Alignment/TwoBodyDecay/src/TwoBodyDecayModel.cc - master - githubmirror/cmssw

Alignment/TwoBodyDecay/src/TwoBodyDecayModel.cc
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08 май 2019, 15:16
08 май 2019, 15:167614b05

#include "Alignment/TwoBodyDecay/interface/TwoBodyDecayModel.h"

TwoBodyDecayModel::TwoBodyDecayModel(double mPrimary, double mSecondary)
    : thePrimaryMass(mPrimary), theSecondaryMass(mSecondary) {}

TwoBodyDecayModel::~TwoBodyDecayModel() {}

AlgebraicMatrix TwoBodyDecayModel::rotationMatrix(double px, double py, double pz) {
  // compute transverse and absolute momentum
  double pT2 = px * px + py * py;
  double p2 = pT2 + pz * pz;
  double pT = sqrt(pT2);
  double p = sqrt(p2);

  AlgebraicMatrix rotMat(3, 3);

  // compute rotation matrix
  rotMat[0][0] = px * pz / pT / p;
  rotMat[0][1] = -py / pT;
  rotMat[0][2] = px / p;

  rotMat[1][0] = py * pz / pT / p;
  rotMat[1][1] = px / pT;
  rotMat[1][2] = py / p;

  rotMat[2][0] = -pT / p;
  rotMat[2][1] = 0.;
  rotMat[2][2] = pz / p;

  return rotMat;
}

AlgebraicMatrix TwoBodyDecayModel::curvilinearToCartesianJacobian(double rho,
                                                                  double theta,
                                                                  double phi,
                                                                  double zMagField) {
  double q = ((rho < 0) ? -1. : 1.);
  double conv = q * zMagField;

  double stheta = sin(theta);
  double ctheta = cos(theta);
  double sphi = sin(phi);
  double cphi = cos(phi);

  AlgebraicMatrix curv2cart(3, 3);

  curv2cart[0][0] = -rho * cphi;
  curv2cart[0][1] = -rho * sphi;
  curv2cart[0][2] = 0.;

  curv2cart[1][0] = cphi * stheta * ctheta;
  curv2cart[1][1] = sphi * stheta * ctheta;
  curv2cart[1][2] = -stheta * stheta;

  curv2cart[2][0] = -sphi;
  curv2cart[2][1] = cphi;
  curv2cart[2][2] = 0.;

  curv2cart *= rho / conv;

  return curv2cart;
}

AlgebraicMatrix TwoBodyDecayModel::curvilinearToCartesianJacobian(const AlgebraicVector &curv, double zMagField) {
  return this->curvilinearToCartesianJacobian(curv[0], curv[1], curv[2], zMagField);
}

AlgebraicVector TwoBodyDecayModel::convertCurvilinearToCartesian(const AlgebraicVector &curv, double zMagField) {
  double rt = fabs(zMagField / curv[0]);

  AlgebraicVector cart(3);
  cart[0] = rt * cos(curv[2]);
  cart[1] = rt * sin(curv[2]);
  cart[2] = rt / tan(curv[1]);

  return cart;
}

const std::pair<AlgebraicVector, AlgebraicVector> TwoBodyDecayModel::cartesianSecondaryMomenta(
    const AlgebraicVector &param) {
  double px = param[TwoBodyDecayParameters::px];
  double py = param[TwoBodyDecayParameters::py];
  double pz = param[TwoBodyDecayParameters::pz];
  double theta = param[TwoBodyDecayParameters::theta];
  double phi = param[TwoBodyDecayParameters::phi];

  // compute transverse and absolute momentum
  double pT2 = px * px + py * py;
  double p2 = pT2 + pz * pz;
  double p = sqrt(p2);

  double sphi = sin(phi);
  double cphi = cos(phi);
  double stheta = sin(theta);
  double ctheta = cos(theta);

  // some constants from kinematics
  double c1 = 0.5 * thePrimaryMass / theSecondaryMass;
  double c2 = sqrt(c1 * c1 - 1.);
  double c3 = 0.5 * c2 * ctheta / c1;
  double c4 = sqrt(p2 + thePrimaryMass * thePrimaryMass);

  // momentum of decay particle 1 in the primary's boosted frame
  AlgebraicMatrix pplus(3, 1);
  pplus[0][0] = theSecondaryMass * c2 * stheta * cphi;
  pplus[1][0] = theSecondaryMass * c2 * stheta * sphi;
  pplus[2][0] = 0.5 * p + c3 * c4;

  // momentum of decay particle 2 in the primary's boosted frame
  AlgebraicMatrix pminus(3, 1);
  pminus[0][0] = -pplus[0][0];
  pminus[1][0] = -pplus[1][0];
  pminus[2][0] = 0.5 * p - c3 * c4;

  AlgebraicMatrix rotMat = rotationMatrix(px, py, pz);

  return std::make_pair(rotMat * pplus, rotMat * pminus);
}

const std::pair<AlgebraicVector, AlgebraicVector> TwoBodyDecayModel::cartesianSecondaryMomenta(const TwoBodyDecay &tbd) {
  return cartesianSecondaryMomenta(tbd.parameters());
}

const std::pair<AlgebraicVector, AlgebraicVector> TwoBodyDecayModel::cartesianSecondaryMomenta(
    const TwoBodyDecayParameters &tbdparam) {
  return cartesianSecondaryMomenta(tbdparam.parameters());
}