/[PAMELA software]/DarthVader/OrbitalInfo/inc/OrbitalInfo.h
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revision 1.21 by mocchiut, Mon Feb 15 21:26:53 2010 UTC revision 1.25 by pam-ts, Tue Sep 16 08:16:02 2014 UTC
# Line 6  Line 6 
6  #include <OrbitalInfoStruct.h>  #include <OrbitalInfoStruct.h>
7  #include <TClonesArray.h>  #include <TClonesArray.h>
8  #include <TMatrixD.h>  #include <TMatrixD.h>
9    #include <TVector3.h>
10    
11  class OrbitalInfoTrkVar : public TObject {  class OrbitalInfoTrkVar : public TObject {
12   private:   private:
# Line 15  class OrbitalInfoTrkVar : public TObject Line 16  class OrbitalInfoTrkVar : public TObject
16      Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ...      Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ...
17      //      //
18      Float_t pitch; ///< Pitch angle      Float_t pitch; ///< Pitch angle
19        Float_t sunangle;
20        Float_t sunmagangle;
21      //      //
22      TMatrixD Eij; ///< vector of incoming particle respect to cartesian geographic coordinates      TMatrixD Eij; ///< vector of incoming particle respect to cartesian geographic coordinates
23      TMatrixD Sij; ///< vector of incoming particle respect to flight coordinates      TMatrixD Sij; ///< vector of incoming particle respect to flight coordinates
# Line 52  class OrbitalInfo : public TObject { Line 55  class OrbitalInfo : public TObject {
55    Float_t lat; ///< degrees from -90 to 90    Float_t lat; ///< degrees from -90 to 90
56    Float_t alt; ///< meters asl    Float_t alt; ///< meters asl
57    
58      TVector3 V;  /// velocity
59    
60    // B components.    // B components.
61    Float_t Bnorth; ///< gauss    Float_t Bnorth; ///< gauss
62    Float_t Beast; ///< gauss    Float_t Beast; ///< gauss
# Line 59  class OrbitalInfo : public TObject { Line 64  class OrbitalInfo : public TObject {
64    
65    Float_t Babs; ///< abs value (guass)    Float_t Babs; ///< abs value (guass)
66    
67      Float_t M;   ///< M
68    
69    Float_t BB0; ///< B abs over the B minimum on this field line    Float_t BB0; ///< B abs over the B minimum on this field line
70    
71    Float_t L; ///< McIlwain's L shell (in earth radii)    Float_t L; ///< McIlwain's L shell (in earth radii)
72    
73  /*   // Dipolar magnetic coordinates (not used). */  /*   // Dipolar magnetic coordinates (not used). */
74  /*   Float_t londip; ///< degrees from -180 to 180 */     Float_t londip; ///< degrees from -180 to 180
75  /*   Float_t latdip; ///< degrees from -90 to 90 */     Float_t latdip; ///< degrees from -90 to 90
 /*   Float_t altdip; ///< meters */  
   
 /*   // Corrected magnetic coordinates (not used). */  
 /*   Float_t loncgm; ///< degrees from -180 to 180 */  
 /*   Float_t latcgm; ///< degrees from -90 to 90 */  
 /*   Float_t altcgm; ///< meters */  
   
 /*   // Corrected B min magnetic coordinates (not used). */  
 /*   Float_t loncbm; ///< degrees from -180 to 180 */  
 /*   Float_t latcbm; ///< degrees from -90 to 90 */  
 /*   Float_t altcbm; ///< meters */  
76    
77       //  Float_t cutoff[17];       //  Float_t cutoff[17];
78    Float_t cutoffsvl;    Float_t cutoffsvl;
79      Float_t igrf_icode;
80    
81    // linear Quaternions    // linear Quaternions
82    Float_t q0; ///< Quaternion 0    Float_t q0; ///< Quaternion 0
83    Float_t q1; ///< Quaternion 1    Float_t q1; ///< Quaternion 1
84    Float_t q2; ///< Quaternion 2    Float_t q2; ///< Quaternion 2
85    Float_t q3; ///< Quaternion 3    Float_t q3; ///< Quaternion 3
     
   //tested sine quaternions  
     
   //Float_t q0t;  
   //Float_t q1t;  
   //Float_t q2t;  
   //Float_t q3t;  
86    
87    // Euler angles (Resurs velocity reference frame)    // Euler angles (Resurs velocity reference frame)
88    Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)    Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
# Line 100  class OrbitalInfo : public TObject { Line 90  class OrbitalInfo : public TObject {
90    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
91    
92    // Pitch angles    // Pitch angles
93        //  Float_t pamzenitangle;  
       //  Float_t pamBangle;  
94    //    //
95    TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates    TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
96    
# Line 122  class OrbitalInfo : public TObject { Line 111  class OrbitalInfo : public TObject {
111                  // 10 - means other unknown problems                  // 10 - means other unknown problems
112                  // -10 - means we use recovered quaternions                  // -10 - means we use recovered quaternions
113        
114    //Int_t R10f; //if 1 we recognize R10 mode using flight data if 0 - no R10 mode if -1 we know nothing about R10 mode    Int_t qkind;  // How matrix Qij was got.
115    //Bool_t R10r;        //if true we recognize R10 mode using recovered data                  // 0 means that it was calculated from flight quaternion
116                    // 1 means that it was calculated from Euler angles from Rotation Table
117        
118    Float_t TimeGap; //Time gap between two points where interpolation have done.    Float_t TimeGap; //Time gap between two points where interpolation have done.
119    
120      Int_t errq;   // flag, if errq == 1 then real flight quaternion (not interpolated) incorrect
121      Int_t azim;   // 0 - means everything is ok
122                    // 1 - means azimutal rotations were performed in this moment and in case of absense of flight quaternions orientation calculated here incorrect
123                    // >1  No flight quaternions, no azimuthal rotations, no adequate data from RotationTable, unaccuracy equals to Bank angle of rotetion in this moment
124        
125    Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};    Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
126    /**    /**
# Line 151  class OrbitalInfo : public TObject { Line 146  class OrbitalInfo : public TObject {
146    void Set();//ELENA    void Set();//ELENA
147    //    //
148    //    //
149      TClonesArray *GetTrackArray(){return OrbitalInfoTrk;} ///< returns a pointer to the track related variables array
150      TClonesArray** GetPointerToTrackArray(){return &OrbitalInfoTrk;}///< returns pointer to pointer to the track array
151    
152    void Clear(Option_t *t=""); // emiliano    void Clear(Option_t *t=""); // emiliano
153    //    //
154    ClassDef(OrbitalInfo, 8);    ClassDef(OrbitalInfo, 10);
155  };  };
156  #endif  #endif
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