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(const OrbitalInfoTrkVar&);
    OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;};
    //
    void Clear(Option_t *t=""); 
    void Delete(Option_t *t=""); //ELENA
    //
    ClassDef(OrbitalInfoTrkVar, 3);
    //
};
        

/**
 * 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
  
  //tested linear quaternions
  
  Float_t q0t;
  Float_t q1t;
  Float_t q2t;
  Float_t q3t;

  // 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
                // -10 - means we use recovered quaternions
  
  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
  Bool_t R10r;  //if true we recognize R10 mode using recovered data
  
  Float_t TimeGap; //Time gap between two points where interpolation have done.
  
  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, 8);
};
#endif
1	#ifndef OrbitalInfo_h
2	#define OrbitalInfo_h
3
4	#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 {
42	private:
43
44	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();
147	~OrbitalInfo(){Delete();}; //ELENA
148	//
149	OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena
150	void Delete(Option_t *t=""); //ELENA
151	void Set();//ELENA
152	//
153	//
154
155	void Clear(Option_t *t=""); // emiliano
156	//
157	ClassDef(OrbitalInfo, 8);
158	};
159	#endif