OrbitalInfo/inc/OrbitalInfo.h

#ifndef OrbitalInfo_h
#define OrbitalInfo_h

#include <TObject.h>
#include <algorithm> // EMILIANO
#include <OrbitalInfoStruct.h>
#include <TClonesArray.h>
#include <TMatrixD.h>

class OrbitalInfoTrkVar : public TObject {
 private:

 public:
    //
    Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ...
    //
    Float_t pitch; ///< Pitch angle
    //
    TMatrixD Eij; ///< vector of incoming particle respect to cartesian geographic coordinates
    TMatrixD Sij; ///< vector of incoming particle respect to flight coordinates
    //
    Float_t cutoff; ///< Calculated cutoff for the incoming particle taking into account particle direction
    //  
    OrbitalInfoTrkVar();
    OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;};
    //
    void Clear(Option_t *t=""); 
    void Delete(Option_t *t=""); //ELENA
    //
    ClassDef(OrbitalInfoTrkVar, 2);
    //
};
        

/**
 * Class that stores position, time, inclination, magnetic field and
 * cutoff informations.
 */
class OrbitalInfo : public TObject {
 private:

 public:
  TClonesArray *OrbitalInfoTrk;

  UInt_t absTime; ///< Absolute Time (seconds) 
  UInt_t OBT; ///< On Board Time (ms)
  UInt_t pkt_num; ///< CPU packet number 

  Float_t lon; ///< degrees from -180 to 180
  Float_t lat; ///< degrees from -90 to 90
  Float_t alt; ///< meters asl

  // B components.
  Float_t Bnorth; ///< gauss
  Float_t Beast; ///< gauss
  Float_t Bdown; ///< gauss

  Float_t Babs; ///< abs value (guass)

  Float_t BB0; ///< B abs over the B minimum on this field line

  Float_t L; ///< McIlwain's L shell (in earth radii)

/*   // Dipolar magnetic coordinates (not used). */
/*   Float_t londip; ///< degrees from -180 to 180 */
/*   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 */

     //  Float_t cutoff[17];
  Float_t cutoffsvl;

  // Quaternions 
  Float_t q0; ///< Quaternion 0
  Float_t q1; ///< Quaternion 1
  Float_t q2; ///< Quaternion 2
  Float_t q3; ///< Quaternion 3

  // Euler angles (Resurs velocity reference frame) 
  Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
  Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)
  Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)

  // Pitch angles 
      //  Float_t pamzenitangle;
      //  Float_t pamBangle;
  //
  TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates

  /**
   * The variable mode means a character time distant between two quaternions, inside which stay every events  
   */
  Int_t mode;   // 0  - means that time different pair of quaternions exuals to 0.25 seconds in R10 mode
                //      (it mean that all quaternions in array is correct)
                // 1  - means that we have R10 mode and use just first value of quaternions array
                // 2  - means that we have non R10 mode and use every quaternions from array.
                // 3  - means normal transition from R10 to non R10 or from non R10 to R10.
                // 4  - means that we have eliminable hole between R10 and non R10 or between non R10 and R10
                // 5  - means that we have uneliminable hole between R10 and non R10 or between non R10 and R10
                // 6  - means that we have eliminable hole inside R10 (in such keys eliminable depends from other factors also)
                // 7  - means that we have uneliminable hole inside R10
                // 8  - means that we have eliminable hole inside non R10
                // 9  - means that we have uneliminable hole inside non R10
                // 10 - means other unknown problems
  
  Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
  /**
     \return Returns the B minimum along the field line.
  */
  Float_t GetB0() { return Babs/BB0; };

  /**
     \return Returns the Stormer vertical cutoff using L shell:
     14.9/L^2 (GV/c).
  */
  Float_t GetCutoffSVL() { return cutoffsvl; };

  void SetFromLevel2Struct(cOrbitalInfo *l2);
  void GetLevel2Struct(cOrbitalInfo *l2) const;
  OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
  //
  OrbitalInfo();
  ~OrbitalInfo(){Delete();}; //ELENA
  //
  OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
  void Delete(Option_t *t=""); //ELENA
  void Set();//ELENA
  //
  //

  void Clear(Option_t *t=""); // emiliano
  //
  ClassDef(OrbitalInfo, 7);
};
#endif
1	mocchiut	1.1	#ifndef OrbitalInfo_h
2	mocchiut	1.2	#define OrbitalInfo_h
3	mocchiut	1.1
4			#include <TObject.h>
5	mocchiut	1.14	#include <algorithm> // EMILIANO
6	pam-fi	1.5	#include <OrbitalInfoStruct.h>
7	mocchiut	1.16	#include <TClonesArray.h>
8	mocchiut	1.18	#include <TMatrixD.h>
9	mocchiut	1.16
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	mocchiut	1.18	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	mocchiut	1.16	//
24			OrbitalInfoTrkVar();
25			OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;};
26			//
27			void Clear(Option_t *t="");
28	mocchiut	1.18	void Delete(Option_t *t=""); //ELENA
29	mocchiut	1.16	//
30	mocchiut	1.18	ClassDef(OrbitalInfoTrkVar, 2);
31	mocchiut	1.16	//
32			};
33
34
35	mocchiut	1.1
36	pam-rm2	1.9	/**
37			* Class that stores position, time, inclination, magnetic field and
38			* cutoff informations.
39			*/
40	mocchiut	1.1	class OrbitalInfo : public TObject {
41	mocchiut	1.16	private:
42
43	mocchiut	1.1	public:
44	mocchiut	1.16	TClonesArray *OrbitalInfoTrk;
45	mocchiut	1.1
46	mocchiut	1.11	UInt_t absTime; ///< Absolute Time (seconds)
47			UInt_t OBT; ///< On Board Time (ms)
48			UInt_t pkt_num; ///< CPU packet number
49
50			Float_t lon; ///< degrees from -180 to 180
51			Float_t lat; ///< degrees from -90 to 90
52			Float_t alt; ///< meters asl
53	pam-rm2	1.9
54			// B components.
55	mocchiut	1.11	Float_t Bnorth; ///< gauss
56			Float_t Beast; ///< gauss
57			Float_t Bdown; ///< gauss
58	pam-rm2	1.9
59	mocchiut	1.11	Float_t Babs; ///< abs value (guass)
60	pam-rm2	1.9
61	mocchiut	1.11	Float_t BB0; ///< B abs over the B minimum on this field line
62	pam-rm2	1.9
63	mocchiut	1.11	Float_t L; ///< McIlwain's L shell (in earth radii)
64	pam-rm2	1.9
65	mocchiut	1.18	/* // Dipolar magnetic coordinates (not used). */
66			/* Float_t londip; ///< degrees from -180 to 180 */
67			/* Float_t latdip; ///< degrees from -90 to 90 */
68			/* Float_t altdip; ///< meters */
69
70			/* // Corrected magnetic coordinates (not used). */
71			/* Float_t loncgm; ///< degrees from -180 to 180 */
72			/* Float_t latcgm; ///< degrees from -90 to 90 */
73			/* Float_t altcgm; ///< meters */
74
75			/* // Corrected B min magnetic coordinates (not used). */
76			/* Float_t loncbm; ///< degrees from -180 to 180 */
77			/* Float_t latcbm; ///< degrees from -90 to 90 */
78			/* Float_t altcbm; ///< meters */
79	pam-rm2	1.7
80	mocchiut	1.18	// Float_t cutoff[17];
81			Float_t cutoffsvl;
82	pam-rm2	1.7
83	mocchiut	1.12	// Quaternions
84	mocchiut	1.13	Float_t q0; ///< Quaternion 0
85			Float_t q1; ///< Quaternion 1
86			Float_t q2; ///< Quaternion 2
87			Float_t q3; ///< Quaternion 3
88
89			// Euler angles (Resurs velocity reference frame)
90			Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch)
91			Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw)
92			Float_t etha; ///< Euler angle etha in the velocity reference frame (roll)
93	pam-rm2	1.7
94	mocchiut	1.16	// Pitch angles
95	mocchiut	1.18	// Float_t pamzenitangle;
96			// Float_t pamBangle;
97			//
98			TMatrixD Iij; ///< Angle between PAMELA Z direction and cartesian geographic coordinates
99	mocchiut	1.16
100	mocchiut	1.13	/**
101			* The variable mode means a character time distant between two quaternions, inside which stay every events
102			*/
103			Int_t mode; // 0 - means that time different pair of quaternions exuals to 0.25 seconds in R10 mode
104			// (it mean that all quaternions in array is correct)
105			// 1 - means that we have R10 mode and use just first value of quaternions array
106			// 2 - means that we have non R10 mode and use every quaternions from array.
107			// 3 - means normal transition from R10 to non R10 or from non R10 to R10.
108			// 4 - means that we have eliminable hole between R10 and non R10 or between non R10 and R10
109			// 5 - means that we have uneliminable hole between R10 and non R10 or between non R10 and R10
110			// 6 - means that we have eliminable hole inside R10 (in such keys eliminable depends from other factors also)
111			// 7 - means that we have uneliminable hole inside R10
112			// 8 - means that we have eliminable hole inside non R10
113			// 9 - means that we have uneliminable hole inside non R10
114	mocchiut	1.16	// 10 - means other unknown problems
115
116			Int_t ntrk(){return OrbitalInfoTrk->GetEntries();};
117	pam-rm2	1.9	/**
118			\return Returns the B minimum along the field line.
119			*/
120	mocchiut	1.8	Float_t GetB0() { return Babs/BB0; };
121
122	pam-rm2	1.9	/**
123			\return Returns the Stormer vertical cutoff using L shell:
124			14.9/L^2 (GV/c).
125			*/
126	mocchiut	1.18	Float_t GetCutoffSVL() { return cutoffsvl; };
127	pam-rm2	1.7
128	pam-fi	1.5	void SetFromLevel2Struct(cOrbitalInfo *l2);
129			void GetLevel2Struct(cOrbitalInfo *l2) const;
130	mocchiut	1.17	OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack);
131	mocchiut	1.16	//
132			OrbitalInfo();
133			~OrbitalInfo(){Delete();}; //ELENA
134			//
135			OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
136			void Delete(Option_t *t=""); //ELENA
137			void Set();//ELENA
138			//
139			//
140	pam-fi	1.5
141	mocchiut	1.15	void Clear(Option_t *t=""); // emiliano
142	mocchiut	1.4	//
143	mocchiut	1.18	ClassDef(OrbitalInfo, 7);
144	mocchiut	1.1	};
145			#endif