/[PAMELA software]/DarthVader/OrbitalInfo/inc/OrbitalInfo.h
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revision 1.2 by mocchiut, Wed Jun 14 09:52:53 2006 UTC revision 1.26 by pam-fi, Wed Oct 15 12:06:49 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>
7    #include <TClonesArray.h>
8    #include <TMatrixD.h>
9    #include <TVector3.h>
10    #include <string.h>//ELENA
11    
12    class OrbitalInfoTrkVar : public TObject {
13     private:
14    
15     public:
16        //
17        Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ...
18        //
19        Float_t pitch; ///< Pitch angle
20        Float_t sunangle;
21        Float_t sunmagangle;
22        //
23        TMatrixD Eij; ///< vector of incoming particle respect to cartesian geographic coordinates
24        TMatrixD Sij; ///< vector of incoming particle respect to flight coordinates
25        //
26        Float_t cutoff; ///< Calculated cutoff for the incoming particle taking into account particle direction
27        //  
28        OrbitalInfoTrkVar();
29        OrbitalInfoTrkVar(const OrbitalInfoTrkVar&);
30        OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;};
31        //
32        void Clear(Option_t *t="");
33        void Delete(Option_t *t=""); //ELENA
34        //
35        ClassDef(OrbitalInfoTrkVar, 3);
36        //
37    };
38            
39    
40    
41    /**
42     * Class that stores position, time, inclination, magnetic field and
43     * cutoff informations.
44     */
45  class OrbitalInfo : public TObject {  class OrbitalInfo : public TObject {
46     private:
47    
48   public:   public:
49      TClonesArray *OrbitalInfoTrk;
50    
51      UInt_t absTime; ///< Absolute Time (seconds)
52      UInt_t OBT; ///< On Board Time (ms)
53      UInt_t pkt_num; ///< CPU packet number
54    
55      Float_t lon; ///< degrees from -180 to 180
56      Float_t lat; ///< degrees from -90 to 90
57      Float_t alt; ///< meters asl
58    
59      TVector3 V;  /// velocity
60    
61      // B components.
62      Float_t Bnorth; ///< gauss
63      Float_t Beast; ///< gauss
64      Float_t Bdown; ///< gauss
65    
66      Float_t Babs; ///< abs value (guass)
67    
68      Float_t M;   ///< M
69    
70      Float_t BB0; ///< B abs over the B minimum on this field line
71    
72      Float_t L; ///< McIlwain's L shell (in earth radii)
73    
74    /*   // Dipolar magnetic coordinates (not used). */
75       Float_t londip; ///< degrees from -180 to 180
76       Float_t latdip; ///< degrees from -90 to 90
77    
78         //  Float_t cutoff[17];
79      Float_t cutoffsvl;
80      Float_t igrf_icode;
81    
82      // linear Quaternions
83      Float_t q0; ///< Quaternion 0
84      Float_t q1; ///< Quaternion 1
85      Float_t q2; ///< Quaternion 2
86      Float_t q3; ///< Quaternion 3
87    
88      // Euler angles (Resurs velocity reference frame)
89      Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
90      Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)
91      Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
92    
93      // Pitch angles
94    
95      //
96      TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
97    
98      /**
99       * The variable mode means a character time distant between two quaternions, inside which stay every events  
100       */
101      Int_t mode;   // 0  - means that time different pair of quaternions exuals to 0.25 seconds in R10 mode
102                    //      (it mean that all quaternions in array is correct)
103                    // 1  - means that we have R10 mode and use just first value of quaternions array
104                    // 2  - means that we have non R10 mode and use every quaternions from array.
105                    // 3  - means normal transition from R10 to non R10 or from non R10 to R10.
106                    // 4  - means that we have eliminable hole between R10 and non R10 or between non R10 and R10
107                    // 5  - means that we have uneliminable hole between R10 and non R10 or between non R10 and R10
108                    // 6  - means that we have eliminable hole inside R10 (in such keys eliminable depends from other factors also)
109                    // 7  - means that we have uneliminable hole inside R10
110                    // 8  - means that we have eliminable hole inside non R10
111                    // 9  - means that we have uneliminable hole inside non R10
112                    // 10 - means other unknown problems
113                    // -10 - means we use recovered quaternions
114      
115      Int_t qkind;  // How matrix Qij was got.
116                    // 0 means that it was calculated from flight quaternion
117                    // 1 means that it was calculated from Euler angles from Rotation Table
118      
119      Float_t TimeGap; //Time gap between two points where interpolation have done.
120    
121      Int_t errq;   // flag, if errq == 1 then real flight quaternion (not interpolated) incorrect
122      Int_t azim;   // 0 - means everything is ok
123                    // 1 - means azimutal rotations were performed in this moment and in case of absense of flight quaternions orientation calculated here incorrect
124                    // >1  No flight quaternions, no azimuthal rotations, no adequate data from RotationTable, unaccuracy equals to Bank angle of rotetion in this moment
125      
126      Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
127      /**
128         \return Returns the B minimum along the field line.
129      */
130      Float_t GetB0() { return Babs/BB0; };
131    
132      /**
133         \return Returns the Stormer vertical cutoff using L shell:
134         14.9/L^2 (GV/c).
135      */
136      Float_t GetCutoffSVL() { return cutoffsvl; };
137    
138      void SetFromLevel2Struct(cOrbitalInfo *l2);
139      void GetLevel2Struct(cOrbitalInfo *l2) const;
140      OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
141      OrbitalInfoTrkVar * GetOrbitalInfoStoredTrack(Int_t seqno);///< returns pointer to the track set related to the seqno number
142    
143      //
144    OrbitalInfo();    OrbitalInfo();
145      ~OrbitalInfo(){Delete();}; //ELENA
146      //
147      OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
148      void Delete(Option_t *t=""); //ELENA
149      void Set();//ELENA
150      //
151      //
152      TClonesArray *GetTrackArray(){return OrbitalInfoTrk;} ///< returns a pointer to the track related variables array
153      TClonesArray** GetPointerToTrackArray(){return &OrbitalInfoTrk;}///< returns pointer to pointer to the track array
154      void SetTrackArray(TClonesArray *track);///<set pointer to the track array
155    
156    ULong64_t absTime; //< Absolute Time    void Clear(Option_t *t=""); // emiliano
   // EM: added On Board Time and CPU Packet Number  
   ULong64_t OBT; //< On Board Time  
   ULong64_t pkt_num; //< CPU packet number  
157    //    //
158    ClassDef(OrbitalInfo, 1)    ClassDef(OrbitalInfo, 10);
159  };  };
160  #endif  #endif
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