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

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revision 1.7 by mocchiut, Thu Mar 15 12:42:47 2007 UTC revision 1.11 by mocchiut, Wed Oct 1 15:25:44 2008 UTC
# Line 1  Line 1 
1  #include <OrbitalInfo.h>  #include <OrbitalInfo.h>
2    
3  OrbitalInfo::OrbitalInfo(){  using namespace std;
   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.;  
4    
5    loncbm = -1000.;  ClassImp(OrbitalInfoTrkVar);
6    latcbm = -1000.;  ClassImp(OrbitalInfo);
   altcbm = -1000.;  
7    
8    std::fill_n(cutoff, 20, 0.);  OrbitalInfoTrkVar::OrbitalInfoTrkVar(){
9      this->Clear();
10    // Quaternions  }
   q0 = -1000.;  
   q1 = -1000.;  
   q2 = -1000.;  
   q3 = -1000.;  
11    
12    // Euler angles (nadir reference frame)  void OrbitalInfoTrkVar::Clear(Option_t *t){
13  //  theta = -1000.;    trkseqno = 0;
14  //  phi = -1000.;    pitch = -1000.;
15  //  etha = -1000.;  }
16    
   // Euler angles (local field reference frame)  
 //  thetamag = -1000.;  
 //  phimag = -1000.;  
 //  ethamag = -1000.;  
17    
18    std::fill_n(goodAttitude, 5, 0);  OrbitalInfo::OrbitalInfo(){
19      OrbitalInfoTrk = 0; //ELENA
20      this->Clear();
21  }  }
22    
23    void OrbitalInfo::Delete(Option_t *t){ //ELENA
24  void OrbitalInfo::Clear(){    //
25      if(OrbitalInfoTrk){
26        OrbitalInfoTrk->Delete(); //ELENA
27        delete OrbitalInfoTrk;  //ELENA
28      }
29      //
30    }; //ELENA
31    
32    void OrbitalInfo::Set(){//ELENA
33      if ( !OrbitalInfoTrk ) OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); //ELENA
34    }//ELENA
35    
36    
37    void OrbitalInfo::Clear(Option_t *t){
38      //
39      if ( OrbitalInfoTrk ) OrbitalInfoTrk->Delete();
40      //
41    absTime = 0;    absTime = 0;
42    OBT = 0;    OBT = 0;
43    pkt_num = 0;    pkt_num = 0;
# Line 87  void OrbitalInfo::Clear(){ Line 74  void OrbitalInfo::Clear(){
74    q3 = -1000.;    q3 = -1000.;
75    
76    // Euler angles (nadir reference frame)    // Euler angles (nadir reference frame)
77   // theta = -1000.;    theta = -1000.;
78   // phi = -1000.;    phi = -1000.;
79   // etha = -1000.;    etha = -1000.;
80    
81    // Euler angles (local field reference frame)    // Euler angles (local field reference frame)
82    //thetamag = -1000.;    //  thetamag = -1000.;
83   // phimag = -1000.;    //  phimag = -1000.;
84    //ethamag = -1000.;    //  ethamag = -1000.;
85    
86      pamzenitangle = -1000.;
87      pamBangle = -1000.;
88    
89    
90    std::fill_n(goodAttitude, 5, 0);    mode = 0;
91      //  std::fill_n(goodAttitude, 5, 0);
92  }  }
93    
94  /**  /**
# Line 139  void OrbitalInfo::GetLevel2Struct(cOrbit Line 131  void OrbitalInfo::GetLevel2Struct(cOrbit
131    l2->q3 = q3;    l2->q3 = q3;
132    
133    // Euler angles (nadir reference frame)    // Euler angles (nadir reference frame)
134   // l2->theta = theta;    l2->theta = theta;
135   // l2->phi = phi;    l2->phi = phi;
136   // l2->etha = etha;    l2->etha = etha;
137    
138      l2->mode = mode;
139    // Euler angles (local field reference frame)    // Euler angles (local field reference frame)
140   // l2->thetamag = thetamag;  //   l2->thetamag = thetamag;
141   // l2->phimag = phimag;  //   l2->phimag = phimag;
142   // l2->ethamag = ethamag;  //   l2->ethamag = ethamag;
143    
144    memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));  //   memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));
145  }  }
146    
147  void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){  void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){
# Line 188  void OrbitalInfo::SetFromLevel2Struct(cO Line 181  void OrbitalInfo::SetFromLevel2Struct(cO
181    q3 = l2->q3;    q3 = l2->q3;
182    
183    // Euler angles (nadir reference frame)    // Euler angles (nadir reference frame)
184    //theta = l2->theta;    theta = l2->theta;
185    //phi = l2->phi;    phi = l2->phi;
186    //etha = l2->etha;    etha = l2->etha;
187    
188      mode = l2->mode;
189    // Euler angles (local field reference frame)    // Euler angles (local field reference frame)
190    //thetamag = l2->thetamag;  //   thetamag = l2->thetamag;
191    //phimag = l2->phimag;  //   phimag = l2->phimag;
192    //ethamag = l2->ethamag;  //   ethamag = l2->ethamag;
193    
194    memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));  //   memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
195  }  }
196    
 ClassImp(OrbitalInfo)  
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