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

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revision 1.13 by mocchiut, Wed Apr 18 14:06:23 2007 UTC revision 1.25 by pam-ts, Tue Sep 16 08:16:02 2014 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    #include <TVector3.h>
10    
11    class OrbitalInfoTrkVar : public TObject {
12     private:
13    
14     public:
15        //
16        Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ...
17        //
18        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
23        TMatrixD Sij; ///< vector of incoming particle respect to flight coordinates
24        //
25        Float_t cutoff; ///< Calculated cutoff for the incoming particle taking into account particle direction
26        //  
27        OrbitalInfoTrkVar();
28        OrbitalInfoTrkVar(const OrbitalInfoTrkVar&);
29        OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;};
30        //
31        void Clear(Option_t *t="");
32        void Delete(Option_t *t=""); //ELENA
33        //
34        ClassDef(OrbitalInfoTrkVar, 3);
35        //
36    };
37            
38    
39    
40  /**  /**
41   * Class that stores position, time, inclination, magnetic field and   * Class that stores position, time, inclination, magnetic field and
42   * cutoff informations.   * cutoff informations.
43   */   */
44  class OrbitalInfo : public TObject {  class OrbitalInfo : public TObject {
45     private:
46    
47   public:   public:
48    OrbitalInfo();    TClonesArray *OrbitalInfoTrk;
   OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena  
49    
50    UInt_t absTime; ///< Absolute Time (seconds)    UInt_t absTime; ///< Absolute Time (seconds)
51    UInt_t OBT; ///< On Board Time (ms)    UInt_t OBT; ///< On Board Time (ms)
# Line 21  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 28  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
76    Float_t altdip; ///< meters  
77         //  Float_t cutoff[17];
78    // Corrected magnetic coordinates (not used).    Float_t cutoffsvl;
79    Float_t loncgm; ///< degrees from -180 to 180    Float_t igrf_icode;
   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  
80    
81    Float_t cutoff[20];    // linear Quaternions
   
   // 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
# Line 60  class OrbitalInfo : public TObject { Line 89  class OrbitalInfo : public TObject {
89    Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)    Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)
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
93    
94      //
95      TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
96    
97    /**    /**
98     * 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  
99     */     */
# Line 74  class OrbitalInfo : public TObject { Line 108  class OrbitalInfo : public TObject {
108                  // 7  - means that we have uneliminable hole inside R10                  // 7  - means that we have uneliminable hole inside R10
109                  // 8  - means that we have eliminable hole inside non R10                  // 8  - means that we have eliminable hole inside non R10
110                  // 9  - means that we have uneliminable hole inside non R10                  // 9  - means that we have uneliminable hole inside non R10
111                                    // 10 - means other unknown problems
112                    // -10 - means we use recovered quaternions
113      
114      Int_t qkind;  // How matrix Qij was got.
115                    // 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.
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();};
126    /**    /**
127       \return Returns the B minimum along the field line.       \return Returns the B minimum along the field line.
128    */    */
# Line 84  class OrbitalInfo : public TObject { Line 132  class OrbitalInfo : public TObject {
132       \return Returns the Stormer vertical cutoff using L shell:       \return Returns the Stormer vertical cutoff using L shell:
133       14.9/L^2 (GV/c).       14.9/L^2 (GV/c).
134    */    */
135    Float_t GetCutoffSVL() { return cutoff[0]; };    Float_t GetCutoffSVL() { return cutoffsvl; };
136    
137    void SetFromLevel2Struct(cOrbitalInfo *l2);    void SetFromLevel2Struct(cOrbitalInfo *l2);
138    void GetLevel2Struct(cOrbitalInfo *l2) const;    void GetLevel2Struct(cOrbitalInfo *l2) const;
139      OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
140      //
141      OrbitalInfo();
142      ~OrbitalInfo(){Delete();}; //ELENA
143      //
144      OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
145      void Delete(Option_t *t=""); //ELENA
146      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(); // emiliano    void Clear(Option_t *t=""); // emiliano
153    //    //
154    ClassDef(OrbitalInfo, 3)    ClassDef(OrbitalInfo, 10);
155  };  };
156  #endif  #endif
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