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 |
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90 |
|
//tested linear quaternions |
91 |
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92 |
|
Float_t q0t; |
93 |
|
Float_t q1t; |
94 |
|
Float_t q2t; |
95 |
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Float_t q3t; |
96 |
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|
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 |
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125 |
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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 |
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Bool_t R10r; //if true we recognize R10 mode using recovered data |
127 |
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128 |
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Float_t TimeGap; //Time gap between two points where interpolation have done. |
129 |
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130 |
Int_t ntrk(){return OrbitalInfoTrk->GetEntries();}; |
Int_t ntrk(){return OrbitalInfoTrk->GetEntries();}; |
131 |
/** |
/** |
154 |
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|
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 |