G4EqMagElectricField.cc

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//
// G4EqMagElectricField implementation
//
// This is the standard right-hand side for equation of motion.
//
// The only case another is required is when using a moving reference
// frame ... or extending the class to include additional forces,
// e.g., an electric field
//
// Author: Vladimir Grichine (CERN), 10.11.1998
// -------------------------------------------------------------------
 
#include "G4EqMagElectricField.hh"
#include "globals.hh"
#include "G4PhysicalConstants.hh"
#include "G4SystemOfUnits.hh"
 
G4EqMagElectricField::G4EqMagElectricField(G4ElectroMagneticField* emField )
  : G4EquationOfMotion( emField )
{
}
 
void  
G4EqMagElectricField::SetChargeMomentumMass(G4ChargeState particleCharge,
                                            G4double,
                                            G4double particleMass)
{
   G4double pcharge = particleCharge.GetCharge();
   fElectroMagCof =  eplus*pcharge*c_light ;
   fMassCof = particleMass*particleMass ; 
}
 
void
G4EqMagElectricField::EvaluateRhsGivenB(const G4double y[],
                                        const G4double Field[],
                                              G4double dydx[] ) const
{
   // Components of y:
   //    0-2 dr/ds, 
   //    3-5 dp/ds - momentum derivatives 
 
   G4double pSquared = y[3]*y[3] + y[4]*y[4] + y[5]*y[5] ;
 
   G4double Energy   = std::sqrt( pSquared + fMassCof );
   G4double cof2     = Energy/c_light ;
 
   G4double pModuleInverse  = 1.0/std::sqrt(pSquared) ;
 
   G4double inverse_velocity = Energy * pModuleInverse / c_light;
 
   G4double cof1     = fElectroMagCof*pModuleInverse ;
 
   dydx[0] = y[3]*pModuleInverse ;                         
   dydx[1] = y[4]*pModuleInverse ;                         
   dydx[2] = y[5]*pModuleInverse ;                        
 
   dydx[3] = cof1*(cof2*Field[3] + (y[4]*Field[2] - y[5]*Field[1])) ;
   
   dydx[4] = cof1*(cof2*Field[4] + (y[5]*Field[0] - y[3]*Field[2])) ; 
 
   dydx[5] = cof1*(cof2*Field[5] + (y[3]*Field[1] - y[4]*Field[0])) ;  
 
   dydx[6] = 0.;//not used
 
   // Lab Time of flight
   //
   dydx[7] = inverse_velocity;
 
   return;
}