/[PAMELA software]/DarthVader/OrbitalInfo/inc/OrbitalInfo.h
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revision 1.23 by pam-mep, Thu Jun 7 14:04:00 2012 UTC revision 1.29 by mocchiut, Wed Nov 18 04:58:28 2015 UTC
# Line 6  Line 6 
6  #include <OrbitalInfoStruct.h>  #include <OrbitalInfoStruct.h>
7  #include <TClonesArray.h>  #include <TClonesArray.h>
8  #include <TMatrixD.h>  #include <TMatrixD.h>
9    #include <TVector3.h>
10    #include <string.h>//ELENA
11    
12  class OrbitalInfoTrkVar : public TObject {  class OrbitalInfoTrkVar : public TObject {
13   private:   private:
# Line 15  class OrbitalInfoTrkVar : public TObject Line 17  class OrbitalInfoTrkVar : public TObject
17      Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ...      Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ...
18      //      //
19      Float_t pitch; ///< Pitch angle      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      TMatrixD Eij; ///< vector of incoming particle respect to cartesian geographic coordinates
24      TMatrixD Sij; ///< vector of incoming particle respect to flight coordinates      TMatrixD Sij; ///< vector of incoming particle respect to flight coordinates
# Line 28  class OrbitalInfoTrkVar : public TObject Line 32  class OrbitalInfoTrkVar : public TObject
32      void Clear(Option_t *t="");      void Clear(Option_t *t="");
33      void Delete(Option_t *t=""); //ELENA      void Delete(Option_t *t=""); //ELENA
34      //      //
35      ClassDef(OrbitalInfoTrkVar, 3);      ClassDef(OrbitalInfoTrkVar, 4);
36      //      //
37  };  };
38                    
# Line 52  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 65  class OrbitalInfo : public TObject { Line 71  class OrbitalInfo : public TObject {
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. */
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
 /*   Float_t altdip; ///< meters */  
   
 /*   // Corrected magnetic coordinates (not used). */  
 /*   Float_t loncgm; ///< degrees from -180 to 180 */  
 /*   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 */  
77    
78       //  Float_t cutoff[17];       //  Float_t cutoff[17];
79    Float_t cutoffsvl;    Float_t cutoffsvl;
# Line 89  class OrbitalInfo : public TObject { Line 84  class OrbitalInfo : public TObject {
84    Float_t q1; ///< Quaternion 1    Float_t q1; ///< Quaternion 1
85    Float_t q2; ///< Quaternion 2    Float_t q2; ///< Quaternion 2
86    Float_t q3; ///< Quaternion 3    Float_t q3; ///< Quaternion 3
     
   //tested sine quaternions  
     
   //Float_t q0t;  
   //Float_t q1t;  
   //Float_t q2t;  
   //Float_t q3t;  
87    
88    // Euler angles (Resurs velocity reference frame)    // Euler angles (Resurs velocity reference frame)
89    Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)    Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
# Line 103  class OrbitalInfo : public TObject { Line 91  class OrbitalInfo : public TObject {
91    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)    Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
92    
93    // Pitch angles    // Pitch angles
94        //  Float_t pamzenitangle;  
       //  Float_t pamBangle;  
95    //    //
96    TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates    TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
97    
# Line 125  class OrbitalInfo : public TObject { Line 112  class OrbitalInfo : public TObject {
112                  // 10 - means other unknown problems                  // 10 - means other unknown problems
113                  // -10 - means we use recovered quaternions                  // -10 - means we use recovered quaternions
114        
115    //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    Int_t qkind;  // How matrix Qij was got.
116    //Bool_t R10r;        //if true we recognize R10 mode using recovered data                  // 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.    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();};    Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
132    /**    /**
# Line 145  class OrbitalInfo : public TObject { Line 143  class OrbitalInfo : public TObject {
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);    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();    OrbitalInfo();
150    ~OrbitalInfo(){Delete();}; //ELENA    ~OrbitalInfo(){Delete();}; //ELENA
# Line 154  class OrbitalInfo : public TObject { Line 154  class OrbitalInfo : public TObject {
154    void Set();//ELENA    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(Option_t *t=""); // emiliano    void Clear(Option_t *t=""); // emiliano
162    //    //
163    ClassDef(OrbitalInfo, 9);    ClassDef(OrbitalInfo, 12);
164  };  };
165  #endif  #endif
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