/[PAMELA software]/DarthVader/OrbitalInfo/inc/OrbitalInfo.h
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revision 1.17 by mocchiut, Fri Oct 31 15:48:58 2008 UTC revision 1.23 by pam-mep, Thu Jun 7 14:04:00 2012 UTC
# Line 5  Line 5 
5  #include <algorithm> // EMILIANO  #include <algorithm> // EMILIANO
6  #include <OrbitalInfoStruct.h>  #include <OrbitalInfoStruct.h>
7  #include <TClonesArray.h>  #include <TClonesArray.h>
8    #include <TMatrixD.h>
9    
10  class OrbitalInfoTrkVar : public TObject {  class OrbitalInfoTrkVar : public TObject {
11   private:   private:
# Line 13  class OrbitalInfoTrkVar : public TObject Line 14  class OrbitalInfoTrkVar : public TObject
14      //      //
15      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, ...
16      //      //
17      Float_t pitch;      Float_t pitch; ///< Pitch angle
18        //
19        TMatrixD Eij; ///< vector of incoming particle respect to cartesian geographic coordinates
20        TMatrixD Sij; ///< vector of incoming particle respect to flight coordinates
21        //
22        Float_t cutoff; ///< Calculated cutoff for the incoming particle taking into account particle direction
23      //        //  
24      OrbitalInfoTrkVar();      OrbitalInfoTrkVar();
25        OrbitalInfoTrkVar(const OrbitalInfoTrkVar&);
26      OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;};      OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;};
27      //      //
28      void Clear(Option_t *t="");      void Clear(Option_t *t="");
29        void Delete(Option_t *t=""); //ELENA
30      //      //
31      ClassDef(OrbitalInfoTrkVar, 1);      ClassDef(OrbitalInfoTrkVar, 3);
32      //      //
33  };  };
34                    
# Line 51  class OrbitalInfo : public TObject { Line 59  class OrbitalInfo : public TObject {
59    
60    Float_t Babs; ///< abs value (guass)    Float_t Babs; ///< abs value (guass)
61    
62      Float_t M;   ///< M
63    
64    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
65    
66    Float_t L; ///< McIlwain's L shell (in earth radii)    Float_t L; ///< McIlwain's L shell (in earth radii)
67    
68    // Dipolar magnetic coordinates (not used).  /*   // Dipolar magnetic coordinates (not used). */
69    Float_t londip; ///< degrees from -180 to 180  /*   Float_t londip; ///< degrees from -180 to 180 */
70    Float_t latdip; ///< degrees from -90 to 90  /*   Float_t latdip; ///< degrees from -90 to 90 */
71    Float_t altdip; ///< meters  /*   Float_t altdip; ///< meters */
72    
73    // Corrected magnetic coordinates (not used).  /*   // Corrected magnetic coordinates (not used). */
74    Float_t loncgm; ///< degrees from -180 to 180  /*   Float_t loncgm; ///< degrees from -180 to 180 */
75    Float_t latcgm; ///< degrees from -90 to 90  /*   Float_t latcgm; ///< degrees from -90 to 90 */
76    Float_t altcgm; ///< meters  /*   Float_t altcgm; ///< meters */
77    
78    // Corrected B min magnetic coordinates (not used).  /*   // Corrected B min magnetic coordinates (not used). */
79    Float_t loncbm; ///< degrees from -180 to 180  /*   Float_t loncbm; ///< degrees from -180 to 180 */
80    Float_t latcbm; ///< degrees from -90 to 90  /*   Float_t latcbm; ///< degrees from -90 to 90 */
81    Float_t altcbm; ///< meters  /*   Float_t altcbm; ///< meters */
82    
83         //  Float_t cutoff[17];
84      Float_t cutoffsvl;
85      Float_t igrf_icode;
86    
87    Float_t cutoff[17];    // linear Quaternions
   
   // Quaternions  
88    Float_t q0; ///< Quaternion 0    Float_t q0; ///< Quaternion 0
89    Float_t q1; ///< Quaternion 1    Float_t q1; ///< Quaternion 1
90    Float_t q2; ///< Quaternion 2    Float_t q2; ///< Quaternion 2
91    Float_t q3; ///< Quaternion 3    Float_t q3; ///< Quaternion 3
92      
93      //tested sine quaternions
94      
95      //Float_t q0t;
96      //Float_t q1t;
97      //Float_t q2t;
98      //Float_t q3t;
99    
100    // Euler angles (Resurs velocity reference frame)    // Euler angles (Resurs velocity reference frame)
101    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 84  class OrbitalInfo : public TObject { Line 103  class OrbitalInfo : public TObject {
103    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
104    
105    // Pitch angles    // Pitch angles
106    Float_t pamzenitangle;        //  Float_t pamzenitangle;
107    Float_t pamBangle;        //  Float_t pamBangle;
108      //
109      TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
110    
111    /**    /**
112     * The variable mode means a character time distant between two quaternions, inside which stay every events       * The variable mode means a character time distant between two quaternions, inside which stay every events  
# Line 102  class OrbitalInfo : public TObject { Line 123  class OrbitalInfo : public TObject {
123                  // 8  - means that we have eliminable hole inside non R10                  // 8  - means that we have eliminable hole inside non R10
124                  // 9  - means that we have uneliminable hole inside non R10                  // 9  - means that we have uneliminable hole inside non R10
125                  // 10 - means other unknown problems                  // 10 - means other unknown problems
126                    // -10 - means we use recovered quaternions
127      
128      //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
129      //Bool_t R10r;        //if true we recognize R10 mode using recovered data
130      
131      Float_t TimeGap; //Time gap between two points where interpolation have done.
132        
133    Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};    Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
134    /**    /**
# Line 113  class OrbitalInfo : public TObject { Line 140  class OrbitalInfo : public TObject {
140       \return Returns the Stormer vertical cutoff using L shell:       \return Returns the Stormer vertical cutoff using L shell:
141       14.9/L^2 (GV/c).       14.9/L^2 (GV/c).
142    */    */
143    Float_t GetCutoffSVL() { return cutoff[0]; };    Float_t GetCutoffSVL() { return cutoffsvl; };
144    
145    void SetFromLevel2Struct(cOrbitalInfo *l2);    void SetFromLevel2Struct(cOrbitalInfo *l2);
146    void GetLevel2Struct(cOrbitalInfo *l2) const;    void GetLevel2Struct(cOrbitalInfo *l2) const;
# Line 130  class OrbitalInfo : public TObject { Line 157  class OrbitalInfo : public TObject {
157    
158    void Clear(Option_t *t=""); // emiliano    void Clear(Option_t *t=""); // emiliano
159    //    //
160    ClassDef(OrbitalInfo, 6);    ClassDef(OrbitalInfo, 9);
161  };  };
162  #endif  #endif
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