380 lines
10 KiB
Plaintext
380 lines
10 KiB
Plaintext
//
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// ********************************************************************
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// * License and Disclaimer *
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// * *
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// * The Geant4 software is copyright of the Copyright Holders of *
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// * the Geant4 Collaboration. It is provided under the terms and *
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// * conditions of the Geant4 Software License, included in the file *
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// * LICENSE and available at http://cern.ch/geant4/license . These *
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// * include a list of copyright holders. *
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// * *
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// * Neither the authors of this software system, nor their employing *
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// * institutes,nor the agencies providing financial support for this *
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// * work make any representation or warranty, express or implied, *
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// * regarding this software system or assume any liability for its *
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// * use. Please see the license in the file LICENSE and URL above *
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// * for the full disclaimer and the limitation of liability. *
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// * *
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// * This code implementation is the result of the scientific and *
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// * technical work of the GEANT4 collaboration. *
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// * By using, copying, modifying or distributing the software (or *
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// * any work based on the software) you agree to acknowledge its *
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// * use in resulting scientific publications, and indicate your *
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// * acceptance of all terms of the Geant4 Software license. *
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// ********************************************************************
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//
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//
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// $Id: G4FieldTrack.icc,v 1.21 2006/11/13 18:24:35 gcosmo Exp $
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// GEANT4 tag $Name: geant4-09-01 $
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//
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// -------------------------------------------------------------------
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// Implementation methods for the embedded class G4ChargeState
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// ----------------------------
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inline G4FieldTrack::
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G4ChargeState::G4ChargeState(G4double charge,
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G4double magnetic_dipole_moment,
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G4double electric_dipole_moment,
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G4double magnetic_charge)
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{
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fCharge= charge;
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fMagn_dipole= magnetic_dipole_moment;
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fElec_dipole= electric_dipole_moment;
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fMagneticCharge= magnetic_charge;
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}
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inline G4FieldTrack::
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G4ChargeState::G4ChargeState(
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const G4FieldTrack::G4ChargeState& right )
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{
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fCharge= right.fCharge;
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fMagn_dipole= right.fMagn_dipole;
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fElec_dipole= right.fElec_dipole;
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fMagneticCharge= right.fMagneticCharge;
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}
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inline void
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G4FieldTrack::InitialiseSpin( const G4ThreeVector& Spin )
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{
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// static G4ThreeVector ZeroVec(0.0, 0.0, 0.0);
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fSpin = Spin;
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// New Member ?? G4bool fHasSpin;
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// fHasSpin = (fSpin != ZeroVec);
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}
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inline void G4FieldTrack::
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G4ChargeState::SetChargeAndMoments(G4double charge,
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G4double magnetic_dipole_moment,
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G4double electric_dipole_moment,
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G4double magnetic_charge )
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// Revise the charge and potentially all moments.
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// By default do not change mdm, edm, mag charge.
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{
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fCharge= charge;
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if( magnetic_dipole_moment < DBL_MAX) fMagn_dipole= magnetic_dipole_moment;
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if( electric_dipole_moment < DBL_MAX) fElec_dipole= electric_dipole_moment;
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if( magnetic_charge < DBL_MAX) fMagneticCharge= magnetic_charge;
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}
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inline
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G4FieldTrack::G4FieldTrack( const G4FieldTrack& rStVec )
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: fDistanceAlongCurve( rStVec.fDistanceAlongCurve),
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fKineticEnergy( rStVec.fKineticEnergy ),
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fRestMass_c2( rStVec.fRestMass_c2),
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fLabTimeOfFlight( rStVec.fLabTimeOfFlight ),
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fProperTimeOfFlight( rStVec.fProperTimeOfFlight ),
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// fMomentumModulus( rStVec.fMomentumModulus ),
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fSpin( rStVec.fSpin ),
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fMomentumDir( rStVec.fMomentumDir ),
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fChargeState( rStVec.fChargeState )
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{
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SixVector[0]= rStVec.SixVector[0];
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SixVector[1]= rStVec.SixVector[1];
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SixVector[2]= rStVec.SixVector[2];
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SixVector[3]= rStVec.SixVector[3];
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SixVector[4]= rStVec.SixVector[4];
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SixVector[5]= rStVec.SixVector[5];
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// fpChargeState= new G4ChargeState( *rStVec.fpChargeState );
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// Can share charge state only when using handles etc
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// fpChargeState = rStVec.fpChargeState;
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}
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inline
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G4FieldTrack::~G4FieldTrack()
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{
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// delete fpChargeState;
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}
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inline G4FieldTrack&
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G4FieldTrack::SetCurvePnt(const G4ThreeVector& pPosition,
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const G4ThreeVector& pMomentum,
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G4double s_curve )
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{
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SixVector[0] = pPosition.x();
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SixVector[1] = pPosition.y();
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SixVector[2] = pPosition.z();
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SixVector[3] = pMomentum.x();
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SixVector[4] = pMomentum.y();
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SixVector[5] = pMomentum.z();
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fMomentumDir = pMomentum.unit();
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fDistanceAlongCurve= s_curve;
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return *this;
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}
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inline
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G4ThreeVector G4FieldTrack::GetPosition() const
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{
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G4ThreeVector myPosition( SixVector[0], SixVector[1], SixVector[2] );
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return myPosition;
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}
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inline
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void G4FieldTrack::SetPosition( G4ThreeVector pPosition)
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{
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SixVector[0] = pPosition.x();
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SixVector[1] = pPosition.y();
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SixVector[2] = pPosition.z();
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}
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inline
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const G4ThreeVector& G4FieldTrack::GetMomentumDir() const
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{
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// G4ThreeVector myMomentum( SixVector[3], SixVector[4], SixVector[5] );
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// return myVelocity;
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return fMomentumDir;
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}
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inline
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G4ThreeVector G4FieldTrack::GetMomentumDirection() const
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{
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return fMomentumDir;
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}
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inline
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G4double G4FieldTrack::GetCurveLength() const
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{
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return fDistanceAlongCurve;
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}
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inline
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void G4FieldTrack::SetCurveLength(G4double nCurve_s)
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{
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fDistanceAlongCurve= nCurve_s;
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}
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inline
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G4double G4FieldTrack::GetKineticEnergy() const
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{
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return fKineticEnergy;
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}
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inline
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void G4FieldTrack::SetKineticEnergy(G4double newKinEnergy)
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{
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fKineticEnergy=newKinEnergy;
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}
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inline
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G4ThreeVector G4FieldTrack::GetSpin() const
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{
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return fSpin;
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}
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inline
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void G4FieldTrack::SetSpin(G4ThreeVector nSpin)
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{
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fSpin=nSpin;
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}
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inline
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G4double G4FieldTrack::GetLabTimeOfFlight() const
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{
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return fLabTimeOfFlight;
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}
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inline
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void G4FieldTrack::SetLabTimeOfFlight(G4double nTOF)
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{
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fLabTimeOfFlight=nTOF;
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}
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inline
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G4double G4FieldTrack::GetProperTimeOfFlight() const
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{
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return fProperTimeOfFlight;
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}
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inline
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void G4FieldTrack::SetProperTimeOfFlight(G4double nTOF)
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{
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fProperTimeOfFlight=nTOF;
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}
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inline
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void G4FieldTrack::SetMomentumDir(G4ThreeVector newMomDir)
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{
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fMomentumDir= newMomDir;
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}
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inline
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G4ThreeVector G4FieldTrack::GetMomentum() const
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{
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return G4ThreeVector( SixVector[3], SixVector[4], SixVector[5] );
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}
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inline
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void G4FieldTrack::SetMomentum(G4ThreeVector pMomentum)
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{
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SixVector[3] = pMomentum.x();
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SixVector[4] = pMomentum.y();
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SixVector[5] = pMomentum.z();
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fMomentumDir = pMomentum.unit();
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}
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inline
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G4double G4FieldTrack::GetCharge() const
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{
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return fChargeState.GetCharge();
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}
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// Dump values to array
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//
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// note that momentum direction is not saved
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inline
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void G4FieldTrack::DumpToArray(G4double valArr[ncompSVEC] ) const
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{
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valArr[0]=SixVector[0];
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valArr[1]=SixVector[1];
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valArr[2]=SixVector[2];
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valArr[3]=SixVector[3];
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valArr[4]=SixVector[4];
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valArr[5]=SixVector[5];
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G4ThreeVector Momentum(valArr[3],valArr[4],valArr[5]);
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// G4double mass_in_Kg;
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// mass_in_Kg = fEnergy / velocity_mag_sq * (1-velocity_mag_sq/c_squared);
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// valArr[6]= mass_in_Kg;
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// The following components may or may not be integrated.
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valArr[6]= fKineticEnergy;
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// valArr[6]=fEnergy; // When it is integrated over, do this ...
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valArr[7]=fLabTimeOfFlight;
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valArr[8]=fProperTimeOfFlight;
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valArr[9]=fSpin.x();
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valArr[10]=fSpin.y();
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valArr[11]=fSpin.z();
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// valArr[13]=fMomentumDir.x();
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// valArr[14]=fMomentumDir.y();
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// valArr[15]=fMomentumDir.z();
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// valArr[]=fDistanceAlongCurve;
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}
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// Load values from array
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//
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// note that momentum direction must-be/is normalised
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inline
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void G4FieldTrack::LoadFromArray(const G4double valArrIn[ncompSVEC], G4int noVarsIntegrated)
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{
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G4int i;
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// Fill the variables not integrated with zero -- so it's clear !!
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static G4double valArr[ncompSVEC];
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for( i=0; i<noVarsIntegrated; i++){
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valArr[i]= valArrIn[i];
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}
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for( i=noVarsIntegrated; i<ncompSVEC; i++) {
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valArr[i]= 0.0;
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}
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SixVector[0]=valArr[0];
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SixVector[1]=valArr[1];
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SixVector[2]=valArr[2];
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SixVector[3]=valArr[3];
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SixVector[4]=valArr[4];
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SixVector[5]=valArr[5];
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G4ThreeVector Momentum(valArr[3],valArr[4],valArr[5]);
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G4double momentum_square= Momentum.mag2();
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fMomentumDir= Momentum.unit();
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fKineticEnergy = momentum_square /
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(std::sqrt(momentum_square+fRestMass_c2*fRestMass_c2)
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+ fRestMass_c2 );
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// The above equation is stable for small and large momenta
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// The following components may or may not be
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// integrated over -- integration is optional
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// fKineticEnergy= valArr[6];
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fLabTimeOfFlight=valArr[7];
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fProperTimeOfFlight=valArr[8];
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fSpin=G4ThreeVector(valArr[9],valArr[10],valArr[11]);
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// fMomentumDir=G4ThreeVector(valArr[13],valArr[14],valArr[15]);
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// fDistanceAlongCurve= valArr[];
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}
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inline
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G4FieldTrack & G4FieldTrack::operator = ( const G4FieldTrack& rStVec )
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{
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if (&rStVec == this) return *this;
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SixVector[0]= rStVec.SixVector[0];
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SixVector[1]= rStVec.SixVector[1];
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SixVector[2]= rStVec.SixVector[2];
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SixVector[3]= rStVec.SixVector[3];
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SixVector[4]= rStVec.SixVector[4];
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SixVector[5]= rStVec.SixVector[5];
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SetCurveLength( rStVec.GetCurveLength() );
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fKineticEnergy= rStVec.fKineticEnergy;
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SetLabTimeOfFlight( rStVec.GetLabTimeOfFlight() );
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SetProperTimeOfFlight( rStVec.GetProperTimeOfFlight() );
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SetSpin( rStVec.GetSpin() );
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// SetMomentumModulus( rStVec.GetMomentumModulus());
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SetMomentumDir( rStVec.fMomentumDir );
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fChargeState= rStVec.fChargeState;
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// (*fpChargeState)= *(rStVec.fpChargeState);
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// fpChargeState= rStVec.fpChargeState; // Handles!!
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return *this;
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}
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void
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G4FieldTrack::UpdateFourMomentum( G4double kineticEnergy,
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const G4ThreeVector& momentumDirection )
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{
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G4double momentum_mag = std::sqrt(kineticEnergy*kineticEnergy
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+2.0*fRestMass_c2*kineticEnergy);
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G4ThreeVector momentumVector= momentum_mag * momentumDirection;
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SetMomentum( momentumVector ); // Also sets direction (from unit)
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fMomentumDir= momentumDirection;
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fKineticEnergy= kineticEnergy;
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}
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void G4FieldTrack::UpdateState( const G4ThreeVector& position,
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G4double laboratoryTimeOfFlight,
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const G4ThreeVector& momentumDirection,
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G4double kineticEnergy
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)
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{
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// SetCurvePnt( position, momentumVector, s_curve=0.0);
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SetPosition( position);
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fLabTimeOfFlight= laboratoryTimeOfFlight;
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fDistanceAlongCurve= 0.0;
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UpdateFourMomentum( kineticEnergy, momentumDirection);
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}
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