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

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revision 1.4 by mocchiut, Fri Jun 30 09:21:57 2006 UTC revision 1.20 by mocchiut, Fri Jan 29 17:27:56 2010 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    
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
39     * cutoff informations.
40     */
41  class OrbitalInfo : public TObject {  class OrbitalInfo : public TObject {
42     private:
43    
44   public:   public:
45      TClonesArray *OrbitalInfoTrk;
46    
47      UInt_t absTime; ///< Absolute Time (seconds)
48      UInt_t OBT; ///< On Board Time (ms)
49      UInt_t pkt_num; ///< CPU packet number
50    
51      Float_t lon; ///< degrees from -180 to 180
52      Float_t lat; ///< degrees from -90 to 90
53      Float_t alt; ///< meters asl
54    
55      // B components.
56      Float_t Bnorth; ///< gauss
57      Float_t Beast; ///< gauss
58      Float_t Bdown; ///< gauss
59    
60      Float_t Babs; ///< abs value (guass)
61    
62      Float_t BB0; ///< B abs over the B minimum on this field line
63    
64      Float_t L; ///< McIlwain's L shell (in earth radii)
65    
66    /*   // Dipolar magnetic coordinates (not used). */
67    /*   Float_t londip; ///< degrees from -180 to 180 */
68    /*   Float_t latdip; ///< degrees from -90 to 90 */
69    /*   Float_t altdip; ///< meters */
70    
71    /*   // Corrected magnetic coordinates (not used). */
72    /*   Float_t loncgm; ///< degrees from -180 to 180 */
73    /*   Float_t latcgm; ///< degrees from -90 to 90 */
74    /*   Float_t altcgm; ///< meters */
75    
76    /*   // Corrected B min magnetic coordinates (not used). */
77    /*   Float_t loncbm; ///< degrees from -180 to 180 */
78    /*   Float_t latcbm; ///< degrees from -90 to 90 */
79    /*   Float_t altcbm; ///< meters */
80    
81         //  Float_t cutoff[17];
82      Float_t cutoffsvl;
83    
84      // Quaternions
85      Float_t q0; ///< Quaternion 0
86      Float_t q1; ///< Quaternion 1
87      Float_t q2; ///< Quaternion 2
88      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)
98      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)
100      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  
110       */
111      Int_t mode;   // 0  - means that time different pair of quaternions exuals to 0.25 seconds in R10 mode
112                    //      (it mean that all quaternions in array is correct)
113                    // 1  - means that we have R10 mode and use just first value of quaternions array
114                    // 2  - means that we have non R10 mode and use every quaternions from array.
115                    // 3  - means normal transition from R10 to non R10 or from non R10 to R10.
116                    // 4  - means that we have eliminable hole between R10 and non R10 or between non R10 and R10
117                    // 5  - means that we have uneliminable hole between R10 and non R10 or between non R10 and R10
118                    // 6  - means that we have eliminable hole inside R10 (in such keys eliminable depends from other factors also)
119                    // 7  - means that we have uneliminable hole inside R10
120                    // 8  - means that we have eliminable hole inside non R10
121                    // 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.
133      */
134      Float_t GetB0() { return Babs/BB0; };
135    
136      /**
137         \return Returns the Stormer vertical cutoff using L shell:
138         14.9/L^2 (GV/c).
139      */
140      Float_t GetCutoffSVL() { return cutoffsvl; };
141    
142      void SetFromLevel2Struct(cOrbitalInfo *l2);
143      void GetLevel2Struct(cOrbitalInfo *l2) const;
144      OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
145      //
146    OrbitalInfo();    OrbitalInfo();
147      ~OrbitalInfo(){Delete();}; //ELENA
148      //
149    OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena    OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
150      void Delete(Option_t *t=""); //ELENA
151    ULong64_t absTime; //< Absolute Time    void Set();//ELENA
152    // EM: added On Board Time and CPU Packet Number    //
   ULong64_t OBT; //< On Board Time  
   ULong64_t pkt_num; //< CPU packet number  
153    //    //
154    void Clear(); // emiliano  
155      void Clear(Option_t *t=""); // emiliano
156    //    //
157    ClassDef(OrbitalInfo, 1)    ClassDef(OrbitalInfo, 8);
158  };  };
159  #endif  #endif
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