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

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revision 1.2 by mocchiut, Wed Jun 14 09:52:53 2006 UTC revision 1.22 by mocchiut, Thu Apr 12 12:27:00 2012 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      Float_t igrf_icode;
84    
85      // linear Quaternions
86      Float_t q0; ///< Quaternion 0
87      Float_t q1; ///< Quaternion 1
88      Float_t q2; ///< Quaternion 2
89      Float_t q3; ///< Quaternion 3
90      
91      //tested sine quaternions
92      
93      //Float_t q0t;
94      //Float_t q1t;
95      //Float_t q2t;
96      //Float_t q3t;
97    
98      // Euler angles (Resurs velocity reference frame)
99      Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
100      Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)
101      Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
102    
103      // Pitch angles
104          //  Float_t pamzenitangle;
105          //  Float_t pamBangle;
106      //
107      TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
108    
109      /**
110       * The variable mode means a character time distant between two quaternions, inside which stay every events  
111       */
112      Int_t mode;   // 0  - means that time different pair of quaternions exuals to 0.25 seconds in R10 mode
113                    //      (it mean that all quaternions in array is correct)
114                    // 1  - means that we have R10 mode and use just first value of quaternions array
115                    // 2  - means that we have non R10 mode and use every quaternions from array.
116                    // 3  - means normal transition from R10 to non R10 or from non R10 to R10.
117                    // 4  - means that we have eliminable hole between R10 and non R10 or between non R10 and R10
118                    // 5  - means that we have uneliminable hole between R10 and non R10 or between non R10 and R10
119                    // 6  - means that we have eliminable hole inside R10 (in such keys eliminable depends from other factors also)
120                    // 7  - means that we have uneliminable hole inside R10
121                    // 8  - means that we have eliminable hole inside non R10
122                    // 9  - means that we have uneliminable hole inside non R10
123                    // 10 - means other unknown problems
124                    // -10 - means we use recovered quaternions
125      
126      //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
127      //Bool_t R10r;        //if true we recognize R10 mode using recovered data
128      
129      Float_t TimeGap; //Time gap between two points where interpolation have done.
130      
131      Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
132      /**
133         \return Returns the B minimum along the field line.
134      */
135      Float_t GetB0() { return Babs/BB0; };
136    
137      /**
138         \return Returns the Stormer vertical cutoff using L shell:
139         14.9/L^2 (GV/c).
140      */
141      Float_t GetCutoffSVL() { return cutoffsvl; };
142    
143      void SetFromLevel2Struct(cOrbitalInfo *l2);
144      void GetLevel2Struct(cOrbitalInfo *l2) const;
145      OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
146      //
147    OrbitalInfo();    OrbitalInfo();
148      ~OrbitalInfo(){Delete();}; //ELENA
149      //
150      OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
151      void Delete(Option_t *t=""); //ELENA
152      void Set();//ELENA
153      //
154      //
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, 9);
159  };  };
160  #endif  #endif
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