22 |
Float_t cutoff; ///< Calculated cutoff for the incoming particle taking into account particle direction |
Float_t cutoff; ///< Calculated cutoff for the incoming particle taking into account particle direction |
23 |
// |
// |
24 |
OrbitalInfoTrkVar(); |
OrbitalInfoTrkVar(); |
25 |
|
OrbitalInfoTrkVar(const OrbitalInfoTrkVar&); |
26 |
OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;}; |
OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;}; |
27 |
// |
// |
28 |
void Clear(Option_t *t=""); |
void Clear(Option_t *t=""); |
29 |
void Delete(Option_t *t=""); //ELENA |
void Delete(Option_t *t=""); //ELENA |
30 |
// |
// |
31 |
ClassDef(OrbitalInfoTrkVar, 2); |
ClassDef(OrbitalInfoTrkVar, 3); |
32 |
// |
// |
33 |
}; |
}; |
34 |
|
|
81 |
// Float_t cutoff[17]; |
// Float_t cutoff[17]; |
82 |
Float_t cutoffsvl; |
Float_t cutoffsvl; |
83 |
|
|
84 |
// Quaternions |
// linear Quaternions |
85 |
Float_t q0; ///< Quaternion 0 |
Float_t q0; ///< Quaternion 0 |
86 |
Float_t q1; ///< Quaternion 1 |
Float_t q1; ///< Quaternion 1 |
87 |
Float_t q2; ///< Quaternion 2 |
Float_t q2; ///< Quaternion 2 |
88 |
Float_t q3; ///< Quaternion 3 |
Float_t q3; ///< Quaternion 3 |
89 |
|
|
90 |
|
//tested sine 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) |
// Euler angles (Resurs velocity reference frame) |
98 |
Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch) |
Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch) |
120 |
// 8 - means that we have eliminable hole inside non R10 |
// 8 - means that we have eliminable hole inside non R10 |
121 |
// 9 - means that we have uneliminable hole inside non R10 |
// 9 - means that we have uneliminable hole inside non R10 |
122 |
// 10 - means other unknown problems |
// 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();}; |
Int_t ntrk(){return OrbitalInfoTrk->GetEntries();}; |
131 |
/** |
/** |
154 |
|
|
155 |
void Clear(Option_t *t=""); // emiliano |
void Clear(Option_t *t=""); // emiliano |
156 |
// |
// |
157 |
ClassDef(OrbitalInfo, 7); |
ClassDef(OrbitalInfo, 8); |
158 |
}; |
}; |
159 |
#endif |
#endif |