/[PAMELA software]/DarthVader/OrbitalInfo/inc/OrbitalInfo.h
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Diff of /DarthVader/OrbitalInfo/inc/OrbitalInfo.h

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revision 1.15 by mocchiut, Fri Nov 23 16:42:41 2007 UTC revision 1.20 by mocchiut, Fri Jan 29 17:27:56 2010 UTC
# Line 4  Line 4 
4  #include <TObject.h>  #include <TObject.h>
5  #include <algorithm> // EMILIANO  #include <algorithm> // EMILIANO
6  #include <OrbitalInfoStruct.h>  #include <OrbitalInfoStruct.h>
7    #include <TClonesArray.h>
8    #include <TMatrixD.h>
9    
10    class OrbitalInfoTrkVar : public TObject {
11     private:
12    
13     public:
14        //
15        Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ...
16        //
17        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();
25        OrbitalInfoTrkVar(const OrbitalInfoTrkVar&);
26        OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;};
27        //
28        void Clear(Option_t *t="");
29        void Delete(Option_t *t=""); //ELENA
30        //
31        ClassDef(OrbitalInfoTrkVar, 3);
32        //
33    };
34            
35    
36    
37  /**  /**
38   * Class that stores position, time, inclination, magnetic field and   * Class that stores position, time, inclination, magnetic field and
39   * cutoff informations.   * cutoff informations.
40   */   */
41  class OrbitalInfo : public TObject {  class OrbitalInfo : public TObject {
42     private:
43    
44   public:   public:
45    OrbitalInfo();    TClonesArray *OrbitalInfoTrk;
   OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena  
46    
47    UInt_t absTime; ///< Absolute Time (seconds)    UInt_t absTime; ///< Absolute Time (seconds)
48    UInt_t OBT; ///< On Board Time (ms)    UInt_t OBT; ///< On Board Time (ms)
# Line 33  class OrbitalInfo : public TObject { Line 63  class OrbitalInfo : public TObject {
63    
64    Float_t L; ///< McIlwain's L shell (in earth radii)    Float_t L; ///< McIlwain's L shell (in earth radii)
65    
66    // Dipolar magnetic coordinates (not used).  /*   // Dipolar magnetic coordinates (not used). */
67    Float_t londip; ///< degrees from -180 to 180  /*   Float_t londip; ///< degrees from -180 to 180 */
68    Float_t latdip; ///< degrees from -90 to 90  /*   Float_t latdip; ///< degrees from -90 to 90 */
69    Float_t altdip; ///< meters  /*   Float_t altdip; ///< meters */
70    
71    // Corrected magnetic coordinates (not used).  /*   // Corrected magnetic coordinates (not used). */
72    Float_t loncgm; ///< degrees from -180 to 180  /*   Float_t loncgm; ///< degrees from -180 to 180 */
73    Float_t latcgm; ///< degrees from -90 to 90  /*   Float_t latcgm; ///< degrees from -90 to 90 */
74    Float_t altcgm; ///< meters  /*   Float_t altcgm; ///< meters */
75    
76    // Corrected B min magnetic coordinates (not used).  /*   // Corrected B min magnetic coordinates (not used). */
77    Float_t loncbm; ///< degrees from -180 to 180  /*   Float_t loncbm; ///< degrees from -180 to 180 */
78    Float_t latcbm; ///< degrees from -90 to 90  /*   Float_t latcbm; ///< degrees from -90 to 90 */
79    Float_t altcbm; ///< meters  /*   Float_t altcbm; ///< meters */
80    
81    Float_t cutoff[20];       //  Float_t cutoff[17];
82      Float_t cutoffsvl;
83    
84    // Quaternions    // Quaternions
85    Float_t q0; ///< Quaternion 0    Float_t q0; ///< Quaternion 0
86    Float_t q1; ///< Quaternion 1    Float_t q1; ///< Quaternion 1
87    Float_t q2; ///< Quaternion 2    Float_t q2; ///< Quaternion 2
88    Float_t q3; ///< Quaternion 3    Float_t q3; ///< Quaternion 3
89      
90      //tested linear quaternions
91      
92      Float_t q0t;
93      Float_t q1t;
94      Float_t q2t;
95      Float_t q3t;
96    
97    // Euler angles (Resurs velocity reference frame)    // Euler angles (Resurs velocity reference frame)
98    Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)    Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
99    Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)    Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)
100    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
101    
102      // Pitch angles
103          //  Float_t pamzenitangle;
104          //  Float_t pamBangle;
105      //
106      TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
107    
108    /**    /**
109     * 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  
110     */     */
# Line 75  class OrbitalInfo : public TObject { Line 119  class OrbitalInfo : public TObject {
119                  // 7  - means that we have uneliminable hole inside R10                  // 7  - means that we have uneliminable hole inside R10
120                  // 8  - means that we have eliminable hole inside non R10                  // 8  - means that we have eliminable hole inside non R10
121                  // 9  - means that we have uneliminable hole inside non R10                  // 9  - means that we have uneliminable hole inside non R10
122                                    // 10 - means other unknown problems
123                    // -10 - means we use recovered quaternions
124      
125      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
126      Bool_t R10r;  //if true we recognize R10 mode using recovered data
127      
128      Float_t TimeGap; //Time gap between two points where interpolation have done.
129      
130      Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
131    /**    /**
132       \return Returns the B minimum along the field line.       \return Returns the B minimum along the field line.
133    */    */
# Line 85  class OrbitalInfo : public TObject { Line 137  class OrbitalInfo : public TObject {
137       \return Returns the Stormer vertical cutoff using L shell:       \return Returns the Stormer vertical cutoff using L shell:
138       14.9/L^2 (GV/c).       14.9/L^2 (GV/c).
139    */    */
140    Float_t GetCutoffSVL() { return cutoff[0]; };    Float_t GetCutoffSVL() { return cutoffsvl; };
141    
142    void SetFromLevel2Struct(cOrbitalInfo *l2);    void SetFromLevel2Struct(cOrbitalInfo *l2);
143    void GetLevel2Struct(cOrbitalInfo *l2) const;    void GetLevel2Struct(cOrbitalInfo *l2) const;
144      OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
145      //
146      OrbitalInfo();
147      ~OrbitalInfo(){Delete();}; //ELENA
148      //
149      OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
150      void Delete(Option_t *t=""); //ELENA
151      void Set();//ELENA
152      //
153      //
154    
155    void Clear(Option_t *t=""); // emiliano    void Clear(Option_t *t=""); // emiliano
156    //    //
157    ClassDef(OrbitalInfo, 3)    ClassDef(OrbitalInfo, 8);
158  };  };
159  #endif  #endif
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