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#ifndef OrbitalInfoStruct_h |
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#define OrbitalInfoStruct_h |
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|
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#include <TVector3.h> |
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#include<TMatrixD.h> |
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|
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struct cOrbitalInfo { |
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|
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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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// Position |
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Float_t lon; // degree from -180 to 180 |
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Float_t lat; // degree from -90 to 90 |
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Float_t alt; // meters |
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|
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TVector3 V; // Velocity |
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|
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TMatrixD Iij; |
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|
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Float_t londip; |
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Float_t latdip; |
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|
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// Magnetic field |
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|
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// components (gauss) |
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Float_t Bnorth; |
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Float_t Beast; |
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Float_t Bdown; |
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|
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// abs value (guass) |
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Float_t Babs; |
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|
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//Earth dipole moment |
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|
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Float_t M; |
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|
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// Minimum along the field line (that is at the magnetic equator) |
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Float_t BB0; |
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|
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// Distance of the magnetic equator in earth radii |
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Float_t L; |
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|
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Float_t cutoffsvl; |
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|
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// Quaternions |
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Float_t q0, q1, q2, q3; |
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|
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// Euler angles (nadir reference frame) |
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Float_t theta, phi, etha; |
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|
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// quality of orientation information |
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Int_t mode; |
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Int_t qkind; |
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Int_t errq; |
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Int_t azim; |
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Int_t rtqual; |
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|
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void InitcOrbitalInfo(){ |
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abstime = 0; |
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obt = 0; |
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pkt_num = 0; |
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} |
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}; |
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|
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#endif |