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#define OrbitalInfo_h |
#define OrbitalInfo_h |
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#include <TObject.h> |
#include <TObject.h> |
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#include <algorithm> // EMILIANO |
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#include <OrbitalInfoStruct.h> |
#include <OrbitalInfoStruct.h> |
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#include <TClonesArray.h> |
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class OrbitalInfoTrkVar : public TObject { |
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private: |
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public: |
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// |
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Int_t trkseqno; // tof sequ. number: -1=ToF standalone, 0=first Tracker track, ... |
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// |
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Float_t pitch; |
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// |
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OrbitalInfoTrkVar(); |
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OrbitalInfoTrkVar* GetOrbitalInfoTrkVar(){return this;}; |
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// |
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void Clear(Option_t *t=""); |
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// |
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ClassDef(OrbitalInfoTrkVar, 1); |
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// |
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}; |
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/** |
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* Class that stores position, time, inclination, magnetic field and |
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* cutoff informations. |
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*/ |
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class OrbitalInfo : public TObject { |
class OrbitalInfo : public TObject { |
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private: |
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public: |
public: |
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OrbitalInfo(); |
TClonesArray *OrbitalInfoTrk; |
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OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena |
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UInt_t absTime; ///< Absolute Time (seconds) |
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UInt_t OBT; ///< On Board Time (ms) |
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UInt_t pkt_num; ///< CPU packet number |
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Float_t lon; ///< degrees from -180 to 180 |
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Float_t lat; ///< degrees from -90 to 90 |
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Float_t alt; ///< meters asl |
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// B components. |
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Float_t Bnorth; ///< gauss |
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Float_t Beast; ///< gauss |
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Float_t Bdown; ///< gauss |
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Float_t Babs; ///< abs value (guass) |
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Float_t BB0; ///< B abs over the B minimum on this field line |
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Float_t L; ///< McIlwain's L shell (in earth radii) |
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// Dipolar magnetic coordinates (not used). |
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Float_t londip; ///< degrees from -180 to 180 |
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Float_t latdip; ///< degrees from -90 to 90 |
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Float_t altdip; ///< meters |
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// Corrected magnetic coordinates (not used). |
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Float_t loncgm; ///< degrees from -180 to 180 |
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Float_t latcgm; ///< degrees from -90 to 90 |
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Float_t altcgm; ///< meters |
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// Corrected B min magnetic coordinates (not used). |
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Float_t loncbm; ///< degrees from -180 to 180 |
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Float_t latcbm; ///< degrees from -90 to 90 |
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Float_t altcbm; ///< meters |
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Float_t cutoff[17]; |
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// Quaternions |
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Float_t q0; ///< Quaternion 0 |
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Float_t q1; ///< Quaternion 1 |
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Float_t q2; ///< Quaternion 2 |
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Float_t q3; ///< Quaternion 3 |
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// Euler angles (Resurs velocity reference frame) |
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Float_t theta; ///< Euler angle theta in the velocity reference frame (pitch) |
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Float_t phi; ///< Euler angle phi in the velocity reference frame (yaw) |
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Float_t etha; ///< Euler angle etha in the velocity reference frame (roll) |
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// Pitch angles |
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Float_t pamzenitangle; |
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Float_t pamBangle; |
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/** |
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* The variable mode means a character time distant between two quaternions, inside which stay every events |
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*/ |
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Int_t mode; // 0 - means that time different pair of quaternions exuals to 0.25 seconds in R10 mode |
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// (it mean that all quaternions in array is correct) |
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// 1 - means that we have R10 mode and use just first value of quaternions array |
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// 2 - means that we have non R10 mode and use every quaternions from array. |
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// 3 - means normal transition from R10 to non R10 or from non R10 to R10. |
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// 4 - means that we have eliminable hole between R10 and non R10 or between non R10 and R10 |
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// 5 - means that we have uneliminable hole between R10 and non R10 or between non R10 and R10 |
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// 6 - means that we have eliminable hole inside R10 (in such keys eliminable depends from other factors also) |
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// 7 - means that we have uneliminable hole inside R10 |
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// 8 - means that we have eliminable hole inside non R10 |
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// 9 - means that we have uneliminable hole inside non R10 |
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// 10 - means other unknown problems |
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Int_t ntrk(){return OrbitalInfoTrk->GetEntries();}; |
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/** |
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\return Returns the B minimum along the field line. |
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*/ |
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Float_t GetB0() { return Babs/BB0; }; |
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/** |
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\return Returns the Stormer vertical cutoff using L shell: |
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14.9/L^2 (GV/c). |
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*/ |
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Float_t GetCutoffSVL() { return cutoff[0]; }; |
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ULong64_t absTime; //< Absolute Time |
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// EM: added On Board Time and CPU Packet Number |
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ULong64_t OBT; //< On Board Time |
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ULong64_t pkt_num; //< CPU packet number |
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// |
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void SetFromLevel2Struct(cOrbitalInfo *l2); |
void SetFromLevel2Struct(cOrbitalInfo *l2); |
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void GetLevel2Struct(cOrbitalInfo *l2) const; |
void GetLevel2Struct(cOrbitalInfo *l2) const; |
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OrbitalInfoTrkVar *GetOrbitalInfoTrkVar(Int_t notrack); |
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// |
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OrbitalInfo(); |
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~OrbitalInfo(){Delete();}; //ELENA |
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// |
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OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena |
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void Delete(Option_t *t=""); //ELENA |
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void Set();//ELENA |
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// |
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// |
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void Clear(); // emiliano |
void Clear(Option_t *t=""); // emiliano |
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// |
// |
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ClassDef(OrbitalInfo, 1) |
ClassDef(OrbitalInfo, 6); |
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}; |
}; |
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#endif |
#endif |
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