--- DarthVader/OrbitalInfo/src/OrbitalInfo.cpp	2007/03/15 12:42:47	1.7
+++ DarthVader/OrbitalInfo/src/OrbitalInfo.cpp	2014/03/28 20:47:15	1.16
@@ -1,56 +1,85 @@
 #include <OrbitalInfo.h>
 
-OrbitalInfo::OrbitalInfo(){
-  absTime = 0;
-  OBT = 0;
-  pkt_num = 0;
-
-  lon = 0.;
-  lat = 0.;
-  alt = 0.;
-
-  Bnorth = 0.;
-  Beast = 0.;
-  Bdown = 0.;
-  Babs = 0.;
-  BB0 = 0.;
-  L = 0.;
-
-  londip = -1000.;
-  latdip = -1000.;
-  altdip = -1000.;
-
-  loncgm = -1000.;
-  latcgm = -1000.;
-  altcgm = -1000.;
-
-  loncbm = -1000.;
-  latcbm = -1000.;
-  altcbm = -1000.;
+using namespace std;
 
-  std::fill_n(cutoff, 20, 0.);
+ClassImp(OrbitalInfoTrkVar);
+ClassImp(OrbitalInfo);
 
-  // Quaternions
-  q0 = -1000.;
-  q1 = -1000.;
-  q2 = -1000.;
-  q3 = -1000.;
+OrbitalInfoTrkVar::OrbitalInfoTrkVar(){
+  this->Clear();
+  //  Eij = new TMatrixD(3,3);
+  //  Sij = new TMatrixD(3,3);
+}
 
-  // Euler angles (nadir reference frame)
-//  theta = -1000.;
-//  phi = -1000.;
-//  etha = -1000.;
+void OrbitalInfoTrkVar::Clear(Option_t *t){
+  trkseqno = 0;
+  pitch = -1000.;
+  sunangle = -1000;
+  sunmagangle = -1000;
+  cutoff = -1000.;
+  Eij.Zero();
+  Sij.Zero();
+}
 
-  // Euler angles (local field reference frame)
-//  thetamag = -1000.;
-//  phimag = -1000.;
-//  ethamag = -1000.;
+void OrbitalInfoTrkVar::Delete(Option_t *t){
+  //  if ( Eij ) Eij->Delete();
+  //  if ( Sij ) Sij->Delete();
+}
 
-  std::fill_n(goodAttitude, 5, 0);
+OrbitalInfo::OrbitalInfo(){
+  OrbitalInfoTrk = 0; //ELENA
+  this->Clear();
 }
 
+OrbitalInfoTrkVar::OrbitalInfoTrkVar(const OrbitalInfoTrkVar &t){
+  //
+  trkseqno = t.trkseqno;  
+  //
+  pitch = t.pitch;
+  cutoff = t.cutoff;
+  sunangle=t.sunangle;
+  sunmagangle=t.sunmagangle;
+  //
+  Eij.ResizeTo(t.Eij);	
+  Eij = t.Eij;	
+  Sij.ResizeTo(t.Sij);	
+  Sij = t.Sij;	
+  //
+};
+
+void OrbitalInfo::Delete(Option_t *t){ //ELENA
+  //
+  //  if ( Iij ) Iij->Delete();
+  if(OrbitalInfoTrk){ 
+    OrbitalInfoTrk->Delete(); //ELENA
+    delete OrbitalInfoTrk;  //ELENA
+  }
+  // 
+}; //ELENA
+
+void OrbitalInfo::Set(){//ELENA
+  if ( !OrbitalInfoTrk ) OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); //ELENA}  
+  //  if ( !Iij ) Iij = new TMatrixD(3,3);
+}//ELENA
+
+OrbitalInfoTrkVar *OrbitalInfo::GetOrbitalInfoTrkVar(Int_t itrk){
+  //    
+  if(itrk >= ntrk()){
+    printf(" OrbitalInfo ERROR: track related variables set %i does not exists! \n",itrk);
+    printf("                    stored track related variables = %i \n",ntrk());
+    return(NULL);
+  }  
+  //
+  if(!OrbitalInfoTrk)return 0; //ELENA
+  TClonesArray &t = *(OrbitalInfoTrk);
+  OrbitalInfoTrkVar *orbtrack = (OrbitalInfoTrkVar*)t[itrk];
+  return orbtrack;
+}
 
-void OrbitalInfo::Clear(){
+void OrbitalInfo::Clear(Option_t *t){
+  //
+  if ( OrbitalInfoTrk ) OrbitalInfoTrk->Delete();
+  //
   absTime = 0;
   OBT = 0;
   pkt_num = 0;
@@ -58,27 +87,22 @@
   lon = -1000.;
   lat = -1000.;
   alt = -1000.;
+  V.SetXYZ(-1000.,-1000.,-1000.);
 
   Bnorth = -1000.;
   Beast = -1000.;
   Bdown = -1000.;
   Babs = -1000.;
+  M = -1000;
   BB0 = -1000.;
   L = -1000.;
 
-  londip = -1000.;
-  latdip = -1000.;
-  altdip = -1000.;
-
-  loncgm = -1000.;
-  latcgm = -1000.;
-  altcgm = -1000.;
-
-  loncbm = -1000.;
-  latcbm = -1000.;
-  altcbm = -1000.;
+   londip = -1000.;
+   latdip = -1000.;
 
-  std::fill_n(cutoff, 20, 0.);
+  //  std::fill_n(cutoff, 20, 0.);
+  //  std::fill_n(cutoff, 2, 0.);
+  cutoffsvl = 0.;
 
   // Quaternions
   q0 = -1000.;
@@ -87,16 +111,17 @@
   q3 = -1000.;
 
   // Euler angles (nadir reference frame)
- // theta = -1000.;
- // phi = -1000.;
- // etha = -1000.;
-
-  // Euler angles (local field reference frame)
-  //thetamag = -1000.;
- // phimag = -1000.;
-  //ethamag = -1000.;
-
-  std::fill_n(goodAttitude, 5, 0);
+  theta = -1000.;
+  phi = -1000.;
+  etha = -1000.;
+
+  Iij.Zero();
+
+  mode = 0;
+  qkind = -1000;
+  errq =  -1000;
+  azim =  -1000;
+  //  std::fill_n(goodAttitude, 5, 0);
 }
 
 /**
@@ -110,27 +135,21 @@
   l2->lon = lon;
   l2->lat = lat;
   l2->alt = alt;
+  l2->V = V;
 
   l2->Bnorth = Bnorth;
   l2->Beast = Beast;
   l2->Bdown = Bdown;
   l2->Babs = Babs;
+  l2->M = M;
   l2->BB0 = BB0;
   l2->L = L;
 
-  l2->londip = londip;
-  l2->latdip = latdip;
-  l2->altdip = altdip;
-
-  l2->loncgm = loncgm;
-  l2->latcgm = latcgm;
-  l2->altcgm = altcgm;
-
-  l2->loncbm = loncbm;
-  l2->latcbm = latcbm;
-  l2->altcbm = altcbm;
+   l2->londip = londip;
+   l2->latdip = latdip;
 
-  memcpy(l2->cutoff, cutoff, sizeof(cutoff));
+  l2->cutoffsvl = cutoffsvl;
+//  memcpy(l2->cutoffsvl, cutoffsvl, sizeof(cutoffsvl));
 
   // Quaternions
   l2->q0 = q0;
@@ -139,16 +158,16 @@
   l2->q3 = q3;
 
   // Euler angles (nadir reference frame)
- // l2->theta = theta;
- // l2->phi = phi;
- // l2->etha = etha;
-
-  // Euler angles (local field reference frame)
- // l2->thetamag = thetamag;
- // l2->phimag = phimag;
- // l2->ethamag = ethamag;
+  l2->theta = theta;
+  l2->phi = phi;
+  l2->etha = etha;
+
+  l2->mode = mode;
+  l2->qkind = qkind;
+  l2->errq = errq;
+  l2->azim = azim;
 
-  memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));
+//   memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));
 }
 
 void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){
@@ -159,27 +178,21 @@
   lon = l2->lon;
   lat = l2->lat;
   alt = l2->alt;
+  V = l2->V;
 
   l2->Bnorth = Bnorth;
   l2->Beast = Beast;
   l2->Bdown = Bdown;
   l2->Babs = Babs;
+  M = l2->M;
   BB0 = l2->BB0;
   L = l2->L;
 
-  londip = l2->londip;
-  latdip = l2->latdip;
-  altdip = l2->altdip;
-
-  loncgm = l2->loncgm;
-  latcgm = l2->latcgm;
-  altcgm = l2->altcgm;
-
-  loncbm = l2->loncbm;
-  latcbm = l2->latcbm;
-  altcbm = l2->altcbm;
+   londip = l2->londip;
+   latdip = l2->latdip;
 
-  memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff));
+//  memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff));
+  l2->cutoffsvl = cutoffsvl;
 
   // Quaternions
   q0 = l2->q0;
@@ -188,16 +201,15 @@
   q3 = l2->q3;
 
   // Euler angles (nadir reference frame)
-  //theta = l2->theta;
-  //phi = l2->phi;
-  //etha = l2->etha;
-
-  // Euler angles (local field reference frame)
-  //thetamag = l2->thetamag;
-  //phimag = l2->phimag;
-  //ethamag = l2->ethamag;
+  theta = l2->theta;
+  phi = l2->phi;
+  etha = l2->etha;
+
+  mode = l2->mode;
+  qkind = l2->qkind;
+  errq = l2->errq;
+  azim = l2->azim;
 
-  memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
+//   memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
 }
 
-ClassImp(OrbitalInfo)