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

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revision 1.5 by mocchiut, Tue Sep 5 14:49:45 2006 UTC revision 1.13 by mocchiut, Tue Nov 11 10:46:44 2008 UTC
# Line 1  Line 1 
1  #include <OrbitalInfo.h>  #include <OrbitalInfo.h>
2    
3    using namespace std;
4    
5    ClassImp(OrbitalInfoTrkVar);
6    ClassImp(OrbitalInfo);
7    
8    OrbitalInfoTrkVar::OrbitalInfoTrkVar(){
9      this->Clear();
10      //  Eij = new TMatrixD(3,3);
11      //  Sij = new TMatrixD(3,3);
12    }
13    
14    void OrbitalInfoTrkVar::Clear(Option_t *t){
15      trkseqno = 0;
16      pitch = -1000.;
17      Eij.Zero();
18      Sij.Zero();
19    }
20    
21    void OrbitalInfoTrkVar::Delete(Option_t *t){
22      //  if ( Eij ) Eij->Delete();
23      //  if ( Sij ) Sij->Delete();
24    }
25    
26  OrbitalInfo::OrbitalInfo(){  OrbitalInfo::OrbitalInfo(){
27    absTime = 0;    OrbitalInfoTrk = 0; //ELENA
28    OBT = 0;    this->Clear();
   pkt_num = 0;  
29  }  }
30    
31    void OrbitalInfo::Delete(Option_t *t){ //ELENA
32      //
33      //  if ( Iij ) Iij->Delete();
34      if(OrbitalInfoTrk){
35        OrbitalInfoTrk->Delete(); //ELENA
36        delete OrbitalInfoTrk;  //ELENA
37      }
38      //
39    }; //ELENA
40    
41    void OrbitalInfo::Set(){//ELENA
42      if ( !OrbitalInfoTrk ) OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); //ELENA}  
43      //  if ( !Iij ) Iij = new TMatrixD(3,3);
44    }//ELENA
45    
46    OrbitalInfoTrkVar *OrbitalInfo::GetOrbitalInfoTrkVar(Int_t itrk){
47      //    
48      if(itrk >= ntrk()){
49        printf(" OrbitalInfo ERROR: track related variables set %i does not exists! \n",itrk);
50        printf("                    stored track related variables = %i \n",ntrk());
51        return(NULL);
52      }  
53      //
54      if(!OrbitalInfoTrk)return 0; //ELENA
55      TClonesArray &t = *(OrbitalInfoTrk);
56      OrbitalInfoTrkVar *orbtrack = (OrbitalInfoTrkVar*)t[itrk];
57      return orbtrack;
58    }
59    
60  void OrbitalInfo::Clear(){  void OrbitalInfo::Clear(Option_t *t){
61      //
62      if ( OrbitalInfoTrk ) OrbitalInfoTrk->Delete();
63      //
64    absTime = 0;    absTime = 0;
65    OBT = 0;    OBT = 0;
66    pkt_num = 0;    pkt_num = 0;
67    
68      lon = -1000.;
69      lat = -1000.;
70      alt = -1000.;
71    
72      Bnorth = -1000.;
73      Beast = -1000.;
74      Bdown = -1000.;
75      Babs = -1000.;
76      BB0 = -1000.;
77      L = -1000.;
78    
79    //   londip = -1000.;
80    //   latdip = -1000.;
81    //   altdip = -1000.;
82    
83    //   loncgm = -1000.;
84    //   latcgm = -1000.;
85    //   altcgm = -1000.;
86    
87    //   loncbm = -1000.;
88    //   latcbm = -1000.;
89    //   altcbm = -1000.;
90    
91      //  std::fill_n(cutoff, 20, 0.);
92      //  std::fill_n(cutoff, 2, 0.);
93      cutoffsvl = 0.;
94    
95      // Quaternions
96      q0 = -1000.;
97      q1 = -1000.;
98      q2 = -1000.;
99      q3 = -1000.;
100    
101      // Euler angles (nadir reference frame)
102      theta = -1000.;
103      phi = -1000.;
104      etha = -1000.;
105    
106      // Euler angles (local field reference frame)
107      //  thetamag = -1000.;
108      //  phimag = -1000.;
109      //  ethamag = -1000.;
110    
111      //  pamzenitangle = -1000.;
112      //  pamBangle = -1000.;
113      Iij.Zero();
114    
115      mode = 0;
116      //  std::fill_n(goodAttitude, 5, 0);
117  }  }
118    
119  /**  /**
# Line 20  void OrbitalInfo::GetLevel2Struct(cOrbit Line 123  void OrbitalInfo::GetLevel2Struct(cOrbit
123    l2->abstime  = absTime;    l2->abstime  = absTime;
124    l2->obt      = OBT;    l2->obt      = OBT;
125    l2->pkt_num  = pkt_num;    l2->pkt_num  = pkt_num;
126    
127      l2->lon = lon;
128      l2->lat = lat;
129      l2->alt = alt;
130    
131      l2->Bnorth = Bnorth;
132      l2->Beast = Beast;
133      l2->Bdown = Bdown;
134      l2->Babs = Babs;
135      l2->BB0 = BB0;
136      l2->L = L;
137    
138    //   l2->londip = londip;
139    //   l2->latdip = latdip;
140    //   l2->altdip = altdip;
141    
142    //   l2->loncgm = loncgm;
143    //   l2->latcgm = latcgm;
144    //   l2->altcgm = altcgm;
145    
146    //   l2->loncbm = loncbm;
147    //   l2->latcbm = latcbm;
148    //   l2->altcbm = altcbm;
149    
150      l2->cutoffsvl = cutoffsvl;
151    //  memcpy(l2->cutoffsvl, cutoffsvl, sizeof(cutoffsvl));
152    
153      // Quaternions
154      l2->q0 = q0;
155      l2->q1 = q1;
156      l2->q2 = q2;
157      l2->q3 = q3;
158    
159      // Euler angles (nadir reference frame)
160      l2->theta = theta;
161      l2->phi = phi;
162      l2->etha = etha;
163    
164      l2->mode = mode;
165      // Euler angles (local field reference frame)
166    //   l2->thetamag = thetamag;
167    //   l2->phimag = phimag;
168    //   l2->ethamag = ethamag;
169    
170    //   memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));
171  }  }
172    
173  void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){  void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){
174    absTime  = l2->abstime;    absTime  = l2->abstime;
175    OBT      = l2->obt;    OBT      = l2->obt;
176    pkt_num  = l2->pkt_num;    pkt_num  = l2->pkt_num;
177    
178      lon = l2->lon;
179      lat = l2->lat;
180      alt = l2->alt;
181    
182      l2->Bnorth = Bnorth;
183      l2->Beast = Beast;
184      l2->Bdown = Bdown;
185      l2->Babs = Babs;
186      BB0 = l2->BB0;
187      L = l2->L;
188    
189    //   londip = l2->londip;
190    //   latdip = l2->latdip;
191    //   altdip = l2->altdip;
192    
193    //   loncgm = l2->loncgm;
194    //   latcgm = l2->latcgm;
195    //   altcgm = l2->altcgm;
196    
197    //   loncbm = l2->loncbm;
198    //   latcbm = l2->latcbm;
199    //   altcbm = l2->altcbm;
200    
201    //  memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff));
202      l2->cutoffsvl = cutoffsvl;
203    
204      // Quaternions
205      q0 = l2->q0;
206      q1 = l2->q1;
207      q2 = l2->q2;
208      q3 = l2->q3;
209    
210      // Euler angles (nadir reference frame)
211      theta = l2->theta;
212      phi = l2->phi;
213      etha = l2->etha;
214    
215      mode = l2->mode;
216      // Euler angles (local field reference frame)
217    //   thetamag = l2->thetamag;
218    //   phimag = l2->phimag;
219    //   ethamag = l2->ethamag;
220    
221    //   memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
222  }  }
223    
 ClassImp(OrbitalInfo)  
   
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