/[PAMELA software]/DarthVader/OrbitalInfo/inc/OrbitalInfo.h
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revision 1.11 by mocchiut, Sun Mar 18 20:22:56 2007 UTC revision 1.18 by mocchiut, Tue Nov 11 10:46:42 2008 UTC
# Line 2  Line 2 
2  #define OrbitalInfo_h  #define OrbitalInfo_h
3    
4  #include <TObject.h>  #include <TObject.h>
5    #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* GetOrbitalInfoTrkVar(){return this;};
26        //
27        void Clear(Option_t *t="");
28        void Delete(Option_t *t=""); //ELENA
29        //
30        ClassDef(OrbitalInfoTrkVar, 2);
31        //
32    };
33            
34    
35    
36  /**  /**
37   * Class that stores position, time, inclination, magnetic field and   * Class that stores position, time, inclination, magnetic field and
38   * cutoff informations.   * cutoff informations.
39   */   */
40  class OrbitalInfo : public TObject {  class OrbitalInfo : public TObject {
41     private:
42    
43   public:   public:
44    OrbitalInfo();    TClonesArray *OrbitalInfoTrk;
   OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena  
45    
46    UInt_t absTime; ///< Absolute Time (seconds)    UInt_t absTime; ///< Absolute Time (seconds)
47    UInt_t OBT; ///< On Board Time (ms)    UInt_t OBT; ///< On Board Time (ms)
# Line 32  class OrbitalInfo : public TObject { Line 62  class OrbitalInfo : public TObject {
62    
63    Float_t L; ///< McIlwain's L shell (in earth radii)    Float_t L; ///< McIlwain's L shell (in earth radii)
64    
65    //! Dipolar magnetic coordinates (not used).  /*   // Dipolar magnetic coordinates (not used). */
66    Float_t londip; ///< degrees from -180 to 180  /*   Float_t londip; ///< degrees from -180 to 180 */
67    Float_t latdip; ///< degrees from -90 to 90  /*   Float_t latdip; ///< degrees from -90 to 90 */
68    Float_t altdip; ///< meters  /*   Float_t altdip; ///< meters */
69    
70    //! Corrected magnetic coordinates (not used).  /*   // Corrected magnetic coordinates (not used). */
71    Float_t loncgm; ///< degrees from -180 to 180  /*   Float_t loncgm; ///< degrees from -180 to 180 */
72    Float_t latcgm; ///< degrees from -90 to 90  /*   Float_t latcgm; ///< degrees from -90 to 90 */
73    Float_t altcgm; ///< meters  /*   Float_t altcgm; ///< meters */
74    
75    //! Corrected B min magnetic coordinates (not used).  /*   // Corrected B min magnetic coordinates (not used). */
76    Float_t loncbm; ///< degrees from -180 to 180  /*   Float_t loncbm; ///< degrees from -180 to 180 */
77    Float_t latcbm; ///< degrees from -90 to 90  /*   Float_t latcbm; ///< degrees from -90 to 90 */
78    Float_t altcbm; ///< meters  /*   Float_t altcbm; ///< meters */
79    
80    Float_t cutoff[20];       //  Float_t cutoff[17];
81      Float_t cutoffsvl;
82    //! Quaternions  
83    Float_t q0, q1, q2, q3;    // Quaternions
84      Float_t q0; ///< Quaternion 0
85    //! Euler angles (nadir reference frame) (not used)    Float_t q1; ///< Quaternion 1
86    //  Float_t theta, phi, etha;    Float_t q2; ///< Quaternion 2
87      Float_t q3; ///< Quaternion 3
88    //! Euler angles (local field reference frame) (not used)  
89    //  Float_t thetamag, phimag, ethamag;    // Euler angles (Resurs velocity reference frame)
90      Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
91    Float_t roll;    Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)
92    Float_t pitch;    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
93    Float_t yaw;  
94      // Pitch angles
95    Int_t mode;        //  Float_t pamzenitangle;
96          //  Float_t pamBangle;
97    // Useful?    //
98    Int_t goodAttitude[5];    TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
99    
100    /**    /**
101       * The variable mode means a character time distant between two quaternions, inside which stay every events  
102       */
103      Int_t mode;   // 0  - means that time different pair of quaternions exuals to 0.25 seconds in R10 mode
104                    //      (it mean that all quaternions in array is correct)
105                    // 1  - means that we have R10 mode and use just first value of quaternions array
106                    // 2  - means that we have non R10 mode and use every quaternions from array.
107                    // 3  - means normal transition from R10 to non R10 or from non R10 to R10.
108                    // 4  - means that we have eliminable hole between R10 and non R10 or between non R10 and R10
109                    // 5  - means that we have uneliminable hole between R10 and non R10 or between non R10 and R10
110                    // 6  - means that we have eliminable hole inside R10 (in such keys eliminable depends from other factors also)
111                    // 7  - means that we have uneliminable hole inside R10
112                    // 8  - means that we have eliminable hole inside non R10
113                    // 9  - means that we have uneliminable hole inside non R10
114                    // 10 - means other unknown problems
115      
116      Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
117      /**
118       \return Returns the B minimum along the field line.       \return Returns the B minimum along the field line.
119    */    */
120    Float_t GetB0() { return Babs/BB0; };    Float_t GetB0() { return Babs/BB0; };
# Line 76  class OrbitalInfo : public TObject { Line 123  class OrbitalInfo : public TObject {
123       \return Returns the Stormer vertical cutoff using L shell:       \return Returns the Stormer vertical cutoff using L shell:
124       14.9/L^2 (GV/c).       14.9/L^2 (GV/c).
125    */    */
126    Float_t GetCutoffSVL() { return cutoff[0]; };    Float_t GetCutoffSVL() { return cutoffsvl; };
127    
128    void SetFromLevel2Struct(cOrbitalInfo *l2);    void SetFromLevel2Struct(cOrbitalInfo *l2);
129    void GetLevel2Struct(cOrbitalInfo *l2) const;    void GetLevel2Struct(cOrbitalInfo *l2) const;
130      OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
131      //
132      OrbitalInfo();
133      ~OrbitalInfo(){Delete();}; //ELENA
134      //
135      OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
136      void Delete(Option_t *t=""); //ELENA
137      void Set();//ELENA
138      //
139      //
140    
141    void Clear(); // emiliano    void Clear(Option_t *t=""); // emiliano
142    //    //
143    ClassDef(OrbitalInfo, 2)    ClassDef(OrbitalInfo, 7);
144  };  };
145  #endif  #endif
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