00001
00002 #include "PhysicsTools/CandUtils/interface/Thrust.h"
00003 #include <cmath>
00004 using namespace reco;
00005 const double pi = M_PI, pi2 = 2 * pi, pi_2 = pi / 2, pi_4 = pi / 4;
00006
00007 void Thrust::init(const std::vector<const Candidate*>& cands) {
00008 int i = 0;
00009 for(std::vector<const Candidate*>::const_iterator t = cands.begin();
00010 t != cands.end(); ++t, ++i)
00011 pSum_ += (p_[i] = (*t)->momentum()).r();
00012 axis_ = axis(finalAxis(initialAxis()));
00013 if (axis_.z() < 0) axis_ *= -1;
00014 thrust_ = thrust(axis_);
00015 }
00016
00017 Thrust::ThetaPhi Thrust::initialAxis() const {
00018 static const int nSegsTheta = 10, nSegsPhi = 10, nSegs = nSegsTheta * nSegsPhi;
00019 int i, j;
00020 double thr[nSegs], max = 0;
00021 int indI = 0, indJ = 0, index = -1;
00022 for (i = 0; i < nSegsTheta ; ++i) {
00023 double z = cos(pi * i / (nSegsTheta - 1));
00024 double r = sqrt(1 - z*z);
00025 for (j = 0; j < nSegsPhi ; ++j) {
00026 double phi = pi2 * j / nSegsPhi;
00027 thr[i * nSegsPhi + j] = thrust(Vector(r*cos(phi), r*sin(phi), z));
00028 if (thr[i*nSegsPhi + j] > max) {
00029 index = i*nSegsPhi + j;
00030 indI = i; indJ = j;
00031 max = thr[index];
00032 }
00033 }
00034 }
00035
00036
00037
00038
00039
00040 double a, b, c = max;
00041 int ind1 = indJ + 1;
00042 if (ind1 >= nSegsPhi) ind1 -= nSegsPhi;
00043 int ind2 = indJ - 1;
00044 if (ind2 < 0) ind2 += nSegsPhi;
00045 a = (thr[ind1] + thr[ind2] - 2*c) / 2;
00046 b = thr[ind1] - a - c;
00047 double maxPhiInd = 0;
00048 if (a != 0) maxPhiInd = -b/(2*a);
00049 double maxThetaInd;
00050 if (indI == 0 || indI == (nSegsTheta - 1))
00051 maxThetaInd = indI;
00052 else {
00053 ind1 = indI + 1;
00054 ind2 = indI - 1;
00055 a = (thr[ind1] + thr[ind2] - 2*c) / 2;
00056 b = thr[ind1] - a - c;
00057 maxThetaInd = 0;
00058 if (a != 0) maxThetaInd = - b/(2*a);
00059 }
00060 return ThetaPhi(pi*(maxThetaInd + indI) / (nSegsTheta - 1),
00061 pi2*(maxPhiInd + indJ) / nSegsPhi);
00062 }
00063
00064 Thrust::ThetaPhi Thrust::finalAxis(ThetaPhi best) const {
00065 static const double epsilon = 0.0001;
00066 double maxChange1=0.0, maxChange2=0.0, a=0.0, b=0.0, c=0.0, thr=0.0;
00067 int mandCt = 3, maxCt = 1000;
00068 bool done;
00069 do {
00070 parabola(a, b, c,
00071 axis(best),
00072 axis(best.theta + epsilon, best.phi),
00073 axis(best.theta - epsilon, best.phi));
00074 maxChange1 = 10*(b < 0 ? -1 : 1);
00075 if (a != 0) maxChange1 = - b/(2*a);
00076 while (fabs(maxChange1 * epsilon) > pi_4) maxChange1 /= 2;
00077 if (maxChange1 == 0 && (best.theta == 0 || best.theta == pi)) {
00078 best.phi += pi_2;
00079 if (best.phi > pi2) best.phi -= pi2;
00080 parabola(a, b, c,
00081 axis(best),
00082 axis(best.theta + epsilon, best.phi),
00083 axis(best.theta - epsilon, best.phi));
00084 maxChange1 = 10 * (b < 0 ? -1 : 1);
00085 if (a != 0) maxChange1 = - b / (2 * a);
00086 }
00087 do {
00088
00089 thr = thrust(axis(best.theta + maxChange1 * epsilon, best.phi)) + epsilon;
00090 if (thr < c) maxChange1 /= 2;
00091 } while (thr < c);
00092
00093 best.theta += maxChange1 * epsilon;
00094 if (best.theta > pi) {
00095 best.theta = pi - (best.theta - pi);
00096 best.phi += pi;
00097 if (best.phi > pi2) best.phi -= pi2;
00098 }
00099 if (best.theta < 0) {
00100 best.theta *= -1;
00101 best.phi += pi;
00102 if (best.phi > pi2) best.phi -= pi2;
00103 }
00104 parabola(a, b, c,
00105 axis(best),
00106 axis(best.theta, best.phi + epsilon),
00107 axis(best.theta, best.phi - epsilon));
00108 maxChange2 = 10 * (b < 0 ? -1 : 1);
00109 if (a != 0) maxChange2 = - b / (2 * a);
00110 while (fabs(maxChange2 * epsilon) > pi_4) { maxChange2 /= 2; }
00111 do {
00112
00113 thr = thrust(axis(best.theta, best.phi + maxChange2 * epsilon)) + epsilon;
00114 if (thr < c) maxChange2 /= 2;
00115 } while (thr < c);
00116 best.phi += maxChange2 * epsilon;
00117 if (best.phi > pi2) best.phi -= pi2;
00118 if (best.phi < 0) best.phi += pi2;
00119 if (mandCt > 0) mandCt --;
00120 maxCt --;
00121 done = (fabs(maxChange1) > 1 || fabs(maxChange2) > 1 || mandCt) && (maxCt > 0);
00122 } while (done);
00123
00124 return best;
00125 }
00126
00127 void Thrust::parabola(double & a, double & b, double & c,
00128 const Vector & a1, const Vector & a2, const Vector & a3) const {
00129 double t1 = thrust(a1), t2 = thrust(a2), t3 = thrust(a3);
00130 a = (t2 - 2 * c + t3) / 2;
00131 b = t2 - a - c;
00132 c = t1;
00133 }
00134
00135 Thrust::Vector Thrust::axis(double theta, double phi) const {
00136 double theSin = sin(theta);
00137 return Vector(theSin * cos(phi), theSin * sin(phi), cos(theta));
00138 }
00139
00140 double Thrust::thrust(const Vector & axis) const {
00141 double result = 0;
00142 double sum = 0;
00143 for (unsigned int i = 0; i < n_; ++i)
00144 sum += fabs(axis.Dot(p_[i]));
00145 if (pSum_ > 0) result = sum / pSum_;
00146 return result;
00147 }