
| 958 |
if (neventsm == 0){ |
| 959 |
if ( debug ) printf("InclinationInfo - WARNING: No quaternions in this File"); |
| 960 |
code = 900; |
| 961 |
} |
| 962 |
// |
| 963 |
Double_t lowerqtime = 0; |
| 964 |
// |
| 965 |
// init quaternions information from mcmd-packets |
| 966 |
// |
| 967 |
Bool_t isf = true; |
| 968 |
|
| 969 |
vector<Float_t> q0; |
| 970 |
vector<Float_t> q1; |
| 971 |
vector<Float_t> q2; |
| 972 |
vector<Float_t> q3; |
| 973 |
vector<Double_t> qtime; |
| 974 |
vector<Float_t> qPitch; |
| 975 |
vector<Float_t> qRoll; |
| 976 |
vector<Float_t> qYaw; |
| 977 |
vector<Int_t> qmode; |
| 978 |
|
| 979 |
Int_t nt = 0; |
| 980 |
UInt_t must = 0; |
| 981 |
|
| 982 |
// |
| 983 |
// run over all the events of the run |
| 984 |
// |
| 985 |
if (verbose) printf("\n Ready to start! \n\n Processed events: \n\n"); |
| 986 |
// |
| 987 |
// |
| 988 |
for ( re = runinfo->EV_FROM; re < (runinfo->EV_FROM+runinfo->NEVENTS); re++){ |
| 989 |
// |
| 990 |
if ( procev%1000 == 0 && procev > 0 && verbose ) printf(" %iK \n",procev/1000); |
| 991 |
if ( debug ) printf(" %i \n",procev); |
| 992 |
// |
| 993 |
if ( l0head->GetEntry(re) <= 0 ) throw -36; |
| 994 |
// |
| 995 |
// absolute time of this event |
| 996 |
// |
| 997 |
ph = eh->GetPscuHeader(); |
| 998 |
atime = dbtime->DBabsTime(ph->GetOrbitalTime()); |
| 999 |
if ( debug ) printf(" %i absolute time \n",procev); |
| 1000 |
// |
| 1001 |
// paranoid check |
| 1002 |
// |
| 1003 |
if ( (atime > (runinfo->RUNTRAILER_TIME+1)) || (atime < (runinfo->RUNHEADER_TIME-1)) ) { |
| 1004 |
if (verbose) printf(" OrbitalInfo - WARNING: event at time outside the run time window, skipping it\n"); |
| 1005 |
jumped++; |
| 1006 |
// debug = true; |
| 1007 |
continue; |
| 1008 |
} |
| 1009 |
|
| 1010 |
// |
| 1011 |
// retrieve tof informations |
| 1012 |
// |
| 1013 |
if ( !reprocall ){ |
| 1014 |
itr = nobefrun + (re - evfrom - jumped); |
| 1015 |
//itr = re-(46438+200241); |
| 1016 |
} else { |
| 1017 |
itr = runinfo->GetFirstEntry() + (re - evfrom - jumped); |
| 1018 |
}; |
| 1019 |
// |
| 1020 |
if ( !standalone ){ |
| 1021 |
if ( itr > nevtofl2 ){ |
| 1022 |
if ( verbose ) printf(" OrbitalInfo - ERROR: no tof events with entry = %i in Level2 file\n",itr); |
| 1023 |
if ( debug ) printf(" nobefrun %u re %u evfrom %u jumped %u reprocall %i \n",nobefrun,re,evfrom,jumped,reprocall); |
| 1024 |
l0File->Close(); |
| 1025 |
code = -904; |
| 1026 |
goto closeandexit; |
| 1027 |
}; |
| 1028 |
// |
| 1029 |
tof->Clear(); |
| 1030 |
// |
| 1031 |
// Clones array must be cleared before going on |
| 1032 |
// |
| 1033 |
if ( hasNucleiTof ){ |
| 1034 |
tcNucleiTof->Delete(); |
| 1035 |
} |
| 1036 |
if ( hasExtNucleiTof ){ |
| 1037 |
tcExtNucleiTof->Delete(); |
| 1038 |
} |
| 1039 |
if ( hasExtTof ){ |
| 1040 |
tcExtTof->Delete(); |
| 1041 |
} |
| 1042 |
// |
| 1043 |
if ( verbose ) printf(" get tof tree entries... entry = %i in Level2 file\n",itr); |
| 1044 |
if ( ttof->GetEntry(itr) <= 0 ){ |
| 1045 |
if ( verbose ) printf(" problems with tof tree entries... entry = %i in Level2 file\n",itr); |
| 1046 |
if ( verbose ) printf(" nobefrun %u re %u evfrom %u jumped %u reprocall %i \n",nobefrun,re,evfrom,jumped,reprocall); |
| 1047 |
throw -36; |
| 1048 |
} |
| 1049 |
if ( verbose ) printf(" gat0\n"); |
| 1050 |
// |
| 1051 |
} |
| 1052 |
// |
| 1053 |
// retrieve tracker informations |
| 1054 |
// |
| 1055 |
if ( !standalone ){ |
| 1056 |
if ( itr > nevtrkl2 ){ |
| 1057 |
if ( verbose ) printf(" OrbitalInfo - ERROR: no trk events with entry = %i in Level2 file\n",itr); |
| 1058 |
if ( debug ) printf(" nobefrun %u re %u evfrom %u jumped %u reprocall %i \n",nobefrun,re,evfrom,jumped,reprocall); |
| 1059 |
l0File->Close(); |
| 1060 |
code = -905; |
| 1061 |
goto closeandexit; |
| 1062 |
} |
| 1063 |
// |
| 1064 |
if ( verbose ) printf(" gat1\n"); |
| 1065 |
trke->Clear(); |
| 1066 |
// |
| 1067 |
// Clones array must be cleared before going on |
| 1068 |
// |
| 1069 |
if ( hasNucleiTrk ){ |
| 1070 |
if ( verbose ) printf(" gat2\n"); |
| 1071 |
tcNucleiTrk->Delete(); |
| 1072 |
if ( verbose ) printf(" gat3\n"); |
| 1073 |
torbNucleiTrk->Delete(); |
| 1074 |
} |
| 1075 |
if ( hasExtNucleiTrk ){ |
| 1076 |
if ( verbose ) printf(" gat4\n"); |
| 1077 |
tcExtNucleiTrk->Delete(); |
| 1078 |
if ( verbose ) printf(" gat5\n"); |
| 1079 |
torbExtNucleiTrk->Delete(); |
| 1080 |
} |
| 1081 |
if ( hasExtTrk ){ |
| 1082 |
if ( verbose ) printf(" gat6\n"); |
| 1083 |
tcExtTrk->Delete(); |
| 1084 |
if ( verbose ) printf(" gat7\n"); |
| 1085 |
torbExtTrk->Delete(); |
| 1086 |
} |
| 1087 |
// |
| 1088 |
if ( verbose ) printf(" get trk tree entries... entry = %i in Level2 file\n",itr); |
| 1089 |
if ( ttrke->GetEntry(itr) <= 0 ) throw -36; |
| 1090 |
// |
| 1091 |
} |
| 1092 |
|
| 1093 |
// |
| 1094 |
procev++; |
| 1095 |
// |
| 1096 |
// start processing |
| 1097 |
// |
| 1098 |
if ( debug ) printf(" %i start processing \n",procev); |
| 1099 |
orbitalinfo->Clear(); |
| 1100 |
// |
| 1101 |
OrbitalInfoTrkVar *t_orb = new OrbitalInfoTrkVar(); |
| 1102 |
if( !(orbitalinfo->OrbitalInfoTrk) ) orbitalinfo->OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); |
| 1103 |
TClonesArray &tor = *orbitalinfo->OrbitalInfoTrk; |
| 1104 |
|
| 1105 |
// Geomagnetic coordinates calculation variables |
| 1106 |
GMtype_CoordSpherical CoordSpherical, DipoleSpherical; |
| 1107 |
GMtype_CoordCartesian CoordCartesian, DipoleCartesian; |
| 1108 |
GMtype_Model Model; |
| 1109 |
GMtype_Pole Pole; |
| 1110 |
|
| 1111 |
// |
| 1112 |
// Fill OBT, pkt_num and absTime |
| 1113 |
// |
| 1114 |
orbitalinfo->pkt_num = ph->GetCounter(); |
| 1115 |
orbitalinfo->OBT = ph->GetOrbitalTime(); |
| 1116 |
orbitalinfo->absTime = atime; |
| 1117 |
if ( debug ) printf(" %i pktnum obt abstime \n",procev); |
| 1118 |
// |
| 1119 |
// Propagate the orbit from the tle time to atime, using SGP(D)4. |
| 1120 |
// |
| 1121 |
if ( debug ) printf(" %i sgp4 \n",procev); |
| 1122 |
cCoordGeo coo; |
| 1123 |
Float_t jyear=0.; |
| 1124 |
// |
| 1125 |
if(atime >= gltle->GetToTime()) { |
| 1126 |
if ( !gltle->Query(atime, dbc) ){ |
| 1127 |
// |
| 1128 |
// Compute the magnetic dipole moment. |
| 1129 |
// |
| 1130 |
if ( debug ) printf(" %i compute magnetic dipole moment \n",procev); |
| 1131 |
UInt_t year, month, day, hour, min, sec; |
| 1132 |
// |
| 1133 |
TTimeStamp t = TTimeStamp(atime, kTRUE); |
| 1134 |
t.GetDate(kTRUE, 0, &year, &month, &day); |
| 1135 |
t.GetTime(kTRUE, 0, &hour, &min, &sec); |
| 1136 |
jyear = (float) year |
| 1137 |
+ (month*31.+ (float) day)/365. |
| 1138 |
+ (hour*3600.+min*60.+(float)sec)/(24.*3600.*365.); |
| 1139 |
// |
| 1140 |
if ( debug ) printf(" %i compute magnetic dipole moment get dipole moment for year\n",procev); |
| 1141 |
if ( debug ) printf(" %i jyear %f dimo %f \n",procev,jyear,dimo); |
| 1142 |
feldcof_(&jyear, &dimo); // get dipole moment for year |
| 1143 |
if ( debug ) printf(" %i compute magnetic dipole moment end\n",procev); |
| 1144 |
|
| 1145 |
GM_TimeAdjustCoefs(year, jyear, G0, G1, H1, &Model); |
| 1146 |
GM_PoleLocation(Model, &Pole); |
| 1147 |
|
| 1148 |
} else { |
| 1149 |
code = -56; |
| 1150 |
goto closeandexit; |
| 1151 |
}; |
| 1152 |
} |
| 1153 |
coo = getCoo(atime, gltle->GetFromTime(), gltle->GetTle()); |
| 1154 |
// |
| 1155 |
cOrbit orbits(*gltle->GetTle()); |
| 1156 |
// |
| 1157 |
// synchronize with quaternions data |
| 1158 |
// |
| 1159 |
if ( isf && neventsm>0 ){ |
| 1160 |
// |
| 1161 |
// First event |
| 1162 |
// |
| 1163 |
isf = false; |
| 1164 |
// upperqtime = atime; |
| 1165 |
lowerqtime = runinfo->RUNHEADER_TIME; |
| 1166 |
for ( ik = 0; ik < neventsm; ik++){ //number of macrocommad packets |
| 1167 |
if ( ch->GetEntry(ik) <= 0 ) throw -36; |
| 1168 |
tmpSize = mcmdev->Records->GetEntries(); |
| 1169 |
// numrec = tmpSize; |
| 1170 |
if ( debug ) cout << "packet number " << ik <<"\tnumber of subpackets is " << tmpSize << endl; |
| 1171 |
for (Int_t j3 = 0;j3<tmpSize;j3++){ //number of subpackets |
| 1172 |
mcmdrc = (pamela::McmdRecord*)mcmdev->Records->At(j3); |
| 1173 |
if ( mcmdrc ){ // missing inclination bug [8RED 090116] |
| 1174 |
if ( debug ) printf(" pluto \n"); |
| 1175 |
if ((int)mcmdrc->ID1 == 226 && mcmdrc->Mcmd_Block_crc_ok == 1){ //Check that it is Inclination Packet |
| 1176 |
L_QQ_Q_l_upper->fill(mcmdrc->McmdData); |
| 1177 |
for (UInt_t ui = 0; ui < 6; ui++){ |
| 1178 |
if (ui>0){ |
| 1179 |
if (L_QQ_Q_l_upper->time[ui]>L_QQ_Q_l_upper->time[0]){ |
| 1180 |
if ( debug ) printf(" here1 %i \n",ui); |
| 1181 |
Double_t u_time = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[ui]*1000-DeltaOBT*1000)); |
| 1182 |
Int_t recSize = recqtime.size(); |
| 1183 |
if(lowerqtime > recqtime[recSize-1]){ |
| 1184 |
// to avoid interpolation between bad quaternions arrays |
| 1185 |
if(sqrt(pow(L_QQ_Q_l_upper->quat[ui][0],2)+pow(L_QQ_Q_l_upper->quat[ui][1],2)+pow(L_QQ_Q_l_upper->quat[ui][2],2)+pow(L_QQ_Q_l_upper->quat[ui][3],2))>0.99999){ |
| 1186 |
Int_t sizeqmcmd = qtime.size(); |
| 1187 |
inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw); |
| 1188 |
qtime[sizeqmcmd]=u_time; |
| 1189 |
q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][0]; |
| 1190 |
q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][1]; |
| 1191 |
q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][2]; |
| 1192 |
q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][3]; |
| 1193 |
qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui); |
| 1194 |
lowerqtime = u_time; |
| 1195 |
orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi); |
| 1196 |
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]); |
| 1197 |
qRoll[sizeqmcmd]=RYPang_upper->Kren; |
| 1198 |
qYaw[sizeqmcmd]=RYPang_upper->Ryskanie; |
| 1199 |
qPitch[sizeqmcmd]=RYPang_upper->Tangazh; |
| 1200 |
} |
| 1201 |
} |
| 1202 |
for(Int_t mu = nt;mu<recSize;mu++){ |
| 1203 |
if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){ |
| 1204 |
if(sqrt(pow(recq0[mu],2)+pow(recq1[mu],2)+pow(recq2[mu],2)+pow(recq3[mu],2))>0.99999){ |
| 1205 |
nt=mu; |
| 1206 |
Int_t sizeqmcmd = qtime.size(); |
| 1207 |
inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw); |
| 1208 |
qtime[sizeqmcmd]=recqtime[mu]; |
| 1209 |
q0[sizeqmcmd]=recq0[mu]; |
| 1210 |
q1[sizeqmcmd]=recq1[mu]; |
| 1211 |
q2[sizeqmcmd]=recq2[mu]; |
| 1212 |
q3[sizeqmcmd]=recq3[mu]; |
| 1213 |
qmode[sizeqmcmd]=-10; |
| 1214 |
orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi); |
| 1215 |
RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,recq0[mu],recq1[mu],recq2[mu],recq3[mu]); |
| 1216 |
qRoll[sizeqmcmd]=RYPang_upper->Kren; |
| 1217 |
qYaw[sizeqmcmd]=RYPang_upper->Ryskanie; |
| 1218 |
qPitch[sizeqmcmd]=RYPang_upper->Tangazh; |
| 1219 |
} |
| 1220 |
} |
| 1221 |
if(recqtime[mu]>=u_time){ |
| 1222 |
if(sqrt(pow(L_QQ_Q_l_upper->quat[ui][0],2)+pow(L_QQ_Q_l_upper->quat[ui][1],2)+pow(L_QQ_Q_l_upper->quat[ui][2],2)+pow(L_QQ_Q_l_upper->quat[ui][3],2))>0.99999){ |
| 1223 |
Int_t sizeqmcmd = qtime.size(); |
| 1224 |
inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw); |
| 1225 |
qtime[sizeqmcmd]=u_time; |
| 1226 |
q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][0]; |
| 1227 |
q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][1]; |
| 1228 |
q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][2]; |
| 1229 |
q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[ui][3]; |
| 1230 |
qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui); |
| 1231 |
lowerqtime = u_time; |
| 1232 |
orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi); |
| 1233 |
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]); |
| 1234 |
qRoll[sizeqmcmd]=RYPang_upper->Kren; |
| 1235 |
qYaw[sizeqmcmd]=RYPang_upper->Ryskanie; |
| 1236 |
qPitch[sizeqmcmd]=RYPang_upper->Tangazh; |
| 1237 |
break; |
| 1238 |
} |
| 1239 |
} |
| 1240 |
} |
| 1241 |
} |
| 1242 |
}else{ |
| 1243 |
if ( debug ) printf(" here2 %i \n",ui); |
| 1244 |
Double_t u_time = dbtime->DBabsTime((UInt_t)(L_QQ_Q_l_upper->time[0]*1000-DeltaOBT*1000)); |
| 1245 |
if(lowerqtime>u_time)nt=0; |
| 1246 |
Int_t recSize = recqtime.size(); |
| 1247 |
if(lowerqtime > recqtime[recSize-1]){ |
| 1248 |
if(sqrt(pow(L_QQ_Q_l_upper->quat[ui][0],2)+pow(L_QQ_Q_l_upper->quat[ui][1],2)+pow(L_QQ_Q_l_upper->quat[ui][2],2)+pow(L_QQ_Q_l_upper->quat[ui][3],2))>0.99999){ |
| 1249 |
Int_t sizeqmcmd = qtime.size(); |
| 1250 |
inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw); |
| 1251 |
qtime[sizeqmcmd]=u_time; |
| 1252 |
q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][0]; |
| 1253 |
q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][1]; |
| 1254 |
q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][2]; |
| 1255 |
q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][3]; |
| 1256 |
qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui); |
| 1257 |
lowerqtime = u_time; |
| 1258 |
orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi); |
| 1259 |
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]); |
| 1260 |
qRoll[sizeqmcmd]=RYPang_upper->Kren; |
| 1261 |
qYaw[sizeqmcmd]=RYPang_upper->Ryskanie; |
| 1262 |
qPitch[sizeqmcmd]=RYPang_upper->Tangazh; |
| 1263 |
} |
| 1264 |
} |
| 1265 |
for(Int_t mu = nt;mu<recSize;mu++){ |
| 1266 |
if(recqtime[mu]>lowerqtime && recqtime[mu]<u_time){ |
| 1267 |
if(sqrt(pow(recq0[mu],2)+pow(recq1[mu],2)+pow(recq2[mu],2)+pow(recq3[mu],2))>0.99999){ |
| 1268 |
nt=mu; |
| 1269 |
Int_t sizeqmcmd = qtime.size(); |
| 1270 |
inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw); |
| 1271 |
qtime[sizeqmcmd]=recqtime[mu]; |
| 1272 |
q0[sizeqmcmd]=recq0[mu]; |
| 1273 |
q1[sizeqmcmd]=recq1[mu]; |
| 1274 |
q2[sizeqmcmd]=recq2[mu]; |
| 1275 |
q3[sizeqmcmd]=recq3[mu]; |
| 1276 |
qmode[sizeqmcmd]=-10; |
| 1277 |
orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi); |
| 1278 |
RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,recq0[mu],recq1[mu],recq2[mu],recq3[mu]); |
| 1279 |
qRoll[sizeqmcmd]=RYPang_upper->Kren; |
| 1280 |
qYaw[sizeqmcmd]=RYPang_upper->Ryskanie; |
| 1281 |
qPitch[sizeqmcmd]=RYPang_upper->Tangazh; |
| 1282 |
} |
| 1283 |
} |
| 1284 |
if(recqtime[mu]>=u_time){ |
| 1285 |
if(sqrt(pow(L_QQ_Q_l_upper->quat[0][0],2)+pow(L_QQ_Q_l_upper->quat[0][1],2)+pow(L_QQ_Q_l_upper->quat[0][2],2)+pow(L_QQ_Q_l_upper->quat[0][3],2))>0.99999){ |
| 1286 |
Int_t sizeqmcmd = qtime.size(); |
| 1287 |
inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw); |
| 1288 |
qtime[sizeqmcmd]=u_time; |
| 1289 |
q0[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][0]; |
| 1290 |
q1[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][1]; |
| 1291 |
q2[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][2]; |
| 1292 |
q3[sizeqmcmd]=L_QQ_Q_l_upper->quat[0][3]; |
| 1293 |
qmode[sizeqmcmd]=holeq(lowerqtime,qtime[sizeqmcmd],L_QQ_Q_l_lower,L_QQ_Q_l_upper,ui); |
| 1294 |
lowerqtime = u_time; |
| 1295 |
orbits.getPosition((double) (u_time - gltle->GetFromTime())/60., &eCi); |
| 1296 |
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]); |
| 1297 |
qRoll[sizeqmcmd]=RYPang_upper->Kren; |
| 1298 |
qYaw[sizeqmcmd]=RYPang_upper->Ryskanie; |
| 1299 |
qPitch[sizeqmcmd]=RYPang_upper->Tangazh; |
| 1300 |
CopyQ(L_QQ_Q_l_lower,L_QQ_Q_l_upper); |
| 1301 |
break; |
| 1302 |
} |
| 1303 |
} |
| 1304 |
} |
| 1305 |
} |
| 1306 |
} |
| 1307 |
} |
| 1308 |
} |
| 1309 |
//if ( debug ) cout << "subpacket " << j3 << "\t qtime = " << qtime[qtime.size()-1] << endl; |
| 1310 |
} |
| 1311 |
} |
| 1312 |
|
| 1313 |
if(qtime.size()==0){ // in case if no orientation information in data |
| 1314 |
if ( debug ) cout << "qtime.size() = 0" << endl; |
| 1315 |
for(UInt_t my=0;my<recqtime.size();my++){ |
| 1316 |
if(sqrt(pow(recq0[my],2)+pow(recq1[my],2)+pow(recq2[my],2)+pow(recq3[my],2))>0.99999){ |
| 1317 |
Int_t sizeqmcmd = qtime.size(); |
| 1318 |
inclresize(qtime,q0,q1,q2,q3,qmode,qRoll,qPitch,qYaw); |
| 1319 |
qtime[sizeqmcmd]=recqtime[my]; |
| 1320 |
q0[sizeqmcmd]=recq0[my]; |
| 1321 |
q1[sizeqmcmd]=recq1[my]; |
| 1322 |
q2[sizeqmcmd]=recq2[my]; |
| 1323 |
q3[sizeqmcmd]=recq3[my]; |
| 1324 |
qmode[sizeqmcmd]=-10; |
| 1325 |
orbits.getPosition((double) (qtime[sizeqmcmd] - gltle->GetFromTime())/60., &eCi); |
| 1326 |
RYPang_upper->TransAngle(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,recq0[my],recq1[my],recq2[my],recq3[my]); |
| 1327 |
qRoll[sizeqmcmd]=RYPang_upper->Kren; |
| 1328 |
qYaw[sizeqmcmd]=RYPang_upper->Ryskanie; |
| 1329 |
qPitch[sizeqmcmd]=RYPang_upper->Tangazh; |
| 1330 |
} |
| 1331 |
} |
| 1332 |
} |
| 1333 |
|
| 1334 |
|
| 1335 |
if ( debug ) printf(" puffi \n"); |
| 1336 |
Double_t tmin = 9999999999.; |
| 1337 |
Double_t tmax = 0.; |
| 1338 |
for(UInt_t tre = 0;tre<qtime.size();tre++){ |
| 1339 |
if(qtime[tre]>tmax)tmax = qtime[tre]; |
| 1340 |
if(qtime[tre]<tmin)tmin = qtime[tre]; |
| 1341 |
} |
| 1342 |
// sorting quaternions by time |
| 1343 |
Bool_t t = true; |
| 1344 |
while(t){ |
| 1345 |
t=false; |
| 1346 |
for(UInt_t i=0;i<qtime.size()-1;i++){ |
| 1347 |
if(qtime[i]>qtime[i+1]){ |
| 1348 |
Double_t tmpr = qtime[i]; |
| 1349 |
qtime[i]=qtime[i+1]; |
| 1350 |
qtime[i+1] = tmpr; |
| 1351 |
tmpr = q0[i]; |
| 1352 |
q0[i]=q0[i+1]; |
| 1353 |
q0[i+1] = tmpr; |
| 1354 |
tmpr = q1[i]; |
| 1355 |
q1[i]=q1[i+1]; |
| 1356 |
q1[i+1] = tmpr; |
| 1357 |
tmpr = q2[i]; |
| 1358 |
q2[i]=q2[i+1]; |
| 1359 |
q2[i+1] = tmpr; |
| 1360 |
tmpr = q3[i]; |
| 1361 |
q3[i]=q3[i+1]; |
| 1362 |
q3[i+1] = tmpr; |
| 1363 |
tmpr = qRoll[i]; |
| 1364 |
qRoll[i]=qRoll[i+1]; |
| 1365 |
qRoll[i+1] = tmpr; |
| 1366 |
tmpr = qYaw[i]; |
| 1367 |
qYaw[i]=qYaw[i+1]; |
| 1368 |
qYaw[i+1] = tmpr; |
| 1369 |
tmpr = qPitch[i]; |
| 1370 |
qPitch[i]=qPitch[i+1]; |
| 1371 |
qPitch[i+1] = tmpr; |
| 1372 |
t=true; |
| 1373 |
} |
| 1374 |
} |
| 1375 |
} |
| 1376 |
|
| 1377 |
if ( debug ){ |
| 1378 |
cout << "we have loaded quaternions: size of quaternions set is "<< qtime.size() << endl; |
| 1379 |
for(UInt_t i=0;i<qtime.size();i++) cout << qtime[i] << "\t"; |
| 1380 |
cout << endl << endl; |
| 1381 |
Int_t lopu; |
| 1382 |
cin >> lopu; |
| 1383 |
} |
| 1384 |
|
| 1385 |
} // if we processed first event |
| 1386 |
|
| 1387 |
|
| 1388 |
//Filling Inclination information |
| 1389 |
Double_t incli = 0; |
| 1390 |
if ( qtime.size() > 1 ){ |
| 1391 |
if ( debug ) cout << "ok quaternions is exist and mu = " << must << endl; |
| 1392 |
if ( debug ) cout << "qtimes[ " << qtime[0] << " , " << qtime[qtime.size()-1] << " ]\tatime = "<<atime<<endl; |
| 1393 |
for(UInt_t mu = must;mu<qtime.size()-1;mu++){ |
| 1394 |
if ( debug ) printf(" ??grfuffi %i sixe %i must %i \n",mu,qtime.size()-1,must); |
| 1395 |
if(qtime[mu+1]>qtime[mu]){ |
| 1396 |
if ( debug ) cout << "qtime[" << mu << "] = " << qtime[mu] << "\tqtime[" << mu+1 << "] = " << qtime[mu+1] << "\tatime = " << atime << endl; |
| 1397 |
if(atime<=qtime[mu+1] && atime>=qtime[mu]){ |
| 1398 |
if ( debug ) cout << "here we have found proper quaternions for interpolation: mu = "<<mu<<endl; |
| 1399 |
must = mu; |
| 1400 |
incli = (qPitch[mu+1]-qPitch[mu])/(qtime[mu+1]-qtime[mu]); |
| 1401 |
orbitalinfo->theta = incli*atime+qPitch[mu+1]-incli*qtime[mu+1]; |
| 1402 |
incli = (qRoll[mu+1]-qRoll[mu])/(qtime[mu+1]-qtime[mu]); |
| 1403 |
orbitalinfo->etha = incli*atime+qRoll[mu+1]-incli*qtime[mu+1]; |
| 1404 |
incli = (qYaw[mu+1]-qYaw[mu])/(qtime[mu+1]-qtime[mu]); |
| 1405 |
orbitalinfo->phi = incli*atime+qYaw[mu+1]-incli*qtime[mu+1]; |
| 1406 |
|
| 1407 |
incli = (q0[mu+1]-q0[mu])/(qtime[mu+1]-qtime[mu]); |
| 1408 |
orbitalinfo->q0 = incli*atime+q0[mu+1]-incli*qtime[mu+1]; |
| 1409 |
incli = (q1[mu+1]-q1[mu])/(qtime[mu+1]-qtime[mu]); |
| 1410 |
orbitalinfo->q1 = incli*atime+q1[mu+1]-incli*qtime[mu+1]; |
| 1411 |
incli = (q2[mu+1]-q2[mu])/(qtime[mu+1]-qtime[mu]); |
| 1412 |
orbitalinfo->q2 = incli*atime+q2[mu+1]-incli*qtime[mu+1]; |
| 1413 |
incli = (q3[mu+1]-q3[mu])/(qtime[mu+1]-qtime[mu]); |
| 1414 |
orbitalinfo->q3 = incli*atime+q3[mu+1]-incli*qtime[mu+1]; |
| 1415 |
Float_t tg = (qtime[mu+1]-qtime[mu])/1000.0; |
| 1416 |
if(tg>=1) tg=0.00; |
| 1417 |
orbitalinfo->TimeGap = TMath::Min(TMath::Abs(qtime[mu+1])-atime,TMath::Abs(atime-qtime[mu]))+tg;//qtime[mu+1]-qtime[mu]; |
| 1418 |
orbitalinfo->mode = qmode[mu+1]; |
| 1419 |
//if(atime==qtime[mu] || atime==qtime[mu+1]) orbitalinfo->qkind = 0; else orbitalinfo->qkind=1; |
| 1420 |
//if(qmode[mu+1]==-10) orbitalinfo->R10r = true;else orbitalinfo->R10r = false; |
| 1421 |
if ( debug ) printf(" grfuffi4 %i \n",mu); |
| 1422 |
break; |
| 1423 |
} |
| 1424 |
} |
| 1425 |
} |
| 1426 |
} |
| 1427 |
if ( debug ) printf(" grfuffi5 \n"); |
| 1428 |
// |
| 1429 |
// ops no inclination information |
| 1430 |
// |
| 1431 |
|
| 1432 |
if ( orbitalinfo->q0< -999 || orbitalinfo->q1 < -999 || orbitalinfo->q2 < -999 || orbitalinfo->q3 < -999 || orbitalinfo->q0 != orbitalinfo->q0 || orbitalinfo->q1 != orbitalinfo->q1 || orbitalinfo->q2 != orbitalinfo->q2 || orbitalinfo->q3 != orbitalinfo->q3 ){ |
| 1433 |
if ( debug ) cout << "ops no iclination information" << endl; |
| 1434 |
orbitalinfo->mode = 10; |
| 1435 |
orbitalinfo->q0 = -1000.; |
| 1436 |
orbitalinfo->q1 = -1000.; |
| 1437 |
orbitalinfo->q2 = -1000.; |
| 1438 |
orbitalinfo->q3 = -1000.; |
| 1439 |
orbitalinfo->etha = -1000.; |
| 1440 |
orbitalinfo->phi = -1000.; |
| 1441 |
orbitalinfo->theta = -1000.; |
| 1442 |
orbitalinfo->TimeGap = -1000.; |
| 1443 |
//orbitalinfo->qkind = -1000; |
| 1444 |
|
| 1445 |
// if ( debug ){ |
| 1446 |
// Int_t lopu; |
| 1447 |
// cin >> lopu; |
| 1448 |
// } |
| 1449 |
if ( debug ) printf(" grfuffi6 \n"); |
| 1450 |
} |
| 1451 |
// |
| 1452 |
if ( debug ) printf(" filling \n"); |
| 1453 |
// ######################################################################################################################### |
| 1454 |
// |
| 1455 |
// fill orbital positions |
| 1456 |
// |
| 1457 |
// Build coordinates in the right range. We want to convert, |
| 1458 |
// longitude from (0, 2*pi) to (-180deg, 180deg). Altitude is |
| 1459 |
// in meters. |
| 1460 |
lon = (coo.m_Lon > M_PI) ? rad2deg(coo.m_Lon - 2*M_PI) : rad2deg(coo.m_Lon); |
| 1461 |
lat = rad2deg(coo.m_Lat); |
| 1462 |
alt = coo.m_Alt; |
| 1463 |
|
| 1464 |
cOrbit orbits2(*gltle->GetTle()); |
| 1465 |
orbits2.getPosition((double) (atime - gltle->GetFromTime())/60., &eCi); |
| 1466 |
// Float_t x=eCi.getPos().m_x; |
| 1467 |
// Float_t y=eCi.getPos().m_y; |
| 1468 |
// Float_t z=eCi.getPos().m_z; |
| 1469 |
|
| 1470 |
TVector3 V(eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z); |
| 1471 |
TVector3 Pos(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z); |
| 1472 |
|
| 1473 |
Float_t dlon=Pos.Phi()*TMath::RadToDeg()-lon; |
| 1474 |
|
| 1475 |
Pos.RotateZ(-dlon*TMath::DegToRad()); |
| 1476 |
V.RotateZ(-dlon*TMath::DegToRad()); |
| 1477 |
Float_t diro; |
| 1478 |
if(V.Z()>0) diro=1; else diro=-1; |
| 1479 |
|
| 1480 |
// 10REDNEW |
| 1481 |
Int_t errq=0; |
| 1482 |
Int_t azim=0; |
| 1483 |
Int_t MU=0; |
| 1484 |
for(UInt_t mu = must;mu<RTtime2.size()-1;mu++){ |
| 1485 |
if(atime<=RTstart[mu+1] && atime>=RTstart[mu]){ |
| 1486 |
errq=RTerrq[mu]; |
| 1487 |
azim=RTazim[mu]; |
| 1488 |
MU=mu; |
| 1489 |
break; |
| 1490 |
} |
| 1491 |
} |
| 1492 |
orbitalinfo->errq = errq; |
| 1493 |
orbitalinfo->azim = azim; |
| 1494 |
orbitalinfo->qkind = 0; |
| 1495 |
|
| 1496 |
if ( debug ) printf(" coord done \n"); |
| 1497 |
if( lon<180 && lon>-180 && lat<90 && lat>-90 && alt>0 ){ |
| 1498 |
// |
| 1499 |
orbitalinfo->lon = lon; |
| 1500 |
orbitalinfo->lat = lat; |
| 1501 |
orbitalinfo->alt = alt; |
| 1502 |
orbitalinfo->V = V; |
| 1503 |
|
| 1504 |
// GMtype_CoordGeodetic location; |
| 1505 |
location.lambda = lon; |
| 1506 |
location.phi = lat; |
| 1507 |
location.HeightAboveEllipsoid = alt; |
| 1508 |
|
| 1509 |
GM_GeodeticToSpherical(Ellip, location, &CoordSpherical); |
| 1510 |
GM_SphericalToCartesian(CoordSpherical, &CoordCartesian); |
| 1511 |
GM_EarthCartToDipoleCartCD(Pole, CoordCartesian, &DipoleCartesian); |
| 1512 |
GM_CartesianToSpherical(DipoleCartesian, &DipoleSpherical); |
| 1513 |
orbitalinfo->londip = DipoleSpherical.lambda; |
| 1514 |
orbitalinfo->latdip = DipoleSpherical.phig; |
| 1515 |
|
| 1516 |
if(debug)cout<<"geodetic:\t"<<lon<<"\t"<<lat<<"\tgeomagnetic:\t"<<orbitalinfo->londip<<"\t"<<orbitalinfo->latdip<<endl; |
| 1517 |
|
| 1518 |
// |
| 1519 |
// compute mag field components and L shell. |
| 1520 |
// |
| 1521 |
if ( debug ) printf(" call igrf feldg \n"); |
| 1522 |
feldg_(&lat, &lon, &alt, &bnorth, &beast, &bdown, &babs); |
| 1523 |
if ( debug ) printf(" call igrf shellg \n"); |
| 1524 |
shellg_(&lat, &lon, &alt, &dimo, &xl, &icode, &bab1); |
| 1525 |
if ( debug ) printf(" call igrf findb \n"); |
| 1526 |
findb0_(&stps, &bdel, &value, &bequ, &rr0); |
| 1527 |
// |
| 1528 |
if ( debug ) printf(" done igrf \n"); |
| 1529 |
orbitalinfo->Bnorth = bnorth; |
| 1530 |
orbitalinfo->Beast = beast; |
| 1531 |
orbitalinfo->Bdown = bdown; |
| 1532 |
orbitalinfo->Babs = babs; |
| 1533 |
orbitalinfo->M = dimo; |
| 1534 |
orbitalinfo->BB0 = babs/bequ; |
| 1535 |
orbitalinfo->L = xl; |
| 1536 |
// Set Stormer vertical cutoff using L shell. |
| 1537 |
orbitalinfo->cutoffsvl = 14.295 / (xl*xl); // |
| 1538 |
if(debug)cout << "L = " << xl << "\tM = " << dimo << "\tvertical cutoff: "<< orbitalinfo->cutoffsvl << endl; |
| 1539 |
|
| 1540 |
/* |
| 1541 |
---------- Forwarded message ---------- |
| 1542 |
Date: Wed, 09 May 2012 12:16:47 +0200 |
| 1543 |
From: Alessandro Bruno <alessandro.bruno@ba.infn.it> |
| 1544 |
To: Mirko Boezio <mirko.boezio@ts.infn.it> |
| 1545 |
Cc: Francesco S. Cafagna <Francesco.Cafagna@ba.infn.it> |
| 1546 |
Subject: Störmer vertical cutoff |
| 1547 |
|
| 1548 |
Ciao Mirko, |
| 1549 |
volevo segnalarti che il valore dello Störmer vertical cutoff nel Level2 è |
| 1550 |
sovrastimato di circa il 4%. |
| 1551 |
Dopo un'approfondita analisi con l'IGRF-05 abbiamo ricavano un valore pari |
| 1552 |
a: 14.295 / L^2 anzichè 14.9 / L^2, valore obsoleto in quanto riferito agli |
| 1553 |
anni '50. |
| 1554 |
*/ |
| 1555 |
//14.9/(xl*xl); |
| 1556 |
orbitalinfo->igrf_icode = icode; |
| 1557 |
// |
| 1558 |
} |
| 1559 |
// |
| 1560 |
if ( debug ) printf(" pitch angle \n"); |
| 1561 |
// |
| 1562 |
// pitch angles |
| 1563 |
// |
| 1564 |
if( orbitalinfo->TimeGap>0){ |
| 1565 |
// |
| 1566 |
if ( debug ) printf(" timegap %f \n",orbitalinfo->TimeGap); |
| 1567 |
Float_t Bx = -orbitalinfo->Bdown; |
| 1568 |
Float_t By = orbitalinfo->Beast; |
| 1569 |
Float_t Bz = orbitalinfo->Bnorth; |
| 1570 |
|
| 1571 |
TMatrixD Qiji(3,3); |
| 1572 |
TMatrixD Qij = PO->QuatoECI(orbitalinfo->q0,orbitalinfo->q1,orbitalinfo->q2,orbitalinfo->q3); |
| 1573 |
TMatrixD Dij = PO->ECItoGEO(Qij,orbitalinfo->absTime,orbitalinfo->lat,orbitalinfo->lon); |
| 1574 |
|
| 1575 |
//10REDNEW |
| 1576 |
/* If initial orientation data have reason to be inaccurate */ |
| 1577 |
Float_t tg = 0.00; |
| 1578 |
Float_t tmptg; |
| 1579 |
if(MU!=0){ |
| 1580 |
// if(orbitalinfo->TimeGap>0 && errq==0 && azim==0){ // 10RED CHECK (comparison between three metod of recovering orientation) |
| 1581 |
if((atime>=RTstart[MU] && atime<RTstart[MU+1] && RTbank1[MU]==0 && RTbank2[MU]==0 && TMath::Abs(orbitalinfo->etha)>0.01) || ((RTbank1[MU]!=0 || RTbank2[MU]!=0) && atime>=RTstart[MU] && atime<RTstart[MU+1] && azim==0 && (errq!=0 || orbitalinfo->TimeGap>10.0 || ((modf(orbitalinfo->TimeGap,&tmptg)*1000>10 || modf(orbitalinfo->TimeGap,&tmptg)*1000==0.0) && orbitalinfo->TimeGap>2.0)))){ |
| 1582 |
/* found in Rotation Table this data for this time interval*/ |
| 1583 |
if(atime<RTtime1[0]) |
| 1584 |
orbitalinfo->azim = 5; //means that RotationTable no started yet |
| 1585 |
else{ |
| 1586 |
// search for angle betwean velosity and direction to north in tangential to Earth surfase plane in satellite position |
| 1587 |
Double_t bank=RTstart[MU]; |
| 1588 |
Double_t tlat=orbitalinfo->lat; |
| 1589 |
|
| 1590 |
tg=modf(orbitalinfo->TimeGap,&tg)*1000; |
| 1591 |
|
| 1592 |
if(atime>=RTpluto1[MU] && atime<=RTpluto2[MU]){ |
| 1593 |
Double_t kar=(RTbank2[MU]-RTbank1[MU])/(RTtime2[MU]-RTtime1[MU]); |
| 1594 |
Double_t bak=RTbank1[MU]-kar*RTtime1[MU]; |
| 1595 |
bank=kar*atime+bak; |
| 1596 |
} |
| 1597 |
if(atime>=RTstart[MU] && atime<RTpluto1[MU]){ |
| 1598 |
Double_t s_dBdt2=(RTbpluto1[MU]-RTbank1[MU])/(RTpluto1[MU]-RTstart[MU]); |
| 1599 |
Double_t s_t2=((Double_t)RTpluto1[MU]+(Double_t)RTstart[MU])/2. - RTstart[MU]; |
| 1600 |
Double_t s_t1=RTstart[MU]-RTstart[MU]; |
| 1601 |
Double_t s_k=s_dBdt2/(s_t2-s_t1); |
| 1602 |
Double_t s_b=-s_k*s_t1; |
| 1603 |
Double_t s_t3=RTpluto1[MU]-RTstart[MU]; |
| 1604 |
Double_t s_b3=RTbpluto1[MU]; |
| 1605 |
Double_t s_c=s_b3-0.5*s_k*s_t3*s_t3 -s_b*s_t3; |
| 1606 |
bank=0.5*s_k*(atime-RTstart[MU])*(atime-RTstart[MU]) + s_b*(atime-RTstart[MU]) + s_c; |
| 1607 |
} |
| 1608 |
if(atime>RTpluto2[MU] && atime<=RTstart[MU+1]){ |
| 1609 |
Double_t s_dBdt2=(RTbpluto2[MU] - RTbank2[MU])/(RTpluto2[MU]-RTstart[MU+1]); |
| 1610 |
Double_t s_t2=((Double_t)RTpluto2[MU]+(Double_t)RTstart[MU+1])/2. - RTstart[MU]; |
| 1611 |
Double_t s_t1=RTstart[MU+1]-RTstart[MU]; |
| 1612 |
Double_t s_k=s_dBdt2/(s_t2-s_t1); |
| 1613 |
Double_t s_b=-s_k*s_t1; |
| 1614 |
Double_t s_t3=RTpluto2[MU]-RTstart[MU]; |
| 1615 |
Double_t s_b3=RTbpluto2[MU]; |
| 1616 |
Double_t s_c=s_b3-0.5*s_k*s_t3*s_t3 -s_b*s_t3; |
| 1617 |
bank=0.5*s_k*(atime-RTstart[MU])*(atime-RTstart[MU]) + s_b*(atime-RTstart[MU]) + s_c; |
| 1618 |
} |
| 1619 |
orbitalinfo->etha=bank; |
| 1620 |
Double_t spitch = 0.00001; // temprary not zero to avoid problem with tranzition from Euler angles to orientation matrix |
| 1621 |
|
| 1622 |
//Estimations of pitch angle of satellite |
| 1623 |
if(TMath::Abs(bank)>0.7){ |
| 1624 |
Float_t spitch1=TMath::DegToRad()*0.7*diro;//RTdir1[MU]; |
| 1625 |
Float_t spitch2=TMath::DegToRad()*0.7*diro;//RTdir2[MU]; |
| 1626 |
Float_t kva=(spitch2-spitch1)/(RTtime2[MU]-RTtime1[MU]); |
| 1627 |
Float_t bva=spitch1-kva*RTtime1[MU]; |
| 1628 |
spitch=kva*atime+bva; |
| 1629 |
} |
| 1630 |
|
| 1631 |
//Calculate Yaw angle accordingly with fit, see picture FitYaw.jpg |
| 1632 |
Double_t yaw=0.00001; // temprary not zero to avoid problem with tranzition from Euler angles to orientation matrix |
| 1633 |
if(TMath::Abs(tlat)<70) |
| 1634 |
yaw = -3.7e-8*tlat*tlat*tlat*tlat + 1.4e-7*tlat*tlat*tlat - 0.0005*tlat*tlat - 0.00025*tlat + 3.6; |
| 1635 |
yaw = diro*yaw; //because should be different sign for ascending and descending orbits! |
| 1636 |
orbitalinfo->phi=yaw; |
| 1637 |
|
| 1638 |
if(TMath::Abs(bank)>0.5 && TMath::Abs(yaw-orbitalinfo->phi)<3.0) yaw=orbitalinfo->phi; |
| 1639 |
|
| 1640 |
// Qiji = PO->EulertoEci(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,bank,yaw,spitch); // 10RED CHECK |
| 1641 |
Qij = PO->EulertoEci(eCi.getPos().m_x,eCi.getPos().m_y,eCi.getPos().m_z,eCi.getVel().m_x,eCi.getVel().m_y,eCi.getVel().m_z,bank,yaw,spitch); // STANDARD |
| 1642 |
orbitalinfo->qkind = 1; |
| 1643 |
|
| 1644 |
//Qij = PO->GEOtoECI(Dij,orbitalinfo->absTime,orbitalinfo->lat,orbitalinfo->lon); // to convert from Dij to Qij |
| 1645 |
|
| 1646 |
} // end of if(atime<RTtime1[0] |
| 1647 |
} // end of f(((orbitalinfo->TimeGap>60.0 && TMath... |
| 1648 |
} // end of MU~=0 |
| 1649 |
|
| 1650 |
TMatrixD qij = PO->ColPermutation(Qij); |
| 1651 |
TMatrixD Fij = PO->ECItoGreenwich(Qij,orbitalinfo->absTime); |
| 1652 |
TMatrixD Gij = PO->ColPermutation(Fij); |
| 1653 |
Dij = PO->ECItoGEO(Qij,orbitalinfo->absTime,orbitalinfo->lat,orbitalinfo->lon); |
| 1654 |
TMatrixD Iij = PO->ColPermutation(Dij); |
| 1655 |
TVector3 SP = PO->GetSunPosition(orbitalinfo->absTime); |
| 1656 |
// go to Pamela reference frame from Resurs reference frame |
| 1657 |
Float_t tmpy = SP.Y(); |
| 1658 |
SP.SetY(SP.Z()); |
| 1659 |
SP.SetZ(-tmpy); |
| 1660 |
TVector3 SunZenith; |
| 1661 |
SunZenith.SetMagThetaPhi(1,23.439281*TMath::DegToRad(),TMath::Pi()/2.); |
| 1662 |
TVector3 SunMag = -SP; |
| 1663 |
SunMag.Rotate(-45*TMath::DegToRad(),SunZenith); |
| 1664 |
tmpy=SunMag.Y(); |
| 1665 |
SunMag.SetY(SunMag.Z()); |
| 1666 |
SunMag.SetZ(-tmpy); |
| 1667 |
|
| 1668 |
orbitalinfo->Iij.ResizeTo(Iij); |
| 1669 |
orbitalinfo->Iij = Iij; |
| 1670 |
// |
| 1671 |
// A1 = Iij(0,2); |
| 1672 |
// A2 = Iij(1,2); |
| 1673 |
// A3 = Iij(2,2); |
| 1674 |
// |
| 1675 |
// orbitalinfo->pamzenitangle = (Float_t)PO->GetPitchAngle(1,0,0,A1,A2,A3); // Angle between zenit and Pamela's main axiz |
| 1676 |
// orbitalinfo->pamBangle = (Float_t)PO->GetPitchAngle(A1,A2,A3,Bx,By,Bz); // Angle between Pamela's main axiz and B |
| 1677 |
// |
| 1678 |
if ( debug ) printf(" matrixes done \n"); |
| 1679 |
if ( !standalone ){ |
| 1680 |
if ( debug ) printf(" !standalone \n"); |
| 1681 |
// |
| 1682 |
// Standard tracking algorithm |
| 1683 |
// |
| 1684 |
Int_t nn = 0; |
| 1685 |
if ( verbose ) printf(" standard tracking \n"); |
| 1686 |
for(Int_t nt=0; nt < tof->ntrk(); nt++){ |
| 1687 |
// |
| 1688 |
ToFTrkVar *ptt = tof->GetToFTrkVar(nt); |
| 1689 |
if (debug) cout<<"tof->ntrk() = "<<tof->ntrk()<<"\tptt->trkseqno = "<<ptt->trkseqno<<"\ttrke->ntrk() = "<<trke->ntrk()<<endl; |
| 1690 |
Double_t E11x = ptt->xtr_tof[0]; // tr->x[0]; |
| 1691 |
Double_t E11y = ptt->ytr_tof[0]; //tr->y[0]; |
| 1692 |
Double_t E11z = zin[0]; |
| 1693 |
Double_t E22x = ptt->xtr_tof[3];//tr->x[3]; |
| 1694 |
Double_t E22y = ptt->ytr_tof[3];//tr->y[3]; |
| 1695 |
Double_t E22z = zin[3]; |
| 1696 |
if ( (E11x < 100. && E11y < 100. && E22x < 100. && E22y < 100.) || ptt->trkseqno != -1 ){ |
| 1697 |
TrkTrack *mytrack = trke->GetStoredTrack(ptt->trkseqno); |
| 1698 |
Float_t rig=1/mytrack->GetDeflection(); |
| 1699 |
Double_t norm = sqrt(pow(E22x-E11x,2)+pow(E22y-E11y,2)+pow(E22z-E11z,2)); |
| 1700 |
// |
| 1701 |
Px = (E22x-E11x)/norm; |
| 1702 |
Py = (E22y-E11y)/norm; |
| 1703 |
Pz = (E22z-E11z)/norm; |
| 1704 |
// |
| 1705 |
t_orb->trkseqno = ptt->trkseqno; |
| 1706 |
// |
| 1707 |
TMatrixD Eij = PO->PamelatoGEO(Iij,Px,Py,Pz); |
| 1708 |
t_orb->Eij.ResizeTo(Eij); |
| 1709 |
t_orb->Eij = Eij; |
| 1710 |
// |
| 1711 |
TMatrixD Sij = PO->PamelatoGEO(Gij,Px,Py,Pz); |
| 1712 |
t_orb->Sij.ResizeTo(Sij); |
| 1713 |
t_orb->Sij = Sij; |
| 1714 |
// |
| 1715 |
t_orb->pitch = (Float_t)PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),Bx,By,Bz); |
| 1716 |
// |
| 1717 |
// SunPosition in instrumental reference frame |
| 1718 |
TMatrixD Kij = PO->PamelatoGEO(qij,Px,Py,Pz); |
| 1719 |
TMatrixD Lij = PO->PamelatoGEO(qij,0,0,1); |
| 1720 |
t_orb->sunangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),-SP.X(),-SP.Y(),-SP.Z()); |
| 1721 |
t_orb->sunmagangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),SunMag.X(),SunMag.Y(),SunMag.Z()); |
| 1722 |
// |
| 1723 |
// |
| 1724 |
Double_t omega = PO->GetPitchAngle(-Eij(0,0),-Eij(1,0),-Eij(2,0),1,0,0) * TMath::DegToRad(); |
| 1725 |
TVector3 Bxy(0,By,Bz); |
| 1726 |
TVector3 Exy(0,-Eij(1,0),-Eij(2,0)); |
| 1727 |
Double_t dzeta=Bxy.Angle(Exy); |
| 1728 |
if (-Eij(1,0) < 0) dzeta=2.0*TMath::Pi() - dzeta; |
| 1729 |
|
| 1730 |
if(debug) cout << "omega = "<<omega*TMath::RadToDeg()<<"\tdzeta = "<<dzeta*TMath::RadToDeg()<<endl; |
| 1731 |
|
| 1732 |
// Formula from D.F. Smart *, M.A. Shea [2005]; A review of geomagnetic cutoff rigidities for earth-orbiting spacecraft |
| 1733 |
if(rig>=0) t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2)); |
| 1734 |
else t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(TMath::Pi()+dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2)); |
| 1735 |
if (debug) cout << "R = " << rig << "\tcutoff = " << t_orb->cutoff << endl; |
| 1736 |
|
| 1737 |
// |
| 1738 |
if ( t_orb->pitch != t_orb->pitch ) t_orb->pitch = -1000.; |
| 1739 |
if ( t_orb->cutoff != t_orb->cutoff ) t_orb->cutoff = -1000.; |
| 1740 |
if ( t_orb->sunangle != t_orb->sunangle ) t_orb->sunangle = -1000.; |
| 1741 |
if ( t_orb->sunmagangle != t_orb->sunmagangle ) t_orb->sunmagangle = -1000.; |
| 1742 |
// |
| 1743 |
if ( debug ) printf(" orbitalinfo->cutoffsvl %f vitaly %f \n",orbitalinfo->cutoffsvl,t_orb->cutoff); |
| 1744 |
// |
| 1745 |
new(tor[nn]) OrbitalInfoTrkVar(*t_orb); |
| 1746 |
nn++; |
| 1747 |
// |
| 1748 |
t_orb->Clear(); |
| 1749 |
// |
| 1750 |
} |
| 1751 |
// |
| 1752 |
} // end standard tracking algorithm |
| 1753 |
|
| 1754 |
// |
| 1755 |
// Code for extended tracking algorithm: |
| 1756 |
// |
| 1757 |
if ( hasNucleiTrk ){ |
| 1758 |
Int_t ttentry = 0; |
| 1759 |
if ( verbose ) printf(" hasNucleiTrk \n"); |
| 1760 |
for(Int_t nt=0; nt < tcNucleiTof->GetEntries() ; nt++){ |
| 1761 |
// |
| 1762 |
if ( verbose ) printf(" got1\n"); |
| 1763 |
ToFTrkVar *ptt = (ToFTrkVar*)(tcNucleiTof->At(nt)); |
| 1764 |
if (verbose) cout<<" tcNucleiTof->GetEntries() = "<<tcNucleiTof->GetEntries()<<"\tptt->trkseqno = "<<ptt->trkseqno<<endl; |
| 1765 |
Double_t E11x = ptt->xtr_tof[0]; // tr->x[0]; |
| 1766 |
Double_t E11y = ptt->ytr_tof[0]; //tr->y[0]; |
| 1767 |
Double_t E11z = zin[0]; |
| 1768 |
Double_t E22x = ptt->xtr_tof[3];//tr->x[3]; |
| 1769 |
Double_t E22y = ptt->ytr_tof[3];//tr->y[3]; |
| 1770 |
Double_t E22z = zin[3]; |
| 1771 |
if ( (E11x < 100. && E11y < 100. && E22x < 100. && E22y < 100.) || ptt->trkseqno != -1 ){ |
| 1772 |
TrkTrack *mytrack = (TrkTrack*)(tcNucleiTrk->At(ptt->trkseqno)); |
| 1773 |
if ( verbose ) printf(" got tcNucleiTrk \n"); |
| 1774 |
Float_t rig=1/mytrack->GetDeflection(); |
| 1775 |
Double_t norm = sqrt(pow(E22x-E11x,2)+pow(E22y-E11y,2)+pow(E22z-E11z,2)); |
| 1776 |
// |
| 1777 |
Px = (E22x-E11x)/norm; |
| 1778 |
Py = (E22y-E11y)/norm; |
| 1779 |
Pz = (E22z-E11z)/norm; |
| 1780 |
// |
| 1781 |
t_orb->trkseqno = ptt->trkseqno; |
| 1782 |
// |
| 1783 |
TMatrixD Eij = PO->PamelatoGEO(Iij,Px,Py,Pz); |
| 1784 |
t_orb->Eij.ResizeTo(Eij); |
| 1785 |
t_orb->Eij = Eij; |
| 1786 |
// |
| 1787 |
TMatrixD Sij = PO->PamelatoGEO(Gij,Px,Py,Pz); |
| 1788 |
t_orb->Sij.ResizeTo(Sij); |
| 1789 |
t_orb->Sij = Sij; |
| 1790 |
// |
| 1791 |
t_orb->pitch = (Float_t)PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),Bx,By,Bz); |
| 1792 |
// |
| 1793 |
// SunPosition in instrumental reference frame |
| 1794 |
TMatrixD Kij = PO->PamelatoGEO(qij,Px,Py,Pz); |
| 1795 |
TMatrixD Lij = PO->PamelatoGEO(qij,0,0,1); |
| 1796 |
t_orb->sunangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),-SP.X(),-SP.Y(),-SP.Z()); |
| 1797 |
t_orb->sunmagangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),SunMag.X(),SunMag.Y(),SunMag.Z()); |
| 1798 |
// |
| 1799 |
// |
| 1800 |
Double_t omega = PO->GetPitchAngle(-Eij(0,0),-Eij(1,0),-Eij(2,0),1,0,0) * TMath::DegToRad(); |
| 1801 |
TVector3 Bxy(0,By,Bz); |
| 1802 |
TVector3 Exy(0,-Eij(1,0),-Eij(2,0)); |
| 1803 |
Double_t dzeta=Bxy.Angle(Exy); |
| 1804 |
if (-Eij(1,0) < 0) dzeta=2.0*TMath::Pi() - dzeta; |
| 1805 |
|
| 1806 |
if(debug) cout << "omega = "<<omega*TMath::RadToDeg()<<"\tdzeta = "<<dzeta*TMath::RadToDeg()<<endl; |
| 1807 |
|
| 1808 |
// Formula from D.F. Smart *, M.A. Shea [2005]; A review of geomagnetic cutoff rigidities for earth-orbiting spacecraft |
| 1809 |
if(rig>=0) t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2)); |
| 1810 |
else t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(TMath::Pi()+dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2)); |
| 1811 |
if (debug) cout << "R = " << rig << "\tcutoff = " << t_orb->cutoff << endl; |
| 1812 |
|
| 1813 |
// |
| 1814 |
if ( t_orb->pitch != t_orb->pitch ) t_orb->pitch = -1000.; |
| 1815 |
if ( t_orb->cutoff != t_orb->cutoff ) t_orb->cutoff = -1000.; |
| 1816 |
if ( t_orb->sunangle != t_orb->sunangle ) t_orb->sunangle = -1000.; |
| 1817 |
if ( t_orb->sunmagangle != t_orb->sunmagangle ) t_orb->sunmagangle = -1000.; |
| 1818 |
// |
| 1819 |
if ( debug ) printf(" orbitalinfo->cutoffsvl %f vitaly %f \n",orbitalinfo->cutoffsvl,t_orb->cutoff); |
| 1820 |
// |
| 1821 |
TClonesArray &tt1 = *torbNucleiTrk; |
| 1822 |
new(tt1[ttentry]) OrbitalInfoTrkVar(*t_orb); |
| 1823 |
ttentry++; |
| 1824 |
// |
| 1825 |
t_orb->Clear(); |
| 1826 |
// |
| 1827 |
} |
| 1828 |
// |
| 1829 |
} |
| 1830 |
} // end standard tracking algorithm: nuclei |
| 1831 |
if ( hasExtNucleiTrk ){ |
| 1832 |
Int_t ttentry = 0; |
| 1833 |
if ( verbose ) printf(" hasExtNucleiTrk \n"); |
| 1834 |
for(Int_t nt=0; nt < tcExtNucleiTof->GetEntries() ; nt++){ |
| 1835 |
// |
| 1836 |
if ( verbose ) printf(" got2\n"); |
| 1837 |
ToFTrkVar *ptt = (ToFTrkVar*)(tcExtNucleiTof->At(nt)); |
| 1838 |
if (verbose) cout<<" tcExtNucleiTof->GetEntries() = "<<tcExtNucleiTof->GetEntries()<<"\tptt->trkseqno = "<<ptt->trkseqno<<endl; |
| 1839 |
Double_t E11x = ptt->xtr_tof[0]; // tr->x[0]; |
| 1840 |
Double_t E11y = ptt->ytr_tof[0]; //tr->y[0]; |
| 1841 |
Double_t E11z = zin[0]; |
| 1842 |
Double_t E22x = ptt->xtr_tof[3];//tr->x[3]; |
| 1843 |
Double_t E22y = ptt->ytr_tof[3];//tr->y[3]; |
| 1844 |
Double_t E22z = zin[3]; |
| 1845 |
if ( (E11x < 100. && E11y < 100. && E22x < 100. && E22y < 100.) || ptt->trkseqno != -1 ){ |
| 1846 |
ExtTrack *mytrack = (ExtTrack*)(tcExtNucleiTrk->At(ptt->trkseqno)); |
| 1847 |
if ( verbose ) printf(" got tcExtNucleiTrk \n"); |
| 1848 |
Float_t rig=1/mytrack->GetDeflection(); |
| 1849 |
Double_t norm = sqrt(pow(E22x-E11x,2)+pow(E22y-E11y,2)+pow(E22z-E11z,2)); |
| 1850 |
// |
| 1851 |
Px = (E22x-E11x)/norm; |
| 1852 |
Py = (E22y-E11y)/norm; |
| 1853 |
Pz = (E22z-E11z)/norm; |
| 1854 |
// |
| 1855 |
t_orb->trkseqno = ptt->trkseqno; |
| 1856 |
// |
| 1857 |
TMatrixD Eij = PO->PamelatoGEO(Iij,Px,Py,Pz); |
| 1858 |
t_orb->Eij.ResizeTo(Eij); |
| 1859 |
t_orb->Eij = Eij; |
| 1860 |
// |
| 1861 |
TMatrixD Sij = PO->PamelatoGEO(Gij,Px,Py,Pz); |
| 1862 |
t_orb->Sij.ResizeTo(Sij); |
| 1863 |
t_orb->Sij = Sij; |
| 1864 |
// |
| 1865 |
t_orb->pitch = (Float_t)PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),Bx,By,Bz); |
| 1866 |
// |
| 1867 |
// SunPosition in instrumental reference frame |
| 1868 |
TMatrixD Kij = PO->PamelatoGEO(qij,Px,Py,Pz); |
| 1869 |
TMatrixD Lij = PO->PamelatoGEO(qij,0,0,1); |
| 1870 |
t_orb->sunangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),-SP.X(),-SP.Y(),-SP.Z()); |
| 1871 |
t_orb->sunmagangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),SunMag.X(),SunMag.Y(),SunMag.Z()); |
| 1872 |
// |
| 1873 |
// |
| 1874 |
Double_t omega = PO->GetPitchAngle(-Eij(0,0),-Eij(1,0),-Eij(2,0),1,0,0) * TMath::DegToRad(); |
| 1875 |
TVector3 Bxy(0,By,Bz); |
| 1876 |
TVector3 Exy(0,-Eij(1,0),-Eij(2,0)); |
| 1877 |
Double_t dzeta=Bxy.Angle(Exy); |
| 1878 |
if (-Eij(1,0) < 0) dzeta=2.0*TMath::Pi() - dzeta; |
| 1879 |
|
| 1880 |
if(debug) cout << "omega = "<<omega*TMath::RadToDeg()<<"\tdzeta = "<<dzeta*TMath::RadToDeg()<<endl; |
| 1881 |
|
| 1882 |
// Formula from D.F. Smart *, M.A. Shea [2005]; A review of geomagnetic cutoff rigidities for earth-orbiting spacecraft |
| 1883 |
if(rig>=0) t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2)); |
| 1884 |
else t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(TMath::Pi()+dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2)); |
| 1885 |
if (debug) cout << "R = " << rig << "\tcutoff = " << t_orb->cutoff << endl; |
| 1886 |
|
| 1887 |
// |
| 1888 |
if ( t_orb->pitch != t_orb->pitch ) t_orb->pitch = -1000.; |
| 1889 |
if ( t_orb->cutoff != t_orb->cutoff ) t_orb->cutoff = -1000.; |
| 1890 |
if ( t_orb->sunangle != t_orb->sunangle ) t_orb->sunangle = -1000.; |
| 1891 |
if ( t_orb->sunmagangle != t_orb->sunmagangle ) t_orb->sunmagangle = -1000.; |
| 1892 |
// |
| 1893 |
if ( debug ) printf(" orbitalinfo->cutoffsvl %f vitaly %f \n",orbitalinfo->cutoffsvl,t_orb->cutoff); |
| 1894 |
// |
| 1895 |
TClonesArray &tt2 = *torbExtNucleiTrk; |
| 1896 |
new(tt2[ttentry]) OrbitalInfoTrkVar(*t_orb); |
| 1897 |
ttentry++; |
| 1898 |
// |
| 1899 |
t_orb->Clear(); |
| 1900 |
// |
| 1901 |
} |
| 1902 |
// |
| 1903 |
} |
| 1904 |
} // end standard tracking algorithm: nuclei extended |
| 1905 |
if ( hasExtTrk ){ |
| 1906 |
Int_t ttentry = 0; |
| 1907 |
if ( verbose ) printf(" hasExtTrk \n"); |
| 1908 |
for(Int_t nt=0; nt < tcExtTof->GetEntries() ; nt++){ |
| 1909 |
// |
| 1910 |
if ( verbose ) printf(" got3\n"); |
| 1911 |
ToFTrkVar *ptt = (ToFTrkVar*)(tcExtTof->At(nt)); |
| 1912 |
if (verbose) cout<<" tcExtTof->GetEntries() = "<<tcExtTof->GetEntries()<<"\tptt->trkseqno = "<<ptt->trkseqno<<endl; |
| 1913 |
Double_t E11x = ptt->xtr_tof[0]; // tr->x[0]; |
| 1914 |
Double_t E11y = ptt->ytr_tof[0]; //tr->y[0]; |
| 1915 |
Double_t E11z = zin[0]; |
| 1916 |
Double_t E22x = ptt->xtr_tof[3];//tr->x[3]; |
| 1917 |
Double_t E22y = ptt->ytr_tof[3];//tr->y[3]; |
| 1918 |
Double_t E22z = zin[3]; |
| 1919 |
if ( (E11x < 100. && E11y < 100. && E22x < 100. && E22y < 100.) || ptt->trkseqno != -1 ){ |
| 1920 |
ExtTrack *mytrack = (ExtTrack*)(tcExtTrk->At(ptt->trkseqno)); |
| 1921 |
if ( verbose ) printf(" got tcExtTrk \n"); |
| 1922 |
Float_t rig=1/mytrack->GetDeflection(); |
| 1923 |
Double_t norm = sqrt(pow(E22x-E11x,2)+pow(E22y-E11y,2)+pow(E22z-E11z,2)); |
| 1924 |
// |
| 1925 |
Px = (E22x-E11x)/norm; |
| 1926 |
Py = (E22y-E11y)/norm; |
| 1927 |
Pz = (E22z-E11z)/norm; |
| 1928 |
// |
| 1929 |
t_orb->trkseqno = ptt->trkseqno; |
| 1930 |
// |
| 1931 |
TMatrixD Eij = PO->PamelatoGEO(Iij,Px,Py,Pz); |
| 1932 |
t_orb->Eij.ResizeTo(Eij); |
| 1933 |
t_orb->Eij = Eij; |
| 1934 |
// |
| 1935 |
TMatrixD Sij = PO->PamelatoGEO(Gij,Px,Py,Pz); |
| 1936 |
t_orb->Sij.ResizeTo(Sij); |
| 1937 |
t_orb->Sij = Sij; |
| 1938 |
// |
| 1939 |
t_orb->pitch = (Float_t)PO->GetPitchAngle(Eij(0,0),Eij(1,0),Eij(2,0),Bx,By,Bz); |
| 1940 |
// |
| 1941 |
// SunPosition in instrumental reference frame |
| 1942 |
TMatrixD Kij = PO->PamelatoGEO(qij,Px,Py,Pz); |
| 1943 |
TMatrixD Lij = PO->PamelatoGEO(qij,0,0,1); |
| 1944 |
t_orb->sunangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),-SP.X(),-SP.Y(),-SP.Z()); |
| 1945 |
t_orb->sunmagangle=(Float_t)PO->GetPitchAngle(Kij(0,0),Kij(1,0),Kij(2,0),SunMag.X(),SunMag.Y(),SunMag.Z()); |
| 1946 |
// |
| 1947 |
// |
| 1948 |
Double_t omega = PO->GetPitchAngle(-Eij(0,0),-Eij(1,0),-Eij(2,0),1,0,0) * TMath::DegToRad(); |
| 1949 |
TVector3 Bxy(0,By,Bz); |
| 1950 |
TVector3 Exy(0,-Eij(1,0),-Eij(2,0)); |
| 1951 |
Double_t dzeta=Bxy.Angle(Exy); |
| 1952 |
if (-Eij(1,0) < 0) dzeta=2.0*TMath::Pi() - dzeta; |
| 1953 |
|
| 1954 |
if(debug) cout << "omega = "<<omega*TMath::RadToDeg()<<"\tdzeta = "<<dzeta*TMath::RadToDeg()<<endl; |
| 1955 |
|
| 1956 |
// Formula from D.F. Smart *, M.A. Shea [2005]; A review of geomagnetic cutoff rigidities for earth-orbiting spacecraft |
| 1957 |
if(rig>=0) t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2)); |
| 1958 |
else t_orb->cutoff = 59.3/(pow(orbitalinfo->L,2)*pow(1+sqrt(1-sin(omega)*sin(TMath::Pi()+dzeta)*pow(cos(orbitalinfo->lat*TMath::DegToRad()),3)),2)); |
| 1959 |
if (debug) cout << "R = " << rig << "\tcutoff = " << t_orb->cutoff << endl; |
| 1960 |
|
| 1961 |
// |
| 1962 |
if ( t_orb->pitch != t_orb->pitch ) t_orb->pitch = -1000.; |
| 1963 |
if ( t_orb->cutoff != t_orb->cutoff ) t_orb->cutoff = -1000.; |
| 1964 |
if ( t_orb->sunangle != t_orb->sunangle ) t_orb->sunangle = -1000.; |
| 1965 |
if ( t_orb->sunmagangle != t_orb->sunmagangle ) t_orb->sunmagangle = -1000.; |
| 1966 |
// |
| 1967 |
if ( debug ) printf(" orbitalinfo->cutoffsvl %f vitaly %f \n",orbitalinfo->cutoffsvl,t_orb->cutoff); |
| 1968 |
// |
| 1969 |
TClonesArray &tt3 = *torbExtTrk; |
| 1970 |
new(tt3[ttentry]) OrbitalInfoTrkVar(*t_orb); |
| 1971 |
ttentry++; |
| 1972 |
// |
| 1973 |
t_orb->Clear(); |
| 1974 |
// |
| 1975 |
} |
| 1976 |
// |
| 1977 |
} |
| 1978 |
} // end standard tracking algorithm: extended |
| 1979 |
|
| 1980 |
} else { |
| 1981 |
if ( debug ) printf(" mmm... mode %u standalone \n",orbitalinfo->mode); |
| 1982 |
} |
| 1983 |
// |
| 1984 |
} else { // HERE IT MISS ALL CODE FOR EXTENDED TRACKING! |
| 1985 |
if ( !standalone ){ |
| 1986 |
// |
| 1987 |
if ( verbose ) printf(" no orb info for tracks \n"); |
| 1988 |
Int_t nn = 0; |
| 1989 |
for(Int_t nt=0; nt < tof->ntrk(); nt++){ |
| 1990 |
// |
| 1991 |
ToFTrkVar *ptt = tof->GetToFTrkVar(nt); |
| 1992 |
if ( ptt->trkseqno != -1 ){ |
| 1993 |
// |
| 1994 |
t_orb->trkseqno = ptt->trkseqno; |
| 1995 |
// |
| 1996 |
t_orb->Eij = 0; |
| 1997 |
// |
| 1998 |
t_orb->Sij = 0; |
| 1999 |
// |
| 2000 |
t_orb->pitch = -1000.; |
| 2001 |
// |
| 2002 |
t_orb->sunangle = -1000.; |
| 2003 |
// |
| 2004 |
t_orb->sunmagangle = -1000; |
| 2005 |
// |
| 2006 |
t_orb->cutoff = -1000.; |
| 2007 |
// |
| 2008 |
new(tor[nn]) OrbitalInfoTrkVar(*t_orb); |
| 2009 |
nn++; |
| 2010 |
// |
| 2011 |
t_orb->Clear(); |
| 2012 |
// |
| 2013 |
} |
| 2014 |
// |
| 2015 |
} |
| 2016 |
// |
| 2017 |
// Code for extended tracking algorithm: |
| 2018 |
// |
| 2019 |
if ( hasNucleiTrk ){ |
| 2020 |
Int_t ttentry = 0; |
| 2021 |
if ( verbose ) printf(" hasNucleiTrk \n"); |
| 2022 |
for(Int_t nt=0; nt < tcNucleiTof->GetEntries() ; nt++){ |
| 2023 |
// |
| 2024 |
ToFTrkVar *ptt = (ToFTrkVar*)(tcNucleiTof->At(nt)); |
| 2025 |
if ( ptt->trkseqno != -1 ){ |
| 2026 |
// |
| 2027 |
t_orb->trkseqno = ptt->trkseqno; |
| 2028 |
// |
| 2029 |
t_orb->Eij = 0; |
| 2030 |
// |
| 2031 |
t_orb->Sij = 0; |
| 2032 |
// |
| 2033 |
t_orb->pitch = -1000.; |
| 2034 |
// |
| 2035 |
t_orb->sunangle = -1000.; |
| 2036 |
// |
| 2037 |
t_orb->sunmagangle = -1000; |
| 2038 |
// |
| 2039 |
t_orb->cutoff = -1000.; |
| 2040 |
// |
| 2041 |
TClonesArray &tz1 = *torbNucleiTrk; |
| 2042 |
new(tz1[ttentry]) OrbitalInfoTrkVar(*t_orb); |
| 2043 |
ttentry++; |
| 2044 |
// |
| 2045 |
t_orb->Clear(); |
| 2046 |
// |
| 2047 |
} |
| 2048 |
// |
| 2049 |
} |
| 2050 |
} |
| 2051 |
if ( hasExtNucleiTrk ){ |
| 2052 |
Int_t ttentry = 0; |
| 2053 |
if ( verbose ) printf(" hasExtNucleiTrk \n"); |
| 2054 |
for(Int_t nt=0; nt < tcExtNucleiTof->GetEntries() ; nt++){ |
| 2055 |
// |
| 2056 |
if ( verbose ) printf(" got2\n"); |
| 2057 |
ToFTrkVar *ptt = (ToFTrkVar*)(tcExtNucleiTof->At(nt)); |
| 2058 |
if ( ptt->trkseqno != -1 ){ |
| 2059 |
// |
| 2060 |
t_orb->trkseqno = ptt->trkseqno; |
| 2061 |
// |
| 2062 |
t_orb->Eij = 0; |
| 2063 |
// |
| 2064 |
t_orb->Sij = 0; |
| 2065 |
// |
| 2066 |
t_orb->pitch = -1000.; |
| 2067 |
// |
| 2068 |
t_orb->sunangle = -1000.; |
| 2069 |
// |
| 2070 |
t_orb->sunmagangle = -1000; |
| 2071 |
// |
| 2072 |
t_orb->cutoff = -1000.; |
| 2073 |
// |
| 2074 |
TClonesArray &tz2 = *torbExtNucleiTrk; |
| 2075 |
new(tz2[ttentry]) OrbitalInfoTrkVar(*t_orb); |
| 2076 |
ttentry++; |
| 2077 |
// |
| 2078 |
t_orb->Clear(); |
| 2079 |
// |
| 2080 |
} |
| 2081 |
// |
| 2082 |
} |
| 2083 |
} |
| 2084 |
if ( hasExtTrk ){ |
| 2085 |
Int_t ttentry = 0; |
| 2086 |
if ( verbose ) printf(" hasExtTrk \n"); |
| 2087 |
for(Int_t nt=0; nt < tcExtTof->GetEntries() ; nt++){ |
| 2088 |
// |
| 2089 |
if ( verbose ) printf(" got3\n"); |
| 2090 |
ToFTrkVar *ptt = (ToFTrkVar*)(tcExtTof->At(nt)); |
| 2091 |
if ( ptt->trkseqno != -1 ){ |
| 2092 |
// |
| 2093 |
t_orb->trkseqno = ptt->trkseqno; |
| 2094 |
// |
| 2095 |
t_orb->Eij = 0; |
| 2096 |
// |
| 2097 |
t_orb->Sij = 0; |
| 2098 |
// |
| 2099 |
t_orb->pitch = -1000.; |
| 2100 |
// |
| 2101 |
t_orb->sunangle = -1000.; |
| 2102 |
// |
| 2103 |
t_orb->sunmagangle = -1000; |
| 2104 |
// |
| 2105 |
t_orb->cutoff = -1000.; |
| 2106 |
// |
| 2107 |
TClonesArray &tz3 = *torbExtNucleiTrk; |
| 2108 |
new(tz3[ttentry]) OrbitalInfoTrkVar(*t_orb); |
| 2109 |
ttentry++; |
| 2110 |
// |
| 2111 |
t_orb->Clear(); |
| 2112 |
// |
| 2113 |
} |
| 2114 |
// |
| 2115 |
} |
| 2116 |
} |
| 2117 |
} |
| 2118 |
} // if( orbitalinfo->TimeGap>0){ |
| 2119 |
// |
| 2120 |
// Fill the class |
| 2121 |
// |
| 2122 |
OrbitalInfotr->Fill(); |
| 2123 |
// |
| 2124 |
delete t_orb; |
| 2125 |
// |
| 2126 |
}; // loop over the events in the run |
| 2127 |
// |
| 2128 |
// Here you may want to clear some variables before processing another run |
| 2129 |
// |
| 2130 |
|
| 2131 |
if ( verbose ) printf(" Clear before new run \n"); |
| 2132 |
delete dbtime; |
| 2133 |
|
| 2134 |
if ( mcmdrc ) mcmdrc->Clear(); |
| 2135 |
mcmdrc = 0; |
| 2136 |
|
| 2137 |
if ( verbose ) printf(" Clear before new run1 \n"); |
| 2138 |
if ( L_QQ_Q_l_lower ) delete L_QQ_Q_l_lower; |
| 2139 |
if ( verbose ) printf(" Clear before new run2 \n"); |
| 2140 |
if ( L_QQ_Q_l_upper ) delete L_QQ_Q_l_upper; |
| 2141 |
if ( verbose ) printf(" Clear before new run3 \n"); |
| 2142 |
if ( RYPang_upper ) delete RYPang_upper; |
| 2143 |
if ( verbose ) printf(" Clear before new run4 \n"); |
| 2144 |
if ( RYPang_lower ) delete RYPang_lower; |
| 2145 |
|
| 2146 |
if ( l0tr ) l0tr->Delete(); |
| 2147 |
|
| 2148 |
if ( verbose ) printf(" End run \n"); |
| 2149 |
|
| 2150 |
}; // process all the runs |
| 2151 |
|
| 2152 |
if (verbose) printf("\n Finished processing data \n"); |
| 2153 |
// |
| 2154 |
closeandexit: |
| 2155 |
// |
| 2156 |
// 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. |
| 2157 |
// |
| 2158 |
if ( !reprocall && reproc && code >= 0 ){ |
| 2159 |
if ( totfileentries > noaftrun ){ |
| 2160 |
if (verbose){ |
| 2161 |
printf("\n Post-processing: copying events from the old tree after the processed run\n"); |
| 2162 |
printf(" Copying %i events in the file which are after the end of the run %i \n",(int)(totfileentries-noaftrun),(int)run); |
| 2163 |
printf(" Start copying at event number %i end copying at event number %i \n",(int)noaftrun,(int)totfileentries); |
| 2164 |
} |
| 2165 |
for (UInt_t j = noaftrun; j < totfileentries; j++ ){ |
| 2166 |
// |
| 2167 |
// Get entry from old tree |
| 2168 |
// |
| 2169 |
if ( OrbitalInfotrclone->GetEntry(j) <= 0 ) throw -36; |
| 2170 |
// |
| 2171 |
// copy orbitalinfoclone to OrbitalInfo |
| 2172 |
// |
| 2173 |
// orbitalinfo->Clear(); |
| 2174 |
// |
| 2175 |
memcpy(&orbitalinfo,&orbitalinfoclone,sizeof(orbitalinfoclone)); |
| 2176 |
// |
| 2177 |
// Fill entry in the new tree |
| 2178 |
// |
| 2179 |
OrbitalInfotr->Fill(); |
| 2180 |
}; |
| 2181 |
if (verbose) printf(" Finished successful copying!\n"); |
| 2182 |
}; |
| 2183 |
//if ( OrbitalInfotrclone ) OrbitalInfotrclone->Clear(); |
| 2184 |
//if ( OrbitalInfotrclone ) OrbitalInfotrclone->Delete(); |
| 2185 |
}; |
| 2186 |
// |
| 2187 |
// Close files, delete old tree(s), write and close level2 file |
| 2188 |
// |
| 2189 |
|
| 2190 |
if ( l0File ) l0File->Close(); |
| 2191 |
if ( myfold ) gSystem->Unlink(tempname.str().c_str()); |
| 2192 |
// |
| 2193 |
if ( OrbitalInfotr ) OrbitalInfotr->SetName("OrbitalInfo"); |
| 2194 |
// |
| 2195 |
if ( file ){ |
| 2196 |
file->cd(); |
| 2197 |
if ( OrbitalInfotr ) OrbitalInfotr->Write("OrbitalInfo", TObject::kOverwrite); // 10 RED bug fixed |
| 2198 |
}; |
| 2199 |
// |
| 2200 |
if (verbose) printf("\n Exiting...\n"); |
| 2201 |
|
| 2202 |
if ( myfold ) gSystem->Unlink(OrbitalInfofolder.str().c_str()); |
| 2203 |
// |
| 2204 |
// the end |
| 2205 |
// |
| 2206 |
if ( dbc ){ |
| 2207 |
dbc->Close(); |
| 2208 |
delete dbc; |
| 2209 |
}; |
| 2210 |
// |
| 2211 |
if (verbose) printf("\n Exiting...\n"); |
| 2212 |
if ( tempfile ) tempfile->Close(); |
| 2213 |
|
| 2214 |
if ( PO ) delete PO; |
| 2215 |
if ( gltle ) delete gltle; |
| 2216 |
if ( glparam ) delete glparam; |
| 2217 |
if ( glparam2 ) delete glparam2; |
| 2218 |
if ( glparam3 ) delete glparam3; |
| 2219 |
if (verbose) printf("\n Exiting3...\n"); |
| 2220 |
if ( glroot ) delete glroot; |
| 2221 |
if (verbose) printf("\n Exiting4...\n"); |
| 2222 |
if ( runinfo ) runinfo->Close(); |
| 2223 |
if ( runinfo ) delete runinfo; |
| 2224 |
|
| 2225 |
if ( tcNucleiTrk ){ |
| 2226 |
tcNucleiTrk->Delete(); |
| 2227 |
delete tcNucleiTrk; |
| 2228 |
tcNucleiTrk = NULL; |
| 2229 |
} |
| 2230 |
if ( tcExtNucleiTrk ){ |
| 2231 |
tcExtNucleiTrk->Delete(); |
| 2232 |
delete tcExtNucleiTrk; |
| 2233 |
tcExtNucleiTrk = NULL; |
| 2234 |
} |
| 2235 |
if ( tcExtTrk ){ |
| 2236 |
tcExtTrk->Delete(); |
| 2237 |
delete tcExtTrk; |
| 2238 |
tcExtTrk = NULL; |
| 2239 |
} |
| 2240 |
|
| 2241 |
if ( tcNucleiTof ){ |
| 2242 |
tcNucleiTof->Delete(); |
| 2243 |
delete tcNucleiTof; |
| 2244 |
tcNucleiTof = NULL; |
| 2245 |
} |
| 2246 |
if ( tcExtNucleiTof ){ |
| 2247 |
tcExtNucleiTof->Delete(); |
| 2248 |
delete tcExtNucleiTof; |
| 2249 |
tcExtNucleiTof = NULL; |
| 2250 |
} |
| 2251 |
if ( tcExtTof ){ |
| 2252 |
tcExtTof->Delete(); |
| 2253 |
delete tcExtTof; |
| 2254 |
tcExtTrk = NULL; |
| 2255 |
} |
| 2256 |
|
| 2257 |
|
| 2258 |
if ( tof ) delete tof; |
| 2259 |
if ( trke ) delete trke; |
| 2260 |
|
| 2261 |
if ( debug ){ |
| 2262 |
cout << "1 0x" << OrbitalInfotr << endl; |
| 2263 |
cout << "2 0x" << OrbitalInfotrclone << endl; |
| 2264 |
cout << "3 0x" << l0tr << endl; |
| 2265 |
cout << "4 0x" << tempOrbitalInfo << endl; |
| 2266 |
cout << "5 0x" << ttof << endl; |
| 2267 |
} |
| 2268 |
// |
| 2269 |
if ( debug ) file->ls(); |
| 2270 |
// |
| 2271 |
if(code < 0) throw code; |
| 2272 |
return(code); |
| 2273 |
} |
| 2274 |
|
| 2275 |
|
| 2276 |
// |
| 2277 |
// Returns the cCoordGeo structure holding the geographical |
| 2278 |
// coordinates for the event (see sgp4.h). |
| 2279 |
// |
| 2280 |
// atime is the abstime of the event in UTC unix time. |
| 2281 |
// tletime is the time of the tle in UTC unix time. |
| 2282 |
// tle is the previous and nearest tle (compared to atime). |
| 2283 |
cCoordGeo getCoo(UInt_t atime, UInt_t tletime, cTle *tle) |
| 2284 |
{ |
| 2285 |
cEci eci; |
| 2286 |
cOrbit orbit(*tle); |
| 2287 |
orbit.getPosition((double) (atime - tletime)/60., &eci); |
| 2288 |
|
| 2289 |
return eci.toGeo(); |
| 2290 |
} |
| 2291 |
|
| 2292 |
// function of copyng of quatrnions classes |
| 2293 |
|
| 2294 |
void CopyQ(Quaternions *Q1, Quaternions *Q2){ |
| 2295 |
for(UInt_t i = 0; i < 6; i++){ |
| 2296 |
Q1->time[i]=Q2->time[i]; |
| 2297 |
for (UInt_t j = 0; j < 4; j++)Q1->quat[i][j]=Q2->quat[i][j]; |
| 2298 |
} |
| 2299 |
return; |
| 2300 |
} |
| 2301 |
|
| 2302 |
// functions of copyng InclinationInfo classes |
| 2303 |
|
| 2304 |
void CopyAng(InclinationInfo *A1, InclinationInfo *A2){ |
| 2305 |
A1->Tangazh = A2->Tangazh; |
| 2306 |
A1->Ryskanie = A2->Ryskanie; |
| 2307 |
A1->Kren = A2->Kren; |
| 2308 |
return; |
| 2309 |
} |
| 2310 |
|
| 2311 |
UInt_t holeq(Double_t lower,Double_t upper,Quaternions *Qlower, Quaternions *Qupper, UInt_t f){ |
| 2312 |
|
| 2313 |
UInt_t hole = 10; |
| 2314 |
Bool_t R10l = false; // Sign of R10 mode in lower quaternions array |
| 2315 |
Bool_t R10u = false; // Sign of R10 mode in upper quaternions array |
| 2316 |
Bool_t insm = false; // Sign that we inside quaternions array |
| 2317 |
// Bool_t mxtml = false; // Sign of mixt mode in lower quaternions array |
| 2318 |
// Bool_t mxtmu = false; // Sign of mixt mode in upper quaternions array |
| 2319 |
Bool_t npasm = false; // Sign of normall pass between R10 and non R10 or between non R10 and R10 |
| 2320 |
UInt_t NCQl = 6; // Number of correct quaternions in lower array |
| 2321 |
// UInt_t NCQu = 6; // Number of correct quaternions in upper array |
| 2322 |
if (f>0){ |
| 2323 |
insm = true; |
| 2324 |
if(Qupper->time[f]-Qupper->time[f-1]==30) R10u = false; |
| 2325 |
if(Qupper->time[f]-Qupper->time[f-1]<1) R10u = true; |
| 2326 |
}else{ |
| 2327 |
insm = false; |
| 2328 |
if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]<2)) R10l = true; |
| 2329 |
if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]<2)) R10u = true; |
| 2330 |
if((Qlower->time[5]-Qlower->time[0]==150)&&(Qlower->time[1]-Qlower->time[0]==30)) R10l = false; |
| 2331 |
if((Qupper->time[5]-Qupper->time[0]==150)&&(Qupper->time[1]-Qupper->time[0]==30)) R10u = false; |
| 2332 |
if((Qlower->time[5]-Qlower->time[0]<2)&&(Qlower->time[1]-Qlower->time[0]==30)){ |
| 2333 |
// mxtml = true; |
| 2334 |
for(UInt_t i = 1; i < 6; i++){ |
| 2335 |
if(Qlower->time[i]-Qlower->time[0]==30*i) NCQl=i; |
| 2336 |
} |
| 2337 |
} |
| 2338 |
// if((Qupper->time[5]-Qupper->time[0]<2)&&(Qupper->time[1]-Qupper->time[0]==30)){ |
| 2339 |
// mxtmu = true; |
| 2340 |
// for(UInt_t i = 1; i < 6; i++){ |
| 2341 |
// if(Qupper->time[i]-Qupper->time[0]==30*i) NCQu=i; |
| 2342 |
// } |
| 2343 |
// } |
| 2344 |
} |
| 2345 |
|
| 2346 |
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; |
| 2347 |
|
| 2348 |
|
| 2349 |
if (R10u&&insm) hole=0; // best event R10 |
| 2350 |
if ((upper-lower<=5)&&(!insm)&&R10l&&R10u) hole = 1; // when first of 6 quaternions in array is correct |
| 2351 |
if (((!R10u)&&insm)||((!insm)&&(!R10u)&&(!R10l)&&((upper-lower==210+(6-NCQl)*30)||(upper-lower==30)))) hole = 2; //non R10 |
| 2352 |
if (npasm&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 3; //normall pass from R10 to non R10 or from non R10 to R10 |
| 2353 |
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 |
| 2354 |
if ((upper-lower>=300)&&(!insm)&&((R10l&&!R10u)||(R10u&&!R10l))) hole = 5; //uneliminable hole between R10 and non R10 or between non R10 and R10 |
| 2355 |
if ((upper-lower>5)&&(upper-lower<=300)&&R10u&&R10l) hole = 6; // eliminable hole inside R10 |
| 2356 |
if ((upper-lower>300)&&R10u&&R10l) hole = 7; //uneliminable hole inside R10 |
| 2357 |
if ((upper-lower>210)&&(upper-lower<=1200)&&(!R10u)&&(!R10l)) hole = 8; //eliminable hole inside non R10 |
| 2358 |
if ((upper-lower>1200)&&!R10u&&!R10l) hole = 9; // uneliminable hole inside non R10 |
| 2359 |
return hole; |
| 2360 |
} |
| 2361 |
|
| 2362 |
void inclresize(vector<Double_t>& t,vector<Float_t>& q0,vector<Float_t>& q1,vector<Float_t>& q2,vector<Float_t>& q3,vector<Int_t>& mode,vector<Float_t>& Roll,vector<Float_t>& Pitch,vector<Float_t>& Yaw){ |
| 2363 |
Int_t sizee = t.size()+1; |
| 2364 |
t.resize(sizee); |
| 2365 |
q0.resize(sizee); |
| 2366 |
q1.resize(sizee); |
| 2367 |
q2.resize(sizee); |
| 2368 |
q3.resize(sizee); |
| 2369 |
mode.resize(sizee); |
| 2370 |
Roll.resize(sizee); |
| 2371 |
Pitch.resize(sizee); |
| 2372 |
Yaw.resize(sizee); |
| 2373 |
} |
| 2374 |
|
| 2375 |
// geomagnetic calculation staff |
| 2376 |
|
| 2377 |
//void GM_ScanIGRF(TString PATH, GMtype_Data *G0, GMtype_Data *G1, GMtype_Data *H1) |
| 2378 |
void GM_ScanIGRF(TSQLServer *dbc, GMtype_Data *G0, GMtype_Data *G1, GMtype_Data *H1) |
| 2379 |
{ |
| 2380 |
GL_PARAM *glp = new GL_PARAM(); |
| 2381 |
Int_t parerror=glp->Query_GL_PARAM(1,304,dbc); // parameters stored in DB in GL_PRAM table |
| 2382 |
if ( parerror<0 ) { |
| 2383 |
throw -902; |
| 2384 |
} |
| 2385 |
/*This function scans inputs G0, G1, and H1 of the IGRF table into 3 data arrays*/ |
| 2386 |
// TString SATH="/data03/Malakhov/pam9Malakhov/installed10/calib/orb-param/"; |
| 2387 |
int i; |
| 2388 |
double temp; |
| 2389 |
char buffer[200]; |
| 2390 |
FILE *IGRF; |
| 2391 |
IGRF = fopen((glp->PATH+glp->NAME).Data(), "r"); |
| 2392 |
// IGRF = fopen(PATH+"IGRF.tab", "r"); |
| 2393 |
G0->size = 25; |
| 2394 |
G1->size = 25; |
| 2395 |
H1->size = 25; |
| 2396 |
for( i = 0; i < 4; i++) |
| 2397 |
{ |
| 2398 |
fgets(buffer, 200, IGRF); |
| 2399 |
} |
| 2400 |
fscanf(IGRF, "g 1 0 %lf ", &G0->element[0]); |
| 2401 |
for(i = 1; i <= 22; i++) |
| 2402 |
{ |
| 2403 |
fscanf(IGRF ,"%lf ", &G0->element[i]); |
| 2404 |
} |
| 2405 |
fscanf(IGRF ,"%lf\n", &temp); |
| 2406 |
G0->element[23] = temp * 5 + G0->element[22]; |
| 2407 |
G0->element[24] = G0->element[23] + 5 * temp; |
| 2408 |
fscanf(IGRF, "g 1 1 %lf ", &G1->element[0]); |
| 2409 |
for(i = 1; i <= 22; i++) |
| 2410 |
{ |
| 2411 |
fscanf( IGRF, "%lf ", &G1->element[i]); |
| 2412 |
} |
| 2413 |
fscanf(IGRF, "%lf\n", &temp); |
| 2414 |
G1->element[23] = temp * 5 + G1->element[22]; |
| 2415 |
G1->element[24] = temp * 5 + G1->element[23]; |
| 2416 |
fscanf(IGRF, "h 1 1 %lf ", &H1->element[0]); |
| 2417 |
for(i = 1; i <= 22; i++) |
| 2418 |
{ |
| 2419 |
fscanf( IGRF, "%lf ", &H1->element[i]); |
| 2420 |
} |
| 2421 |
fscanf(IGRF, "%lf\n", &temp); |
| 2422 |
H1->element[23] = temp * 5 + H1->element[22]; |
| 2423 |
H1->element[24] = temp * 5 + H1->element[23]; |
| 2424 |
if ( glp ) delete glp; |
| 2425 |
} /*GM_ScanIGRF*/ |
| 2426 |
|
| 2427 |
void GM_SetEllipsoid(GMtype_Ellipsoid *Ellip) |
| 2428 |
{ |
| 2429 |
/*This function sets the WGS84 reference ellipsoid to its default values*/ |
| 2430 |
Ellip->a = 6378.137; /*semi-major axis of the ellipsoid in */ |
| 2431 |
Ellip->b = 6356.7523142;/*semi-minor axis of the ellipsoid in */ |
| 2432 |
Ellip->fla = 1/298.257223563;/* flattening */ |
| 2433 |
Ellip->eps = sqrt(1- ( Ellip->b * Ellip->b) / (Ellip->a * Ellip->a )); /*first eccentricity */ |
| 2434 |
Ellip->epssq = (Ellip->eps * Ellip->eps); /*first eccentricity squared */ |
| 2435 |
Ellip->re = 6371.2;/* Earth's radius */ |
| 2436 |
} /*GM_SetEllipsoid*/ |
| 2437 |
|
| 2438 |
|
| 2439 |
void GM_EarthCartToDipoleCartCD(GMtype_Pole Pole, GMtype_CoordCartesian EarthCoord, GMtype_CoordCartesian *DipoleCoords) |
| 2440 |
{ |
| 2441 |
/*This function converts from Earth centered cartesian coordinates to dipole centered cartesian coordinates*/ |
| 2442 |
double X, Y, Z, CosPhi, SinPhi, CosLambda, SinLambda; |
| 2443 |
CosPhi = cos(TMath::DegToRad()*Pole.phi); |
| 2444 |
SinPhi = sin(TMath::DegToRad()*Pole.phi); |
| 2445 |
CosLambda = cos(TMath::DegToRad()*Pole.lambda); |
| 2446 |
SinLambda = sin(TMath::DegToRad()*Pole.lambda); |
| 2447 |
X = EarthCoord.x; |
| 2448 |
Y = EarthCoord.y; |
| 2449 |
Z = EarthCoord.z; |
| 2450 |
|
| 2451 |
/*These equations are taken from a document by Wallace H. Campbell*/ |
| 2452 |
DipoleCoords->x = X * CosPhi * CosLambda + Y * CosPhi * SinLambda - Z * SinPhi; |
| 2453 |
DipoleCoords->y = -X * SinLambda + Y * CosLambda; |
| 2454 |
DipoleCoords->z = X * SinPhi * CosLambda + Y * SinPhi * SinLambda + Z * CosPhi; |
| 2455 |
} /*GM_EarthCartToDipoleCartCD*/ |
| 2456 |
|
| 2457 |
void GM_GeodeticToSpherical(GMtype_Ellipsoid Ellip, GMtype_CoordGeodetic CoordGeodetic, GMtype_CoordSpherical *CoordSpherical) |
| 2458 |
{ |
| 2459 |
double CosLat, SinLat, rc, xp, zp; /*all local variables */ |
| 2460 |
/* |
| 2461 |
** Convert geodetic coordinates, (defined by the WGS-84 |
| 2462 |
** reference ellipsoid), to Earth Centered Earth Fixed Cartesian |
| 2463 |
** coordinates, and then to spherical coordinates. |
| 2464 |
*/ |
| 2465 |
|
| 2466 |
CosLat = cos(TMath::DegToRad()*CoordGeodetic.phi); |
| 2467 |
SinLat = sin(TMath::DegToRad()*CoordGeodetic.phi); |
| 2468 |
|
| 2469 |
/* compute the local radius of curvature on the WGS-84 reference ellipsoid */ |
| 2470 |
|
| 2471 |
rc = Ellip.a / sqrt(1.0 - Ellip.epssq * SinLat * SinLat); |
| 2472 |
|
| 2473 |
/* compute ECEF Cartesian coordinates of specified point (for longitude=0) */ |
| 2474 |
|
| 2475 |
xp = (rc + CoordGeodetic.HeightAboveEllipsoid) * CosLat; |
| 2476 |
zp = (rc*(1.0 - Ellip.epssq) + CoordGeodetic.HeightAboveEllipsoid) * SinLat; |
| 2477 |
|
| 2478 |
/* compute spherical radius and angle lambda and phi of specified point */ |
| 2479 |
|
| 2480 |
CoordSpherical->r = sqrt(xp * xp + zp * zp); |
| 2481 |
CoordSpherical->phig = TMath::RadToDeg()*asin(zp / CoordSpherical->r); /* geocentric latitude */ |
| 2482 |
CoordSpherical->lambda = CoordGeodetic.lambda; /* longitude */ |
| 2483 |
} /*GM_GeodeticToSpherical*/ |
| 2484 |
|
| 2485 |
void GM_PoleLocation(GMtype_Model Model, GMtype_Pole *Pole) |
| 2486 |
{ |
| 2487 |
/*This function finds the location of the north magnetic pole in spherical coordinates. The equations are |
| 2488 |
**from Wallace H. Campbell's Introduction to Geomagnetic Fields*/ |
| 2489 |
|
| 2490 |
Pole->phi = TMath::RadToDeg()*-atan(sqrt(Model.h1 * Model.h1 + Model.g1 * Model.g1)/Model.g0); |
| 2491 |
Pole->lambda = TMath::RadToDeg()*atan(Model.h1/Model.g1); |
| 2492 |
} /*GM_PoleLocation*/ |
| 2493 |
|
| 2494 |
void GM_SphericalToCartesian(GMtype_CoordSpherical CoordSpherical, GMtype_CoordCartesian *CoordCartesian) |
| 2495 |
{ |
| 2496 |
/*This function converts spherical coordinates into Cartesian coordinates*/ |
| 2497 |
double CosPhi = cos(TMath::DegToRad()*CoordSpherical.phig); |
| 2498 |
double SinPhi = sin(TMath::DegToRad()*CoordSpherical.phig); |
| 2499 |
double CosLambda = cos(TMath::DegToRad()*CoordSpherical.lambda); |
| 2500 |
double SinLambda = sin(TMath::DegToRad()*CoordSpherical.lambda); |
| 2501 |
|
| 2502 |
CoordCartesian->x = CoordSpherical.r * CosPhi * CosLambda; |
| 2503 |
CoordCartesian->y = CoordSpherical.r * CosPhi * SinLambda; |
| 2504 |
CoordCartesian->z = CoordSpherical.r * SinPhi; |
| 2505 |
} /*GM_SphericalToCartesian*/ |
| 2506 |
|
| 2507 |
void GM_TimeAdjustCoefs(Float_t year, Float_t jyear, GMtype_Data g0d, GMtype_Data g1d, GMtype_Data h1d, GMtype_Model *Model) |
| 2508 |
{ |
| 2509 |
/*This function calls GM_LinearInterpolation for the coefficients to estimate the value of the |
| 2510 |
**coefficient for the given date*/ |
| 2511 |
int index; |
| 2512 |
double x; |
| 2513 |
index = (year - GM_STARTYEAR) / 5; |
| 2514 |
x = (jyear - GM_STARTYEAR) / 5; |
| 2515 |
Model->g0 = GM_LinearInterpolation(index, index+1, g0d.element[index], g0d.element[index+1], x); |
| 2516 |
Model->g1 = GM_LinearInterpolation(index, index+1, g1d.element[index], g1d.element[index+1], x); |
| 2517 |
Model->h1 = GM_LinearInterpolation(index, index+1, h1d.element[index], h1d.element[index+1], x); |
| 2518 |
} /*GM_TimeAdjustCoefs*/ |
| 2519 |
|
| 2520 |
double GM_LinearInterpolation(double x1, double x2, double y1, double y2, double x) |
| 2521 |
{ |
| 2522 |
/*This function takes a linear interpolation between two given points for x*/ |
| 2523 |
double weight, y; |
| 2524 |
weight = (x - x1) / (x2 - x1); |
| 2525 |
y = y1 * (1 - weight) + y2 * weight; |
| 2526 |
return y; |
| 2527 |
}/*GM_LinearInterpolation*/ |
| 2528 |
|
| 2529 |
void GM_CartesianToSpherical(GMtype_CoordCartesian CoordCartesian, GMtype_CoordSpherical *CoordSpherical) |
| 2530 |
{ |
| 2531 |
/*This function converts a point from Cartesian coordinates into spherical coordinates*/ |
| 2532 |
double X, Y, Z; |
| 2533 |
|
| 2534 |
X = CoordCartesian.x; |
| 2535 |
Y = CoordCartesian.y; |
| 2536 |
Z = CoordCartesian.z; |
| 2537 |
|
| 2538 |
CoordSpherical->r = sqrt(X * X + Y * Y + Z * Z); |
| 2539 |
CoordSpherical->phig = TMath::RadToDeg()*asin(Z / (CoordSpherical->r)); |
| 2540 |
CoordSpherical->lambda = TMath::RadToDeg()*atan2(Y, X); |
| 2541 |
} /*GM_CartesianToSpherical*/ |
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