| 68 |
Int_t fYomin; ///< last plane [0,11] for which the trajectory MUST be contained in section YO. Default 1000 means all the planes, if less than 10 events can be only partially contained in a section (NB: THIS INTRODUCE AN ENERGY DEPENDENT SELECTION CONTAINMENT EFFICIENCY) |
Int_t fYomin; ///< last plane [0,11] for which the trajectory MUST be contained in section YO. Default 1000 means all the planes, if less than 10 events can be only partially contained in a section (NB: THIS INTRODUCE AN ENERGY DEPENDENT SELECTION CONTAINMENT EFFICIENCY) |
| 69 |
Int_t fYemin; ///< last plane [0,11] for which the trajectory MUST be contained in section YE. Default 1000 means all the planes, if less than 10 events can be only partially contained in a section (NB: THIS INTRODUCE AN ENERGY DEPENDENT SELECTION CONTAINMENT EFFICIENCY) |
Int_t fYemin; ///< last plane [0,11] for which the trajectory MUST be contained in section YE. Default 1000 means all the planes, if less than 10 events can be only partially contained in a section (NB: THIS INTRODUCE AN ENERGY DEPENDENT SELECTION CONTAINMENT EFFICIENCY) |
| 70 |
Bool_t indep; ///< flag to switch between INDEPENDENT or COHERENT mode, default false - COHERENT mode selected |
Bool_t indep; ///< flag to switch between INDEPENDENT or COHERENT mode, default false - COHERENT mode selected |
| 71 |
|
Float_t X0pl; ///< transversed X0 for each W plane taking into account inclination of the trajectory |
| 72 |
// |
// |
| 73 |
// conversion factors |
// conversion factors |
| 74 |
// |
// |
| 275 |
Int_t GetColumn(){return fColumn;}; ///< number of column which contains the track |
Int_t GetColumn(){return fColumn;}; ///< number of column which contains the track |
| 276 |
Int_t GetColumn(TString section); ///< number of column which contains the track for section "section" |
Int_t GetColumn(TString section); ///< number of column which contains the track for section "section" |
| 277 |
// |
// |
| 278 |
|
Float_t Get_X0pl(){return X0pl;}; ///< transversed X0 for each W plane taking into account inclination of the trajectory |
| 279 |
|
Float_t GetX0max(){ return x0max;}; ///< get the given X0 (test purpose only) |
| 280 |
|
// |
| 281 |
// Get pointers |
// Get pointers |
| 282 |
// |
// |
| 283 |
CaloLong* GetCaloLong(){return clong;}; ///< Get calolong object. |
CaloLong* GetCaloLong(){return clong;}; ///< Get calolong object. |
| 296 |
void Print(); ///< Print variables on STDOUT |
void Print(); ///< Print variables on STDOUT |
| 297 |
void Print(Option_t *option){Print();}; ///< compatibility with TObject |
void Print(Option_t *option){Print();}; ///< compatibility with TObject |
| 298 |
// |
// |
| 299 |
ClassDef(CaloEnergy,2); |
ClassDef(CaloEnergy,3); |
| 300 |
}; |
}; |
| 301 |
|
|
| 302 |
#endif |
#endif |