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#ifndef OrbitalInfo_h |
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#define OrbitalInfo_h |
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|
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#include <TObject.h> |
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#include <OrbitalInfoStruct.h> |
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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 { |
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public: |
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OrbitalInfo(); |
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OrbitalInfo* GetOrbitalInfo(){return this;}; // Elena |
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|
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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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|
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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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|
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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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|
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Float_t Babs; ///< abs value (guass) |
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|
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Float_t BB0; ///< B abs over the B minimum on this field line |
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|
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Float_t L; ///< McIlwain's L shell (in earth radii) |
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|
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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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|
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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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|
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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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|
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Float_t cutoff[20]; |
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|
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// Quaternions |
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Float_t q0, q1, q2, q3; |
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// Euler angles (nadir reference frame) (not used) |
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Float_t theta, phi, etha; |
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// Euler angles (local field reference frame) (not used) |
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Float_t thetamag, phimag, ethamag; |
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|
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// Useful? |
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Int_t goodAttitude[5]; |
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|
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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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/** |
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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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|
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void SetFromLevel2Struct(cOrbitalInfo *l2); |
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void GetLevel2Struct(cOrbitalInfo *l2) const; |
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|
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void Clear(); // emiliano |
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// |
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ClassDef(OrbitalInfo, 2) |
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}; |
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#endif |