/[PAMELA software]/DarthVader/OrbitalInfo/inc/OrbitalInfo.h
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revision 1.11 by mocchiut, Sun Mar 18 20:22:56 2007 UTC revision 1.27 by malakhov, Tue Mar 3 10:57:59 2015 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    #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   * Class that stores position, time, inclination, magnetic field and
43   * cutoff informations.   * cutoff informations.
44   */   */
45  class OrbitalInfo : public TObject {  class OrbitalInfo : public TObject {
46     private:
47    
48   public:   public:
49    OrbitalInfo();    TClonesArray *OrbitalInfoTrk;
   OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena  
50    
51    UInt_t absTime; ///< Absolute Time (seconds)    UInt_t absTime; ///< Absolute Time (seconds)
52    UInt_t OBT; ///< On Board Time (ms)    UInt_t OBT; ///< On Board Time (ms)
# Line 21  class OrbitalInfo : public TObject { Line 56  class OrbitalInfo : public TObject {
56    Float_t lat; ///< degrees from -90 to 90    Float_t lat; ///< degrees from -90 to 90
57    Float_t alt; ///< meters asl    Float_t alt; ///< meters asl
58    
59      TVector3 V;  /// velocity
60    
61    // B components.    // B components.
62    Float_t Bnorth; ///< gauss    Float_t Bnorth; ///< gauss
63    Float_t Beast; ///< gauss    Float_t Beast; ///< gauss
# Line 28  class OrbitalInfo : public TObject { Line 65  class OrbitalInfo : public TObject {
65    
66    Float_t Babs; ///< abs value (guass)    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    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)    Float_t L; ///< McIlwain's L shell (in earth radii)
73    
74    //! Dipolar magnetic coordinates (not used).  /*   // Dipolar magnetic coordinates (not used). */
75    Float_t londip; ///< degrees from -180 to 180     Float_t londip; ///< degrees from -180 to 180
76    Float_t latdip; ///< degrees from -90 to 90     Float_t latdip; ///< degrees from -90 to 90
77    Float_t altdip; ///< meters  
78         //  Float_t cutoff[17];
79    //! Corrected magnetic coordinates (not used).    Float_t cutoffsvl;
80    Float_t loncgm; ///< degrees from -180 to 180    Float_t igrf_icode;
81    Float_t latcgm; ///< degrees from -90 to 90  
82    Float_t altcgm; ///< meters    // linear Quaternions
83      Float_t q0; ///< Quaternion 0
84    //! Corrected B min magnetic coordinates (not used).    Float_t q1; ///< Quaternion 1
85    Float_t loncbm; ///< degrees from -180 to 180    Float_t q2; ///< Quaternion 2
86    Float_t latcbm; ///< degrees from -90 to 90    Float_t q3; ///< Quaternion 3
87    Float_t altcbm; ///< meters  
88      // Euler angles (Resurs velocity reference frame)
89    Float_t cutoff[20];    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    //! Quaternions    // Pitch angles
   Float_t q0, q1, q2, q3;  
94    
95    //! Euler angles (nadir reference frame) (not used)    //
96    //  Float_t theta, phi, etha;    TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
   
   //! Euler angles (local field reference frame) (not used)  
   //  Float_t thetamag, phimag, ethamag;  
   
   Float_t roll;  
   Float_t pitch;  
   Float_t yaw;  
   
   Int_t mode;  
   
   // Useful?  
   Int_t goodAttitude[5];  
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                    // -1 - Very Strange flight data, I don't know how to understand them
126    
127      Int_t rtqual; // 0 - means orientation data for period whe this event registered is in agreement with fligh orioentation data, one can fully trust such event when it calculated using Rotation Table (qkind=1)
128                    // 1 - means orientation data was not compared with flight data (during of absence of them), one should check them somehow
129                    // 2 - means orientation data calculated with flight data has disagreement with rotation table data and thre were not enough of flight data to correct RT.
130      
131      Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
132      /**
133       \return Returns the B minimum along the field line.       \return Returns the B minimum along the field line.
134    */    */
135    Float_t GetB0() { return Babs/BB0; };    Float_t GetB0() { return Babs/BB0; };
# Line 76  class OrbitalInfo : public TObject { Line 138  class OrbitalInfo : public TObject {
138       \return Returns the Stormer vertical cutoff using L shell:       \return Returns the Stormer vertical cutoff using L shell:
139       14.9/L^2 (GV/c).       14.9/L^2 (GV/c).
140    */    */
141    Float_t GetCutoffSVL() { return cutoff[0]; };    Float_t GetCutoffSVL() { return cutoffsvl; };
142    
143    void SetFromLevel2Struct(cOrbitalInfo *l2);    void SetFromLevel2Struct(cOrbitalInfo *l2);
144    void GetLevel2Struct(cOrbitalInfo *l2) const;    void GetLevel2Struct(cOrbitalInfo *l2) const;
145      OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
146      OrbitalInfoTrkVar * GetOrbitalInfoStoredTrack(Int_t seqno);///< returns pointer to the track set related to the seqno number
147    
148      //
149      OrbitalInfo();
150      ~OrbitalInfo(){Delete();}; //ELENA
151      //
152      OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
153      void Delete(Option_t *t=""); //ELENA
154      void Set();//ELENA
155      //
156      //
157      TClonesArray *GetTrackArray(){return OrbitalInfoTrk;} ///< returns a pointer to the track related variables array
158      TClonesArray** GetPointerToTrackArray(){return &OrbitalInfoTrk;}///< returns pointer to pointer to the track array
159      void SetTrackArray(TClonesArray *track);///<set pointer to the track array
160    
161    void Clear(); // emiliano    void Clear(Option_t *t=""); // emiliano
162    //    //
163    ClassDef(OrbitalInfo, 2)    ClassDef(OrbitalInfo, 11);
164  };  };
165  #endif  #endif
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