Go to the documentation of this file.00001
00002 #include "Alignment/TwoBodyDecay/interface/TwoBodyDecayModel.h"
00003
00004
00005 TwoBodyDecayModel::TwoBodyDecayModel( double mPrimary, double mSecondary ) :
00006 thePrimaryMass( mPrimary ), theSecondaryMass( mSecondary ) {}
00007
00008
00009 TwoBodyDecayModel::~TwoBodyDecayModel() {}
00010
00011
00012 AlgebraicMatrix TwoBodyDecayModel::rotationMatrix( double px, double py, double pz )
00013 {
00014
00015 double pT2 = px*px + py*py;
00016 double p2 = pT2 + pz*pz;
00017 double pT = sqrt( pT2 );
00018 double p = sqrt( p2 );
00019
00020 AlgebraicMatrix rotMat( 3, 3 );
00021
00022
00023 rotMat[0][0] = px*pz/pT/p;
00024 rotMat[0][1] = -py/pT;
00025 rotMat[0][2] = px/p;
00026
00027 rotMat[1][0] = py*pz/pT/p;
00028 rotMat[1][1] = px/pT;
00029 rotMat[1][2] = py/p;
00030
00031 rotMat[2][0] = -pT/p;
00032 rotMat[2][1] = 0.;
00033 rotMat[2][2] = pz/p;
00034
00035 return rotMat;
00036 }
00037
00038
00039 AlgebraicMatrix TwoBodyDecayModel::curvilinearToCartesianJacobian( double rho, double theta, double phi, double zMagField )
00040 {
00041 double q = ( ( rho < 0 ) ? -1. : 1. );
00042 double conv = q*zMagField;
00043
00044 double stheta = sin( theta );
00045 double ctheta = cos( theta );
00046 double sphi = sin( phi );
00047 double cphi = cos( phi );
00048
00049 AlgebraicMatrix curv2cart( 3, 3 );
00050
00051 curv2cart[0][0] = -rho*cphi;
00052 curv2cart[0][1] = -rho*sphi;
00053 curv2cart[0][2] = 0.;
00054
00055 curv2cart[1][0] = cphi*stheta*ctheta;
00056 curv2cart[1][1] = sphi*stheta*ctheta;
00057 curv2cart[1][2] = -stheta*stheta;
00058
00059 curv2cart[2][0] = -sphi;
00060 curv2cart[2][1] = cphi;
00061 curv2cart[2][2] = 0.;
00062
00063 curv2cart *= rho/conv;
00064
00065 return curv2cart;
00066 }
00067
00068
00069 AlgebraicMatrix TwoBodyDecayModel::curvilinearToCartesianJacobian( AlgebraicVector curv, double zMagField )
00070 {
00071 return this->curvilinearToCartesianJacobian( curv[0], curv[1], curv[2], zMagField );
00072 }
00073
00074
00075 AlgebraicVector TwoBodyDecayModel::convertCurvilinearToCartesian( AlgebraicVector curv, double zMagField )
00076 {
00077 double rt = fabs( zMagField/curv[0] );
00078
00079 AlgebraicVector cart( 3 );
00080 cart[0] = rt*cos( curv[2] );
00081 cart[1] = rt*sin( curv[2] );
00082 cart[2] = rt/tan( curv[1] );
00083
00084 return cart;
00085 }
00086
00087
00088 const std::pair< AlgebraicVector, AlgebraicVector > TwoBodyDecayModel::cartesianSecondaryMomenta( const AlgebraicVector & param )
00089 {
00090 double px = param[TwoBodyDecayParameters::px];
00091 double py = param[TwoBodyDecayParameters::py];
00092 double pz = param[TwoBodyDecayParameters::pz];
00093 double theta = param[TwoBodyDecayParameters::theta];
00094 double phi = param[TwoBodyDecayParameters::phi];
00095
00096
00097 double pT2 = px*px + py*py;
00098 double p2 = pT2 + pz*pz;
00099 double p = sqrt( p2 );
00100
00101 double sphi = sin( phi );
00102 double cphi = cos( phi );
00103 double stheta = sin( theta );
00104 double ctheta = cos( theta );
00105
00106
00107 double c1 = 0.5*thePrimaryMass/theSecondaryMass;
00108 double c2 = sqrt( c1*c1 - 1. );
00109 double c3 = 0.5*c2*ctheta/c1;
00110 double c4 = sqrt( p2 + thePrimaryMass*thePrimaryMass );
00111
00112
00113 AlgebraicMatrix pplus( 3, 1 );
00114 pplus[0][0] = theSecondaryMass*c2*stheta*cphi;
00115 pplus[1][0] = theSecondaryMass*c2*stheta*sphi;
00116 pplus[2][0] = 0.5*p + c3*c4;
00117
00118
00119 AlgebraicMatrix pminus( 3, 1 );
00120 pminus[0][0] = -pplus[0][0];
00121 pminus[1][0] = -pplus[1][0];
00122 pminus[2][0] = 0.5*p - c3*c4;
00123
00124 AlgebraicMatrix rotMat = rotationMatrix( px, py, pz );
00125
00126 return std::make_pair( rotMat*pplus, rotMat*pminus );
00127 }
00128
00129
00130 const std::pair< AlgebraicVector, AlgebraicVector > TwoBodyDecayModel::cartesianSecondaryMomenta( const TwoBodyDecay & tbd )
00131 {
00132 return cartesianSecondaryMomenta( tbd.parameters() );
00133 }
00134
00135 const std::pair< AlgebraicVector, AlgebraicVector > TwoBodyDecayModel::cartesianSecondaryMomenta( const TwoBodyDecayParameters & tbdparam )
00136 {
00137 return cartesianSecondaryMomenta( tbdparam.parameters() );
00138 }