/[PAMELA software]/DarthVader/OrbitalInfo/inc/OrbitalInfo.h
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revision 1.12 by mocchiut, Tue Mar 20 20:56:28 2007 UTC revision 1.19 by mocchiut, Thu Dec 11 10:08:15 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(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 32  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, q1, q2, q3;    Float_t q0; ///< Quaternion 0
86      Float_t q1; ///< Quaternion 1
87    // Euler angles (nadir reference frame) (not used)    Float_t q2; ///< Quaternion 2
88    Float_t theta, phi, etha;    Float_t q3; ///< Quaternion 3
89    
90    // Euler angles (local field reference frame) (not used)    // Euler angles (Resurs velocity reference frame)
91    Float_t thetamag, phimag, ethamag;    Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
92      Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)
93    // Useful?    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
94    Int_t goodAttitude[5];  
95      // Pitch angles
96          //  Float_t pamzenitangle;
97          //  Float_t pamBangle;
98      //
99      TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
100    
101    /**    /**
102       * The variable mode means a character time distant between two quaternions, inside which stay every events  
103       */
104      Int_t mode;   // 0  - means that time different pair of quaternions exuals to 0.25 seconds in R10 mode
105                    //      (it mean that all quaternions in array is correct)
106                    // 1  - means that we have R10 mode and use just first value of quaternions array
107                    // 2  - means that we have non R10 mode and use every quaternions from array.
108                    // 3  - means normal transition from R10 to non R10 or from non R10 to R10.
109                    // 4  - means that we have eliminable hole between R10 and non R10 or between non R10 and R10
110                    // 5  - means that we have uneliminable hole between R10 and non R10 or between non R10 and R10
111                    // 6  - means that we have eliminable hole inside R10 (in such keys eliminable depends from other factors also)
112                    // 7  - means that we have uneliminable hole inside R10
113                    // 8  - means that we have eliminable hole inside non R10
114                    // 9  - means that we have uneliminable hole inside non R10
115                    // 10 - means other unknown problems
116      
117      Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
118      /**
119       \return Returns the B minimum along the field line.       \return Returns the B minimum along the field line.
120    */    */
121    Float_t GetB0() { return Babs/BB0; };    Float_t GetB0() { return Babs/BB0; };
# Line 70  class OrbitalInfo : public TObject { Line 124  class OrbitalInfo : public TObject {
124       \return Returns the Stormer vertical cutoff using L shell:       \return Returns the Stormer vertical cutoff using L shell:
125       14.9/L^2 (GV/c).       14.9/L^2 (GV/c).
126    */    */
127    Float_t GetCutoffSVL() { return cutoff[0]; };    Float_t GetCutoffSVL() { return cutoffsvl; };
128    
129    void SetFromLevel2Struct(cOrbitalInfo *l2);    void SetFromLevel2Struct(cOrbitalInfo *l2);
130    void GetLevel2Struct(cOrbitalInfo *l2) const;    void GetLevel2Struct(cOrbitalInfo *l2) const;
131      OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
132      //
133      OrbitalInfo();
134      ~OrbitalInfo(){Delete();}; //ELENA
135      //
136      OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
137      void Delete(Option_t *t=""); //ELENA
138      void Set();//ELENA
139      //
140      //
141    
142    void Clear(); // emiliano    void Clear(Option_t *t=""); // emiliano
143    //    //
144    ClassDef(OrbitalInfo, 2)    ClassDef(OrbitalInfo, 7);
145  };  };
146  #endif  #endif
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