Baryon Pro duction in Z Decay

Christopher G Tully

A DISSERTATION

PRESENTED TO THE FACULTY

OF PRINCETON UNIVERSITY

IN CANDIDACY FOR THE DEGREE

OF DOCTOR OF PHILOSOPHY

RECOMMENDED FOR ACCEPTANCE

BY THE DEPARTMENT OF PHYSICS

January

ABSTRACT

How quarks b ecome conned into ordinary matter is a dicult theoretical

question The p ointatwhich this o ccurs cannot b e measured by exp eriment

but other prop erties related to connement can Baryon pro duction is a

situation where one typ e of connement is chosen over another

In this thesis pro duction rate measurements have b een p erformed for

and baryons pro duced in hadronic decays of the Z The rates are

low compared to meson pro duction but the particular prop erties of and

decay allow these particles to be identied amongst the many mesons

accompanying them The average number of and per hadronic Z

decay was found to be

D E

N

stat syst

and

D E

N

stat syst

resp ectively

These measurements take advantage of the unique photon detection capa

bility of the L Exp eriment The rates are in agreement with those measured

by other LEP detectors iii

CONTENTS

Abstract iii

Acknowledgements v

Intro duction

Particle Creation and Detection

Searching for Particle Decays

Going Back in Time

The History Behind SubNuclear Particles Quarks

Discovery of the Pion

The Quark Constituent Mo del

Deep Inelastic Scattering

Quantum Chromo dynamics

eak Interaction Quarks and the Electrow

Radiation from Quarks

The Standard Mo del and Its Help ers

Fundamental Interactions

The GSW Standard Mo del of Electroweak Interactions

The Prop erties of Quarks from Z Decay

Quantum Chromo dynamics

Hadronization Phenomenology

Hyp eron Decay

Particle Acceleration and Collision

The Large LEP Collider

LEP Injector Chain

LEP Main Ring

The L Exp eriment

SubDetectors of the L Exp eriment vii

viii Contents

Trigger and DataAcquisition System

Tracking and Calorimetry

Tracking

Ideal Tra jectories

The Geometry of the Tracking Detectors

Tracking Measurements

Track Fitting and Error Propagation

Calculation of the Primary Vertex

Calorimetry

Electromagnetic Showers

The Geometry of the Electromagnetic Calorimeter

The Electromagnetic Shower Shap e

Statistically Determined Errors on Energy and Angu

lar Measurements

Gain and Oset Calibration of the Electronics

Energy Resolution and Linearity Measurements

Baryon Pro duction Measurements

Secondary Vertices

Kinematic Constraints

Measurement of the Baryon

Measurement of the Baryon

Pro duction Rates

Comparison with Other LEP Measurements

Polarization

Summary and Outlo ok

A BGO Resolution Functions

B BGO Noise DeCorrelation Algorithm

C Constrained Fit Details

C Denitions

C Fit

C Calculation

C Convergence

C Directed Steps

INTRODUCTION

Reaching higher energies probing smaller distances revisiting earlier times

in the evolution of the universe these are all ways of discussing the direction

which particle physicists pursue to uncover the elementary building blo cks

and interactions of matter When relativity and quantum mechanics were

merged in the late s to form a more complete description of particle

dynamics it b ecame understo o d that the number and typ es of particles in a

system did not have to remain unchanged in time The freedom to annihilate

and create new particles was linked to the relativistic quantum description

of elementary forces

In this thesis a study is made of the rate of pro duction of dierenttyp es

of baryons heavier versions of ordinary nuclear matter Baryons are par

ticularly interesting to study because they are conserved This means that

for every baryon pro duced an antibaryon will also be pro duced Baryons

are heavier than other particles hence the origin of their name Their rate

of pro duction is related to their mass their conservation law and prop er

ties of the system from which they arise In particular the pro duction

rate dep endence on baryon mass is a measure of the temp erature at which

quarks b ecome conned within ordinary matter Longlived but unstable

baryons known as hyp erons have a signature whichallows them to b e iden

tied amongst other particle decays That is whythe and baryons in

particular are measured in this thesis and not others

The creation of heavy matter is achieved by the op eration of largescale

particle colliders Charged particles intro duced into the nearly p erfect vac

uum of a b eam pip e can be accelerated and steered with electromagnetic

elds The Large ElectronPositronLEP Collider lo cated near Geneva

Switzerland is to day the highest energy electronp ositron collider in the

world LEP was designed to have four principal collision poin ts equally

spaced along its km circumference The L Exp eriment led bySamuel C

C Ting occupies one of these interaction regions and is the source of data

used in this thesis

Intro duction

Particle Creation and Detection

At the centralmost part of the L Exp eriment highenergy b eams of elec

trons and p ositrons are broughtinto collision The particles created in these

collisions are detected by the surrounding apparatus The apparatus consists

of two main comp onents tracking and calorimetry

The goal of the inner part of the detector the tracking is to measure

the tra jectories of the particles coming from the center of the detector while

aecting the ideal unmeasured tra jectories as little as p ossible High

energy particles can travel through thin light materials and gaseous volumes

without losing a large fraction of their initial momentum However the small

amountthey do lose can be used to track their tra jectories

The function of the outer part of the detector the calorimetry is to stop

and measure the energies of all the particles which have tra velled through

the tracking region This task is achieved by using tons of heavy materials

intersp ersed or instrumented with devices that gauge the total number of

material interactions which o ccur during the stopping pro cess The number

and distribution of material interactions can then b e related to initial energies

and typ es of particles which hit the calorimetry

Searching for Particle Decays

Measuring the prop erties of shortlived particles requires a bit of detective

work Only a handful of particles pro duced in beam collisions live long

evacuated b eam pip e Therefore the bulk of enough to make it out of the

the particles that enter the tracking and calorimetry are longlived particles

which come from particle decays

But in fact how do es one know that the shortlived particles even existed

if they cannot be measured directly When a particle decays the particles

coming from this decay will satisfy a set of kinematic relationships Although

the kinematics of the longlived particles are measured with the tracking and

calorimetry there are measurement errors This intro duces the concept of

satisfying kinematic relationships within errors

When searching for the evidence of a particular particle decay among

the decay pro ducts of several dierent particles there is no smoking gun

The analysis requires that distributions of candidate particle decays sho w

statistical evidence for the presence of a particular particle typ e The most

Going Back in Time

telling distribution to identify a particle is the mass distribution In addition

to a set of discrete symmetry and angular momentum quantum numb ers

particles are distinguished by the way they interact and by their mass

Going Back in Time

As was indicated heavy particles are formed in the vacuum of the b eam pip e

when highenergy and p ositrons are collided This is not a nor

mal everyday exp erience The evolution of interaction energies into particle

states froze out as the universe co oled down Typical interaction energies in

everyday life are well b elow that needed to generate nuclear matter

The central story is ab out how particle interactions will b ehavewhenthe

interaction energies b ecome closer and closer to those b elieved to b e present

in the early universe The LEP Collider energies were designed for studying

a particular p erio d of history called the Electroweak Era During this p erio d

the interaction resp onsible for radioactivity in heavy atomic nuclei takes on

a new form This form is called the Z particle and it is created when an

electron and p ositron collide with an energy which is equal to or within close

vicinityofthephysical mass of the Z particle multiplied byc from Einsteins

Emc

When Z particles decay into subnuclear particles quarks the ensuing

interactions generate a large number and variety of strongly interacting par

ticles known as The formation of hadrons with dierent masses

and quantum numb ers dep ends on the prop erties of the quarks coming from

Z decay and the elementary interactions This pro cess cannot yet be calcu

lated but app ears to o ccur at a characteristic temp erature the hadronization

temp erature Understanding how this feature is related to the elementary

strong interaction and quark connement could have an impact on prop

erties of the early universe and hence on yettob eseen asp ects of to days

universe The highenergy frontier of reaching the unication of all the forces

of nature and how they entangle in the dawn of all matter formation seems

to day as far away as the most distant galaxies but with every observation

and study this gap diminishes

Intro duction

THE HISTORY BEHIND SUBNUCLEAR PARTICLES

QUARKS

Many original ideas and challenging measurements brought ab out the quark

mo del and the theory of the strong interaction The following historical p er

sp ectivewas drawn mainly from a conference which coincided with the start

of this thesis research Hop efully some of the terms and ideas in Chapter

will b ecome more clear when viewed with their historical context in mind

Discovery of the Pion

The distinction b etween dierentchemical elements has its origin in the nu

clei of atoms However nuclei play a very passive role in chemistry Its

not the nuclei themselves which determine the chemical b eha vior of the dif

ferent elements but rather the system of electrons which forms from the

electromagnetic interaction with the nucleus The interaction which forms

the nuclei themselves has amuch shorter distance over which it acts

H Yukawa in explained the range of the nuclear force by attributing

its origin to the exchange of a massive particle called the pion Quantum

mechanics views the binding of atomic electrons to the charge of a nucleus as

due to the exchange of photons Photons are massless and the range of the

electromagnetic interaction is innite Yukawa saw the limit in the range of

the interaction binding nucleons within nuclei as being due to the exchange

of a massive particle The mass of the exchanged particle limits the range of

the interaction The measured range of the nuclear force allowed Yukawato

predict the mass of the pion The pion was later discovered at its predicted

mass in by CF Powell and his coworkers

Conference on the History of Original Ideas and Basic Discoveries in Particle Physics

held at the Ettore Ma jorana Centre for Scientic Culture in Erice Sicily July August

The History Behind SubNuclear Particles Quarks

The Quark Constituent Mo del

Strangely enough the strong interaction didnt stop with protons neutrons

and pions Not only would the scattering of pions o of protons reveal new

higher mass versions of the proton but at suciently high energies pairs of

particles would be formed that have distinctly dierent behavior from that

of pions and protons A new charge was needed to describ e the behavior

of these strange particles This charge was named hyp ercharge and was

intro duced in by M GellMann and K Nishijima as a quantit y which

was conserved by the strong interaction

By M GellMann and Y Ne eman develop ed a mathematical de

scription whichwas able to explain the proliferating zo o of particles b eing

found by exp erimentalists The algebra of SU classied strongly interact

ing particles by their spin and parity This description created geometrically

constructed tables of particle typ es Many of the predicted particle typ es

had already b een measured but some had not the most illustrious of which

was the sss

Spin Octet Decuplet Spin

nudd puud ddd udd uud uuu

uds

  

dds uus dds uds uus

uds

 

dss uss dss uss

sss

Flavor Symmetry SU Baryon Families

It was not until that M GellMann and indep endently G Zweig pro

p osed that SU tables could be explained by describing all strongly inter

acting particles hadrons as b eing made from three avors of quarks u d

Manybaryons are named with capital Greek letters

Deep Inelastic Scattering

and s The quarks were assigned to have spin and fractional electric

charge and resp ectively This scheme identied protons

and its heavier versions generally called baryons as being comp osed of

three quarks

Deep Inelastic Scattering

As fantastic as the notion of quarks sounded the idea that they would have

fractional charge was unsettling No exp erimental evidence existed to sup

p ort this conjecture Also missing was an explanation of howthe uuu

for instance could haveawavefunction with complete symmetry in spin and

avor but still haveanoverall antisymmetric wavefunction This is the well

kno wn Pauli exclusion principle for particles with fractional total angular

momentum Some feature intrinsic to the strong interaction seemed to be

missing

Exp eriments at the Stanford Linear AcceleratorSLAC starting in

charted the way with highenergy electron scattering exp eriments o of pro

tons and deuterons In the case where the scattered electron has caused a

change in the internal structure of the proton this collision is called inelastic

Inelastic collisions are clearly identied by the kinematic relationship of the

incoming and scattered electron The inelastic b ehavior of the target protons

and deuterons was measured for a range of scattering angles and energies

Several imp ortant prop erties of the quark mo del and the strong interac

tion were measured in electronnucleon deepinelastic scattering exp eriments

The scattering data from dierent energies and angles was found to b e related

by a sp ecic scaling prop erty now called Bjorken scaling This b ehav

ior implied that pointlikecharged constituents were present within protons

and neutrons and that these constituents behaved as free particles at least

for a short time in deeply inelastic collisions The electron scattering data

also determined by means of the GrossCallan relationship that the charged

constituents in nucleons were spin particles

Electrons were not the only means of lo oking inside of a nucleon High

energy neutrinos prob e the nucleon by means of the weak interaction alone

The uniquely dierent interaction of the neutrino was used by D Gross

and C LlewellynSmith to derive a sum rule which counted the net num

ber of quarks present in nucleons The quark mo del prediction of Gell

Mann and Zweig of nucleons containing three quark constituents was ver

The History Behind SubNuclear Particles Quarks

ied by the Exp eriment at the Europ ean Center for Nuclear

ResearchCERN in

Quantum Chromo dynamics

That something missing from the strong interaction was arriving A new

quantity emerged that would be the analogue of the electric charge for the

strong interaction It was called color The b ehavior of color explained the

uuu wavefunction and why hadrons had no longrange strong inter

action The dynamics of color however such as why quarks were conned

free particles in deepinelastic scattering to hadrons but still behaved like

exp eriments were as yet unknown

In D Gross and F Wilczek and indep endently HD Politzer cal

culated asymptotic freedom for the nonAb elian gauge theory based on an

exact SU color symmetry group This theory also called Quantum

Chromo dynamics or QCD plays the part of the renormalizable eld theories

used to describ e the weak and electromagnetic interactions It is the funda

mental theory of the strong interaction For the region in energy where the

strong coupling constant is small accurate QCD calculations can be made

and compared with exp eriment

Quarks and the Electroweak Interaction

The unication of the weak and electromagnetic forces implied that left

handed quarks came in doublets This parallel to the weak chargedcurrent

interaction of leptons gave structure to the assignment of quark charges and

avors The rst verication of this theory came from the results on elas

tic neutrinonucleon scattering measurements made by the Gargamelle Ex

periment at CERN in the discovery of neutral currents Elastic

scattering of a neutrino o of a quark was predicted to o ccur through the ex

change of the massive Z particle This particle was later pro duced in proton

antiproton collisions at CERN in

The picture of the electroweak doublets of particles was incomplete

Both the theoretical analyses of axial anomalies and the GlashowIliop oulos

MaianiGIM mechanism implied the existence of a second charge

quark The GIM mechanism as it applied to neutral kaon decays to

dimuons was used to estimate the mass of the missing charm quark

Gluon Radiation from Quarks

neutrino electronneutrino

e

muon e electron

quark u

quark d s strangequark

Electroweak Doublets Known Quarks and Leptons in the Year

In November of the charm quark was discovered in the form of the

narrow charm anticharm quark bound state pro duced in b oth the proton

xedtarget exp eriment of Samuel CC Ting in Bro okhaven New York and

in electronp ositron collisions at SLAC in California This moment of time

was known as the Nov emb er Revolution It marked an incredible p erio d of

scientic development in the area of particle physics There were nowknown

to b e four quarks A standard mo del describing the electroweak interactions

of b oth quarks and leptons had b een formed

Gluon Radiation from Quarks

In QCD quarks are attracted to each other by the exchange of In

highenergy collisions quarks can radiate gluons in the same way as electrons

exhibit photon emission in the electromagnetic interaction An essential

prop erty of gluons and the strong interaction is that the gluons themselves

carry the color charge Scattered quarks and energetic gluons will always

form hadrons from the growing strength of the strong interaction as colored

particles separate Hadrons are colorless and exhibit no longrange strong

interaction

In the PETRA accelerator in Hamburg Germany began colliding

electrons and p ositrons in the search for the QCD prediction of gluon emission

from quarks This was a dicult step for the four PETRA exp eriments as

the observation of jets of hadrons coming from energetic quark pro duction

was a new phenomenon The pro duction of a quark antiquark pair with

in addition the emission of an energetic gluon causes three jets of particles

to be formed The QCD prediction that these jets of particles should line

in a plane and that the angles and energies of the three jets should follow

a statistical pattern was veried in particular by the MARKJ TASSO

and PLUTO Exp eriments The rst measurement of the strength of the

The History Behind SubNuclear Particles Quarks

strong interaction coupling constant for threejets events was p erformed by

the JADE Exp eriment indicating a size over a factor of larger than the

electromagnetic interaction

THE AND ITS HELPERS

This chapter contains all the theory and phenomenology needed to describ e

and interpret the measurements presented in Chapter

Fundamental Interactions

The Dirac equation intro duced in was the rst relativistically covariant

equation describing a quantum mechanical spin particle The equation

in mo dern notation is written

i m

where m is the mass of the particle

iq xt

The ability to change the phase of the wavefunction e

h varies in space and time x t violates the covariance of in a way whic

equation

The covariance is reestablished by intro ducing a eld A such that

A A A

D iq A

The Dirac equation written with the covariant derivative D now describ es

the motion of a particle with charge q interacting with an electromagnetic

eld

Electromagnetism is an example of how lo cal gauge invariance generates

a fundamental interaction describ ed by a eld To describ e the weak and

electromagnetic interactions together the covariant derivative b ecomes

Y

D ig T W ig B

This intro duces three new elds W W W W and in addition the

electromagnetic interaction has changed slightly now written B as will

The Standard Mo del and Its Help ers

be explained b elow The op erator T determines the strength of the weak

interaction The magnitude and comp onents of T are dierent for right

handed and lefthanded particles

Quarks and leptons are characterized by the way they interact under

the weak interaction as seen in Table Lefthanded particles app ear in

and righthanded particles are singlets T doublets T

The LeftHanded World The RightHanded World

leptonneutrino

e

lepton e e

L L L R R R

u quark c t u c t

L L L R R R

quark d s b d s b

L L L R R R

Tab The World of Quarks and Leptons is Split by the Weak Interaction

The weak interaction as it w as intro duced in equation lacks one of

its most telling features that is being weak Fields such as A have an

equation of motion They are in their own right particles as the photon

is the particle describ ed by A Apart from the coupling constants b eing

p otentially smaller the interaction would be weak if the particles describing

the W had nonzero masses

The theoretical diculty with intro ducing a nonzero mass to a eld is

that the equation of motion describing the eld loses its invariance under

lo cal gauge transformations Even so the lo cal gauge invariance can be

present but hidden through relationships between masses and couplings

The masses of the particles describing the weak interaction were discovered

by way of a theory of hidden gauge invariance known as the electroweak

theory of S Glashow A Salam and S Weinberg

The handedness of a particle is determined by the relativeorientation of its spin and

momentum

Fundamental Interactions

The GSW Standard Mo del of Electroweak Interactions

Starting with the covariant derivative the kinetic energy of a spin

particle is given by

Y

B j j ig T W ig

In the case where the spin particle has a selfinteracting p otential known

as the Higgs p otential

V jj jj

for and p ositive the minimum value of jj is nonzero jj

min

With jj nonzero the kinetic energy term of the Higgs particle be

min

comes the dierence of with resp ect to its minim um p otential energy In

the single doublet mo del T Y this minimum is chosen to b e

p

p

hi

This generates a constant term from the kinetic energy

Y

B hi ig T W ig

g

gW g B W iW W iW

M Z M W W

Z W

namely the masses of the W W and Z particles which are the physical

elds of the weak interaction The remaining eld

g W gB

p

A

g g

is the massless eld of the electromagnetic interaction

The Standard Mo del and Its Help ers

The Prop erties of Quarks from Z Decay

The couplings of the Z to quarks and leptons listed in Table can be

separated into lefthanded couplings and righthanded couplings by use of

the helicity pro jection op erators acting on a particle f

f f f f

L R

Then expressing the interaction in the form

f f

f Z c f c

L R

f f

the values for c and c are

L R

f f

c T q sin c q sin

W W

L R

with

sin M M

W

W Z

sin

W

where the eective coupling sin deviates from the treelevel coupling

W

Of particular interest to the measurements made in Chapter is the

fraction of Z decays to quarkantiquark q q pairs

BrZ q q

P

f f

N jc j jc j

c

L R

f duscb

P P

f f f f

jc j jc j N jc j jc j

c

L R L R

f duscb f e

e

where N is the number of colors in the strong interaction

c

The longitudinal p olarization of quarks coming from Z decay is

f f

jc j jc j

L R

P P

q q

f f

jc j jc j

L R

This deviation allowed LEP measurements to predict the mass of the top quark b efore

it was discovered at Fermilab in Similar predictions now exist for the Higgs mass

The quark sums have b een mo died by a QCD correction factor M

QCD s Z

not written in the ab ove formula This factor gives crosssection measurements sensitivity

to the strong coupling constant

Quantum Chromo dynamics

Quantum Chromo dynamics

The inclusion of the elementary strong interaction into the covariant deriva

tive adds eight new elds The particles asso ciated to these elds are called

gluons

Y

D ig T W ig B ig G

s

G The eight elds G G G G G G G G

p

p r g g r

br bg

r rg g

r rg gbb r b g b

have a corresp ondence to the eight generators of the SU color group The

gluon indices are closely linked with color ow Figures and

q

r

q

b

Fig Color ow demonstrated in single gluon exchange

r

g

b

Fig Color ow demonstrated in the triple gluon vertex

The strength of the strong interaction changes with scale following the

principle of the renormalization group The strong coupling

g

s

s

Electroweak symmetry breaking will not generate mass in the gluon elds as long as

the Higgs scalar has no color charge

The indices r g and b represent the colors red green and blue The combination of all three colors is white or color neutral

The Standard Mo del and Its Help ers

has a dep endence on the renormalization scale which to onelo op is given

by

s

s s

b N N

s c f

where N is the number of colors and N is the number of quark

c f

avors contributing to the lo op corrections This equation predicts that the

strength of the strong coupling constant decreases at high energy It also

identies a quantity known as the Landau p ole

C

exp

C

b

s

At the scale of the Landau pole the strength of the strong interaction be

comes divergently strong This is believed to be reason why all quarks and

gluons b ecome conned within hadrons Connement cannot be calculated

with Feynman p erturbation theory and only has an approximate phenomeno

logical description

Hadronization Phenomenology

Twotyp es of hadrons have b een measured by exp eriments These are mesons

b ound states of q qandbaryons b ound states of qqq and their antiparticles

In b oth cases the color p otential for the singlet combination is attractive

typ e Color Representation Color Coupling of the Singlet

singlet negative is attractive

mesons

s

baryons

s

Tab Sign of the Potential Energy for Color Singlet Combinations

The basic features of hadron pro duction rates in e e annihilation are

describ ed by the following parameterization

E

J

bind

N

s

T

p

e hN i C

s

s

C

B

First computed by D Gross and F Wilczek and indep endently by HD Politzer

Quantum Chromo dynamics

The rate hN i is the exp ected number of primary hadrons pro duced per

p

event The overall normalization factor C dep ends on the centerofmass

s

energy The parameter C is a suppression factor for baryon pro duction

B

dened to be for mesons The constants T and are universal and

s

the values of J N and E dep end on prop erties of the hadron Namely

s bind

J is the total intrinsic angular momentum N is the number of strange

s

quarks in the hadron according to the quark constituent mo del and E

bind

P

m is the hadron binding energy A list of tted parameters for M

q h

i

i

equation is given in Table

p

Parameters s GeV Simultaneous Fit

s

m GeV

T GeV

p

C C

s

C

B

dof

C C

Tab Fit values for LEP data and to data at dierentcenterofmass energies

The observed rate of hadrons dep ends on the numb er of primary hadrons

pro duced describ ed by equation and on the number of hadrons pro

duced from decays socalled feeddown Feeddown can be computed by

predicting all of the primary hadron pro duction and then computing the

decay contributions for all hadrons up to a mass of GeV from measure

ments in the Particle Data Bo ok Hadron masses ab ove GeV have

suciently small pro duction rates to b e neglected an exception to which are

hadrons pro duced directly from c and b quark pro duction discussed in

Primary hadrons are those which arise directly from the transition of quarks into con

ned particles The quark avor distribution of the inital q q pair aects hadron pro duction

rates and is accounted for separately

The values of the strange quark constituentmassm and the up and down constituent

s

masses are also needed The assumptions and denitions used for Table are that

m GeV m m and m m  m

s u d s u

The Standard Mo del and Its Help ers

Hyp eron Decay

The prop erties of hyp eron decay are accurately parameterized by a phe

nomenological interaction density

y

g g g g H

p p int

p

p

where the two terms corresp ond toand decay resp ectively

Parity nonconservation in hyp eron decays which is presentinH when

int

b oth g and g are nonzero was exp erimentally discovered in following

the insight of TD Lee and CN Yang A consequence of parity violation

is the p ossibility to measure the p olarization of hyp erons based on decay

angular distributions

The p olarization observable hs ip changes sign under a parity trans

formation The sp ecic implication is that the hyp eron deca y rate will have

a p olarization dep endence on the decayangular distribution of the pion

d

P cos

dcos

where P is the magnitude of the p olarization The measured values of for

several hyp erons are given in Table

Hyp eron

p

n

p

n

p

n

Tab Hyp eron Decay Parameters

PARTICLE ACCELERATION AND COLLISION

The Large ElectronPositronLEP Collider

The design criteria for the LEP Collider were largely inuenced by the opp or

tunity to study in detail the prop erties of the massive particles resp onsible

for electroweak interactions In particular a machine achieving electron

p ositron collision energies of approximately GeV would be capable of

studying the pro duction and decay of the Z particle At GeV the pair

pro duction of W W could b e observed These twogoalswere achieved after

the machine was constructed in Some of the lineshap e data collected

by the L Exp eriment from e e collisions pro duced by LEP from several

years of op eration is displayed in Figure ] 1992 Data nb

] L3 [ L3 1991 Data 30 1990 Data 30 pb [ )) Fit Result γ )) γ ( 20 − 20 W + hadrons( W → → 0 − Z 10 e 10 +

→ Data (e − Standard Model σ e

+ no ZWW vertex ν (e e exchange

σ 0 0 88 90 92 94 96 160 170 180 190 200

Collision Energy [GeV] Collision Energy [GeV]

Fig L CrossSection Measurements for Z and W W Pro duction

LEP is a circular collider building up on the existing system of circular

accelerators op erated at CERN There are four exp eriments situated around

Particle Acceleration and Collision

the km circumference of the LEP ring These are L ALEPH OPAL and

DELPHI Their relative lo cations can be seen in Figure

ALEPH LEP OPAL LEP: Large Electron Positron collider SPS: Super AAC: Complex ISOLDE: Isotope Separator OnLine DEvice

North Area PSB: Proton Synchrotron Booster PS: Proton Synchrotron

SPS LPI: Lep Pre-Injector L3 DELPHI EPA: Electron Positron Accumulator LIL: Lep Injector Linac LINAC: LINear ACcelerator West Area LEAR: Low Energy Antiproton Ring

AAC

ISOLDE East Area pbar electrons * PSB LPI e+ PS e- protons e- * EPA LIL antiprotons Pb ions

LINAC2 South Area

LINAC3 LEAR

p Pb ions

Fig CERN Accelerator Complex

The acceleration to the nal collision energies achievable by LEP pro ceeds

rst through a chain of multipurp ose accelerators generally referred to as

the injector chain

LEP Injector Chain

The LEP injector b egins with two linear accelerators in tandem a high

current MeV electron linac used for p ositron pro duction followed by a

lowercurrent linac for accelerating electrons and p ositrons to MeV prior

to injection into the ElectronPositron AccumulatorEPA The linacs pro

duce a nanosecond pulse of p ositrons or electrons every milliseconds

These pulses are accumulated into bunches of particles which circulate in

The Large ElectronPositronLEP Collider

the EPA Since p ositrons need to be created from electron collisions with a

target p ositrons are accumulated times slower than electrons

After seconds of p ositron accumulation the bunches are transferred to

the Proton SynchrotronPS accelerator These are accelerated to GeV

b efore injection into the Sup er Proton SynchrotronSPS The SPS accel

erates up to GeV and then transfers the electron and p ositron bunches

into LEP The lling rate is roughly milliAmpsminute and the total

currents accelerated by the LEP machine is ab out milliAmps of p ositrons

colliding with milliAmps of electrons

LEP Main Ring

In the LEP main ring the system of acceleration is based on the radio

frequency oscillation of electric elds within conducting and sup erconduct

ing cavities As electrons pass through a cell of a cavity the electric elds are

timed to oscillate in a direction of acceleration see Figure for a picture

of LEP copp er RF cavities A corresp onding timing is also present for the

p ositrons which countercirculate in the same beam pip e as the electrons

The time interval referring to a p erio d of RF electric eld oscillation is called

an RF bucket

There are an integral number of RF buckets in the LEP machine The

number is and the frequency of oscillation is MHz The RF

buckets are the basic building blo ck for setting up the timing of collisions at

the interaction p oints of the four LEP exp eriments Several timing schemes

were using during the and years of op eration as shown in Table

of Bunches Bunch Spacing of Bunchlets Bunchlet Spacing

s RF Buckets s RF Buckets

s

s

s s

Tab LEP Accelerator Timing Schemes During and

An amazing asp ect of the CERN accelerator complex is the ability of the SPS to

handle an electron and p ositron injection momentum of GeV by setting the b ending

elds down to roughly Gauss while one second b efore they were set at Gauss

during proton acceleration for the North Hall and West Hall xedtarget exp eriments

The cycling of particles through the machines is called the SPS Sup erCycle whichhasa p erio d of ab out seconds

Particle Acceleration and Collision

Fig LEP Copp er RF Cavities The evacuated b eam pip e containing the

electron and p ositron b eams is lo cated in the right b ottom of the picture

b efore it passes into a series of copp er RF cavities The waveguides

feeding the RF cavities from the left are connected to a nearby Klystron

The L Exp eriment

The L Exp eriment is p ositioned at one of four main interaction points of

LEP It was constructed by a group of physicists technicians and engineers

from dierent countries from around the world The leader of the

collab oration is Samuel CC Ting The op eration of the detector b egan with

the startup of LEP in and has continued through

Two of the most visible features of the detector design are the large

volume electromagnet which houses the exp eriment and a long stainless

steel supp ort tub e The supp ort tub e susp ends all of the detector comp o

nents in midair along the central axis of the magnet as seen in Figure

What is called the L Detector is actually a collection of many individ

ual subdetectors each designed to make sp ecialized measurements These

comp onents are drawn in Figure

Bunchlets are a substructure of a normal bunch sometimes called bunch trains

Listed in the Guinness Bo ok of Records as the Worlds Largest Electromagnet

The L Exp eriment

Fig The L Magnet and Supp ort Tub e During Installation

In this picture the do ors of the magnet are op en and the newly installed

supp ort tub e has b een p ositioned along the center of magnet

Muon Detector

Magnet Coil

e+ Door

BGO Crystals Luminosity Monitor

Hadron Calorimeter Inner Tracking e-

Fig Persp ective View of the L SubDetectors

Particle Acceleration and Collision

SubDetectors of the L Exp eriment

Here is a list of the principal detector subsystems and their function

Inner Tracking Detectors Charged particles originating directly

from the e e interaction p oint or so on after will have their tra jecto

ries measured by the inner tracking detectors

Silicon MicroVertex Detector Records accurate p osition infor

mation immediately outside the b eam pip e volume

TimeExpansion Chamber Measures the curvature of charged

tracks b ending under the action of the solenoidal magnet eld

ZChamber Determines how far forward or backward a charged

particle has travelled b efore leaving the volume of the inner track

ing detectors

Electromagnetic CalorimeterECAL A homogeneous scintillat

ing crystal calorimeter comp osed of Bismuth Germanate Bi GeO

generally referred to as BGO Measures the total energy of electrons

p ositrons and photons In addition it acts as the rst nuclear interac

tion length for combined energy measurements with the HCAL

Hadron CalorimeterHCAL Consists of uranium absorb er plates

instrumented with prop ortional wire chamber readout Measures the

energy of pions protons and other strongly interacting particles by

sampling showering particles in b etween layers of absorb er plates

Muon Chamb ers pass through the many tons of BGO ura

nium and steel to leave acharged track in these cham b ers

Barrel Chambers Three layers of drift chambers mounted on the

exterior of the supp ort tub e Measures the curvature of muon

tracks due to the magnetic eld of the solenoid

ForwardBackward Chambers Muons travelling through the do ors

of the magnet are b entby a toroidal magnetic eld These cham

bers measure the amount of deection to determine the momen

tum of the muon

Scintillation Counters Positioned between the ECAL and HCAL

they determine the time at which particles have passed through the

counters to subnanosecond precision Used for cosmic m uon rejection

and LEP bunchlet tagging

The L Exp eriment

Luminosity Monitor Designed primarily to detect electronp ositron

scattering at small angles it provides a highstatistics measurementof

the collision luminosityofthe LEP beams

Trigger and DataAcquisition System

Essential to the op eration of the exp eriment is a system which determines

whether or not a particle has been detected by one of the subdetectors

Following initial particle detection a decision is made as to whether the

detector should record the information measured ab out this particle and

p otentially other particles which have interacted with the detector This

system is called the trigger and dataacquisition A decision is made

every time the LEP b eams are broughtin to collision The amountoftimeto

make the level trigger decision is less than the time b etween bunchcrossings

see Table for bunch spacings Further reductions in the number of

recorded events are made by two additional levels of trigger logic The nal

rate of events recorded to tap e during highluminosity LEP running is roughly Hz

Particle Acceleration and Collision

TRACKING AND CALORIMETRY

A photographic camera records an image by a technique that dep ends on

how visible light interacts with a chemical emulsion In the same way a

uses the interactions of longlived particles not sp ecically

visible light to form a picture of what has happ ened in a highenergy colli

sion In particular charged pions protons and antiprotons and photons are

detected by the tracking and calorimetry Detector readings are translated

into measurements by anticipating the pattern of readings exp ected from

individual particles and groups of particles

Tracking

Ideal Tra jectories

A charged particle moving in a uniform magnetic eld will follow the path

of a helix in space A convenient form for describing this tra jectory is given

by the following equations J Alcaraz L Note

C s C s

cos x x sin s sinc

r

C s C s

y y cos s sinc sin

r

z z s tan

These functions dene vequantities C tan z whichmust b e de

termined from the measurements made by the tracking system The param

eterization is in three indep endentvariables xy z that represent a p osition

in space The variable s is an arc length in the x y plane The co ordinate

x y is used as a reference from which to compute and

r r

Tracking and Calorimetry

The Geometry of the Tracking Detectors

Charged particles originating from within the beam pip e will traverse three

dierent tracking detectors b efore reaching the calorimetry These are the

Silicon MicroVertex DetectorSMD the Time Expansion Chamb erTEC

and the ZChamb er as shown in Figure Each tracking detector mea

sures co ordinates along the tra jectory of the charged particle The p osition

resolution changes from m in the ZChamb er to m in the TEC to

m in the SMD This follows the progressive imp ortance of extrap olating

the measured track back to its pro duction vertex

Grid Z-Chamber { Anodes Cathodes Grid

Outer Charged TEC particle Inner track TEC SMD Vertex

Y B

X

Fig The Inner Tracking Detectors of the L Exp eriment Acharged

particle pro duced within the beam pip e will rst cross the SMD then

the TEC and nally the ZChamb er b efore hitting the calorimetry

Tracking Measurements

A charged particle suers energy loss due to ionization as it travels through

materials The precision by which the p osition of ionization can be deter

Tracking

mined within a gas or silicon substrate is the intrinsic resolution of the track

ing detector In a silicon detector and in a gaslled strip chamb er the strip

pitch as well as the charge sharing on neighb oring strips determines the in

trinsic resolution In a drift chamb er the situation is a bit more complicated

The p osition within the chamb er is measured by the time it takes for ioniza

tion electrons to drift through the gas under the inuence of an electric and

magnetic eld

Silicon MicroVertex Detector

The SMD consists of m thin wafers of silicon with microstrips of dop ed

silicon and metal implanted on b oth the top and b ottom surfaces The

microstrips are accurately placed on the silicon wafer with the same tech

nology made for electronic integrated circuits in chip fabrication When a

voltage bias is applied across the volume of the silicon wafer electronhole

afer when an ionizing particle passes through will pairs created within the w

be collected by nearby strips on b oth surfaces as shown in Figure

Ionizing Particle

n +

  + + − holes + − − + 300 μm + − + − electrons −

                                                                                                                              p+

50 μm

Fig Charge Sharing on Neighboring Strips in the SMD

An ionizing particle passing through a silicon wafer will create electron

hole pairs in the interior of the silicon Electrons are collected by strips

on the b ottom surface and holes by strips on the top surface

Charged particles crossing the SMD will hit two layers of doublesided

silicon The orientation of the microstrips on two surfaces is orthogonal

Since the wafer is very thin and carefully supp orted a measurement of a

co ordinate from strips on the top and b ottom surfaces can be accurately

Tracking and Calorimetry

translated to a point in space along the tra jectory of a charged particle

An imp ortant geometrical arrangement of the two layers of silicon greatly

improves the pattern recognition of assigning the correct strip readings to a

track as seen in Figure

True Tracks

Outer Layer Rotated 2 degrees

Ghost Tracks

Fig Stereo Arrangement of the Silicon Layers in the SMD

The correct assignment of strip co ordinates to charged particle tracks

is aided by the degree rotation of the outer silicon layer An incorrect

pairing of strip co ordinates will cause a reconstructed tracktopoint back

to a dierent pro duction point The black lines drawn on each layer

represent the microstrip readings

The grouping of strips in the readout of the SMD is optimized to reduce

the number of readout channels while not deteriorating the intrinsic p erfor

mance of the tracker In particular the angle at which an ionizing particle

crosses a wafer changes the charge sharing on neighb oring strips and there

fore the accuracy of determining the strip co ordinate In lowangle regions

the number of z strips which are readout is reduced The strip co ordinate

errors listed in Table were determined from ts to the and

data

TimeExpansion Chamber

The tracking detectors are immersed in the uniform magnetic eld of the

L solenoid This eld p oints along the axis of the beam pip e Therefore

charged particles traveling transverse to the b eam pip e will followa circular

Tracking

Silicon Layer Strip Co ordinate Error m Readout Pitch Region

strips m m

z strips m m tan m

m m tan m

Tab SMD Strip Co ordinate Errors

path The curvature C of this path is related to the transverse momentum

p of the particle through the relationship

t

BkG cms

where C is measured in mm p GeVc

t

jC j

Curvature is the quadratic deviation from a straightline tra jectory there

fore the accuracy with which it can b e measured has a quadratic dep endence

on the span of the co ordinate measurements made on a track

The total lever arm available for co ordinate measurements in the TEC

is cm radially with an additional cm to the innermost SMD layer

To comp ensate for this relatively short lever arm the TEC was sp ecially

designed to attain driftdistance measurements as accurate as m one

of the best ever achieved with a drift chamb er The technique relies on a

low driftvelo city region complimenting an accurately describ ed amplication

region These regions are drawn in Figure An example of the achieved

resolution measured in data is shown in Figure for an outermost

TEC wire

Track Fitting and Error Propagation

Material eects within a tracking region are characterized by the angular

deection of a particle from multiple scattering

r

X MeV

cP X

where X is the radiation length of the material X is the length of material

traversed and P is the momentum in MeVc of the particle The particle

velo city normalized to the sp eed of light contains the multiplescattering

The symbol  indicates that the errors are added in quadrature

Tracking and Calorimetry

Grid Grid Charged Cathode wires . wires track plane Focus wire . . Anode wire . . Amplification Drift

region region

Fig The Electric Field Lines of the TimeExpansion Chamber

Electrons pro duced by ionization drift under the inuence of a low

strength uniform electric eld from the side of the Catho de towards the

Grid wires Electrons which pass the Grid wires enter a high electric eld

region and are fo cused onto an Ano de wire The timing measurements of

when the rst ionization electrons reacheach of the Ano de wires relative

toaTimeMarker reference are the principal measurements of the TEC

dep endence on the charged particle mass m

r

P

P m

For P MeVc a proton has a factor of larger contribution from

multiplescattering errors than acharged pion

To p erform track tting in the presence of dense materials a mathe

matical technique called Kalman ltering is used The Kalman lter needs

both an initial estimate of the tra jectory parameters of the track and the

In RE Kalman develop ed an optimal solution for estimating linear dynamic

systems in the presence of random Gaussiandistributed deviations One of the rst ma jor

applications of this technique was done by the Jet Propulsion Lab oratory for the guid

Tracking

TimeExpansion Chamber

0.4 Fig

Single Wire Resolution

diusion in the gas

0.3 Electron causes large drift distance mea

0.2

surements to have increasingly

resolution (mm) larger errors

→ 0.1

0 02040 → drift distance (mm)

TEC wire 62+

measurement errors in the form of acovariance matrix These estimates are

provided by the TEC The ano de wire measurements are t with the ideal

tra jectory equations and the t errors are used as an initial estimate

of the covariance matrix

The Kalman lter track t pro ceeds through several steps First the

extrap olation of the track back through the dense material layers lo cated

between the TEC drift volume and the b eam pip e vacuum must b e accurately

computed In particular the track tra jectory parameters are allowed to

change within the errors estimated from multiplescattering b etween the TEC

drift volume measurement and the SMD measured co ordinates Then the

Kalman lter iterates over the tra jectory predictions and SMD measurements

to determine the b est error estimation and track extrap olation into the b eam

pip e vacuum where the particle is assumed to originate

Calculation of the Primary Vertex

When several particles originate from the same p ointinspace they are said

to come from a common vertex The lo cation of this vertex can b e computed

from the intersection of the measured chargedparticle tra jectories The pri

mary vertex of a highenergy collision o ccurs within the beam pip e vacuum

and sp ecically within the overlap of the electron and p ositron b eam currents

ance system of the Ranger rob ot spacecrafts sent toward the Earths mo on in the early

s Optimal combination of radar data with inertial sensor readings pro duced an

overall tra jectory estimate with a minimum exp enditure of fuel

This calculation is p erformed by the GEANE package and makes use of a detailed description of the detector geometry and materials

Tracking and Calorimetry

set by the LEP machine The physical ap erture over which the LEP b eams

are collided is called the b eam sp ot see Table

LEP Beam Sp ot Size m

m

x

m

y

m

z

Tab LEP Beam Sp ot Size in and

The calculation of the primary vertex requires foremost a set of tracks

which have accurate error estimations of their tra jectory within the b eam

pip e vacuum This is achieved with the Kalman lter describ ed in Sec

tion The weeding out of tracks which do not b elong to the primary

vertex is done with a probability calculation

N

trk

X

T

T

t f v q G v v t f v q v v V

i i ll i i ll

N

i

ll

trk

i

th

where t is the vector of measured parameters for the i track and G the

i i

corresp onding covariance matrix f v q are the predicted measurements

i

assuming the track originated from the vertex v with momentum q and

i

with V describing the size of the beam sp ot The v is the llvertex

ll ll

dimension of t is corresp onding to the measurements C tan z

i

of the ideal tra jectory equations

For each track the probability P P is computed and

i

N N

trk trk

if either the probability of the vertex t P is below or any P

i

N

trk

is below the track with the lowest P is removed The t pro cedure is

i

iterated until no track needs to be removed If in the end less than three

tracks remain no primary vertex is computed

The primary vertex calculation is the work of Gerhard Raven L Note

The LEP machine is p erio dically lled with electron and positron beams see Sec

tion A single ll provides enough collision luminositytolasttypically hours The

llvertex is the average vertex p osition determined over this interval

Calorimetry

Calorimetry

Electromagnetic Showers

Photons with an energy more than an order of magnitude larger than the

mass of an electron will interact with dense matter primarily through the

pro cess of electronp ositron pair pro duction Similarly electrons and p ositrons

will interact with atomic nuclei to radiate photons through the bremsstrah

lung pro cess as shown in Figure These pro cesses o ccur roughly once p er

every radiation length of material encountered and the particles pro duced in

these interactions will also interact with the material As b oth pair pro duc

tion and bremsstrahlung involve one particle coming in and two going out

the total number of interacting particles increases geometrically

e

Pair Pro duction

nucleus

e

e

Bremsstrahlung

nucleus

e

Fig Electromagnetic Shower Development

The pro cesses resp onsible for electromagnetic shower proliferation in

dense materials are pair pro duction and bremsstrahlung

The proliferation of photons electrons and p ositrons pro duced from pair

pro duction and bremsstrahlung is called an electromagnetic shower The

energy of all the particles pro duced in a shower is eventually absorb ed by

atomic electrons once the interaction energies are below twice the electron

mass Direct interactions with atomic electrons include Compton scatter

ing the photo electric eect lowenergy electronp ositron annihilation and

ionization loss

Masses and energies can b e directly compared when expressed in units where the sp eed

of light is equal to from Einsteins E mc

Tracking and Calorimetry

The Geometry of the Electromagnetic Calorimeter

Surrounding the inner tracking system of the SMD TEC and ZChamber is

an electromagnetic calorimeter comp osed of Bismuth GermanateBGO A

total of individually instrumented BGO crystals are arranged to form

two halfbarrels and two endcaps as shown in Figure



Beampip e

Fig BGO Electromagnetic Calorimeter Geometry

One of the purp oses of the BGO detector is to measure the energy of pho

tons pro duced within the b eam pip e or tracking volume The BGO crystals

point almost directly towards the primary interaction region and provide

more than radiations lengths of stopping p ower for electromagnetic show

ers

In a BGO crystal the passage of lowenergy electrons and p ositrons

through the crystal lattice causes shortlived excitations in the system of lat

tice electrons The sp ecial prop erty of these crystals is that the deexcitation

of lattice electrons can generate green light As the crystal is optically trans

parent the numb er of scintillation photons can b e counted with photo dio des

attached to the surface and the amount of scintillation can b e used to com

pute the energy of the electromagnetic shower

The BGO crystals in the barrel p ointaway from the primary vertex in azimuthal angle

to prevent particles from traveling down the cracks b etween adjacent crystals The BGO

endcaps were never fully pushed up against the barrel and therefore are nonp ointing

This was done to keep the endange of the tracking detector from shadowing the barrel

and to make space for the tracking cables to pass b etween the BGO barrel and endcap

Calorimetry

The Electromagnetic Shower Shap e

The spatial extent of an electromagnetic shower has a characteristic lateral

size as can be seen in Figure The mean p ercentage of containment in

the centralmost crystal of a shower is roughly The remaining p ortion

of the shower energy is mainly distributed in neighb oring crystals However

some energy is lost in the supp ort material b etween crystals and in the case

of electromagnetic showers below GeV frontend leakage of the shower

b ecomes signicant as discussed in Section Rearend leakage however

is b elow even for GeV show ers

l

l

Energy

Crysta

Energy

Crysta

 

Fig Electromagnetic Shower Shap e in the BGO

On the right is the distribution of energy measurements exp ected in each

crystal from an electromagnetic shower centered on an arrayofBGO

crystals On the left is the continuous lateral distribution of energy de

p osition exp ected in a single crystal The amount of energy dep osition

exp ected at a p oint in the integral over the volume of a crystal This

distribution is known as the transverse shower shap e

The distribution of energy measurements in crystals surrounding the

centralmost crystal is the only means of identifying electromagnetic show

ers Once identied more precise information can be computed ab out the

shower such as b etter p osition and energy measurements

Statistically Determined Errors on Energy and Angular

Measurements

The BGO calorimeter stands prominently as the most accurate photon de

tector at LEP The behavior of the measurement errors with photon energy and angle is simply describ ed and lends itself to statistical parameterization

Tracking and Calorimetry

The rst resolution function to b e studied was the energy resolution in the

barrel region The highenergy p erformance of the barrel was studied exten

sively in the years in the CERN X test b eam line and with sim

ulation These measurements were p erformed at and GeV

Below GeV the resolution curve was supplemented with ideal simulation

data for photons in hadronic decays of the Z An imp ortant asp ect of

lowenergy photon measurements can b e seen in Figure Namelythere

Entries 1809 100 Mean -.1272E-01 RMS .6711E-01 UDFLW 34.00 OVFLW 2.000 62.89 / 81 80 A 70.96

x0 .01265

FrontEnd Leakage xc -.01021 Fig

σ .03806

distribution of the

60 The

fractional error in MeV

photon energy measure

40

ments shows a tail toward

low energy 20 Number of Measured Photons/Bin

0 -0.2 -0.1 0 0.1 0.2

Δ(E-EMC)/E

are two distinct energy resolution functions one for the upp eredge and one

that describ es the tailing distribution

In order to match up with the already wellmeasured Gaussian error dis

tributions at highenergy a split function was used to t the width of the

photon energy distributions

A expax x if x x

c

f x

B exp bx x if xx

c

where a b ax x and B A exp ax x This

c c

leaves four free parameters the three parameters Ax for a Gaussian

upp eredge t and one parameter x which splices in an exp onential tail

c

continuously and which is smo oth in the rst derivative A combined t of

Ideal running conditions means in this case no calibration errors p erfect linearityno

electronic noise no missing channels and a xed energy threshold of MeV for all crystals

Calorimetry

the X data and the Gaussian error from the supplemental data results in

a resolution function which is the same as the resolution function of the X

data alone

Gaussian

p

E E

E

E

To account for the tailing distribution on the lower side the RMS was com

puted of the t function for several energies This results in a more

accurate resolution function for low energies

E

Full

p

E E exp

E

E

Both the Gaussian and full energy resolution functions are plotted in Fig

ure

10 12.00 / 11 14 9 P1 3.418 .2916

P2 .8539 .1163 Neglecting Crystal Size

(E)/E (%) 8 12 E (E) (mrad) φ

σ

7 σ

10

Full

6

8 5

4 6

3

4

2 2 1 Gaussian

0 0 10-1 1 10 10-1 1 10

E (GeV) E (GeV)

Fig BGO Resolution Functions in Energy and Angle

On the left are the two curves describing the energy resolution in the

BGO barrel On the rightistheresolution function in the barrel

The second resolution function to b e studied was the angular resolution

function in the barrel The data from X at and GeV was

To avoid underows the lowenergy exp onential term should be set to zero ab ove GeV

Tracking and Calorimetry

supplemented with simulation data down to MeV An imp ortant eect

found only b elow MeV comes from the limiting angular resolution from

the nite size of the crystal Singlecrystal photon measurements will have

p

mrad the RMS of a at an angular resolution of mrad

distribution with mrad being the average angular size of a crystal in

The resolution function for all energies was found to be

mrad

p

E mrad

E E E

c

with

E

h i

E E

c

E E

exp

E

and is plotted in Figure The value E GeV was determined

from the limiting angular resolution and a t to the data

The resolution function in the barrel and all of the endcap resolution

functions are summarized in App endix A

Gain and Oset Calibration of the Electronics

The wide range of energies measured by the BGO calorimeter is digitized with

a oatingp oint ADC The basic principle b ehind a oatingp oint ADC is

to use an accurate Nbit ADC with a short conversion time to cover a

dynamic range of signals which is larger than N bits This is done by making

several copies of the signal with dierent linear amplications The cop y

which has the highest amplication but is still within the range of the Nbit

ADC will have the least digitization error The digital readings therefore

have N bits of mantissa from the ADC and a few bits to record which signal

amplication was used for digitization This format is commonly known as

a oatingp oint representation

The calibration of the gains and osets internal to each oatingp oint

ADC matches up the dierent linear amplication regions to pro duce an

overall linear resp onse for the full range of input signals The design of the

BGO ADCs uses an accurate bit ADC with a s conversion time to

Toavoid underows the function E should b e set to zero ab ove GeV

c

Name coined by R Sumner formerly of Princeton University Further designs of the

FloatingPointUnitwere invented byP Denes Princeton University

Calorimetry

cover bits of dynamic range with dierent linear amplications A

passive split of the signal after the preamp separates the lower three and

higher three signal gains as the highenergy and lowenergy channels resp ec

tively When the input signal for a particular amplication approaches the

maximum voltage of the bit ADC the next lower amplication is used for

digitization The energy equivalence of the transition between gains within

the oatingp oint ADC has a spread which dep ends on the gain calibrations

osets p edestals and energy calibrations The distribution of transition en

ergies is plotted in Figure

2000 1500 1000 500 0 BGO Channels/Bin -1 2 10 1 10 10

Floating-Point ADC Transition Energy (GeV)

Fig The BGO FloatingPoint ADC

The distribution of transition energies for all the BGO ADCs The

three p eaks on the left corresp ond to the lowenergy channel The three

p eaks on the right corresp ond to the highenergy channel with the sixth

p eak indicating the maximum energy a single crystal can contain with

out saturating the ADC The maximum energies are distributed around

GeV

A metho d of relative gain and oset calibration of the oatingp oint ADC

was incorp orated as a sp ecial readout mo de of the electronics known as

bump mo de In bump mo de the signal on the samplehold is rst digitized

on the highest gain signal not saturating the ADC and then is digitized

a second time on the next lower signal amplication The dro op on the

The dierent signal amplications are approximately and The

dynamic range of bits is computed by summing the bits from the ADC plus the

bits of maximal gain change The digitization error is b elow even down to MeV

Tracking and Calorimetry

samplehold is negligible so the two readings provide a direct comparison

between two dierent signal gains as seen in Figure

4000 3000 2000 1000 0 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2 First and Second ADC Reading

Energy Computed from First ADC Reading (GeV)

Fig Bump Mo de Data

For each ADC reading on the optimal gain a second reading of the same

signal is taken on the next lower gain Data taken with a wide range

of signal inputs allows for the relative gain and oset calibration of two

successiveinternal gains of the oatingp oint ADC

To calibrate the BGO readout was put into bump mo de during three

LEP lls of Z running in The combination of hadronic Z decays

and Bhabha data p opulated the full range of signal inputs The remeasured

gains and osets were compared with the test set measurements which

are still currently in use see Tables and

Side G G G G G

RB Mean

RMS

RB Mean

RMS

Tab Bump Mo de Gain ReCalibration

The percentage change in the relative gains between the test set

measurements and the Z bump mo de data is less than for all

gains except G The increase of the BGO integration gate from sto

s at the b eginning of is b elieved to b e the cause of this change

Calorimetry

Side O O O O

RB Mean ADC

RMS ADC

RB Mean ADC

RMS ADC

Tab Bump Mo de Oset ReCalibration

The change in osets from to is less than ADC count

Energy Resolution and Linearity Measurements

The resolution functions derived in Section neglected the eect of elec

tronic noise calibration errors and p ossible nonlinearities in the energy mea

surement The correction for electronic noise and energy linearity can b e de

rived from the observed width and lo cation of the mass p eaks of the and

resonances measured in their two photon decaymode The mass distribution

for two photon combinations in hadronic decays of the Z taken in is

shown in Figure

60000

m MeV

MeV

50000

40000

Combinations

m MeV 30000

γγ

MeV

20000

10000

0 0 0.2 0.4 0.6 0.8 1

mγγ (GeV)

Fig BGO Energy Linearity Measured with and  Resonances

The dierence in the width of the mass p eak in data and Monte Carlo

simulation is used as a measurement of the electronic noise contribution

to the energy resolution The photon energies in the data have

b een rescaled by a factor in order to repro duce the mass peak

lo cations for the and  determined in the Monte Carlo simulation

Tracking and Calorimetry

The calibration errors and an additional linearity measurement can b e de

termined from the observed width and lo cation of the GeV and GeV

electron p eaks from Bhabha scattering measured in data taken in The

Bhabha p eaks for these two b eam energies are shown in Figure

80

E GeV

70 BEAM

E GeV

e

60

GeV E

50

E GeV

40 BEAM

E GeV e

30

GeV E

20

Number of Electrons/bin

R 10

0 30 40 50 60 70 80 90 100

Measured Bhabha Electron Energy (GeV)

Fig BGO Energy Linearity Measured with Bhabha Scattering

The BGO energy calibration is adjusted every datataking p erio d to

agree with the GeV Bhabha peak No further adjustment was

needed to obtain less than energy nonlinearityfor the GeV

highenergy Bhabhas The width of the Bhabha p eak is a measurement

of the calibration errors

The overall energy resolution function is mo died by the electronic

noise and calibration error terms

Full Full

E E N N E

correlated calibration

E E intrinsic

with MeV MeV and in

intrinsic correlated calibration

datataking A metho d for reducing the amount of correlated noise which

has b een applied on all data taken since is describ ed in App endix B

C Tully L Note The BGO calibration is maintained with several

The width of the Bhabha p eak is slightly more narrow The data provides

acheck of the energy linearityover a wide range of energies within the same calibration

period The measured Bhabha p eaks in Figure have b een corrected for dead crystals

and ret with an electromagnetic shower shap e using metho ds develop ed by IKominis and INemenman L Note

Calorimetry

monitoring systems A unique in situ calibration system based on an

RFQ proton accelerator and a lithium target has provided accurate recali

bration of the detector for several years

Fig Readout Thresholds

number of crystals read

10 The

out as a function of energy in

the central array of the

te Carlo

8 Mon

photon shower is a measure

R

the energy thresholds Be

6 of

I

lowMeVtheaverage num

Data

of crystals readout drops

4 ber

b elow This is function

lowest energy shower

2 ally the

which can reliably be identi ed as a photon Average Number of Crystals Above Threshold 0 0 0.4 0.8 1.2 1.6 2

Photon Energy (GeV)

The value of N is the numb er of crystals ab ove threshold in a array

centered on the electromagnetic shower As the readout thresholds are set

on a daily basis to keep up with external changes in the noise or ground

conditions within the L detector the static MeV thresholds set in the

Monte Carlo simulation are not a p erfect description for computing N A

comparison of N for data and Monte Carlo for selected photons is

shown in Figure The discrepancy in these distributions aects the

accuracy of the energy resolution function

Tracking and Calorimetry

BARYON PRODUCTION MEASUREMENTS

Secondary Vertices

Particle decays characterized by the presence of secondary vertices stand out

among a background of longlived particle tracks as seen in Figure

e

p

e

e

K

e

K

K

Fig Evidence for the Baryon

The baryon predicted from the SU avor mo del was found in

K b eam bubble chamb er exp eriments at Bro okhaven in

This eventwas identied during scanning by NP Samios Although the nonp ointing

and high transverse momentum were the initial signatures for the the two

converted photons from the decayunambiguously identied the decay

Baryon Pro duction Measurements

Kinematic Constraints

The application of external information to mo dify the direct measurements

made by a detector or to p erform hyp othesis testing is in general referred

to as kinematic constrained tting The decay in Figure contains

three secondary vertices constructed from two charged tracks namely the

two converted s and the The dimensional op ening angle b etween the

two s can b e determined by requiring them to originate from the same p oint

and to form the mass of a A similar assumption can be made for the

measurement The numerical technique for constrained tting is somewhat

involved but is included in App endix C for reference

Measurement of the Baryon

The decay prop erties of the baryon have already b een determined by

previous exp eriments The decay mo de p with a branching

ratio of can b e identied by combining measurements from the tracking

and calorimetry

+

Σ p πο

Fig Decay Kinematics

baryon decays at The p

Momentum

the p oint v

s Direction γ 1

γ 2 vs Primary

Vertex

The signature of a p decay is a single charged track and two pho

tons measured in the calorimeter If the decay p oint of the were known

the two photons would reconstruct to the mass of the within the error of

the measurements Similarly at this decay p oint the total momentum of the

would be equal to the sum of the proton and momenta These two

pieces of kinematic information in addition to the assumption that the

Measurementofthe Baryon

is pro duced at the primary vertex can b e expressed as follows

d v p v p v p v

s p s s s

v m m

s

The computed probability for candidates to satisfy these constraints is

plotted in Figure The atness of the signal distribution indicates accu

rate error estimation has b een made for the measurements

10 3

10 2

10 Candidates + Σ 1

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

P probability

sv tx

Fig Computed Probability for p Decay Kinematics

The agreement in data and Monte Carlo simulation is shown with the

p oints and op en histogram resp ectively The solid histogram is the dis

tribution for true decays based on Monte Carlo generator information

The inclusive pro duction rate measurement of baryons is based on a

selection of hadronic Z decays which have a measured primary vertex The

hadronic selection is similar to that used for electroweak lineshap e measure

ments and is based primarily on the observation of a wellbalanced high

measured by particlemultiplicityevent with nearly the full collision energy

the calorimeters

Hadronic Event Selection

p

E s

p erp endicular

p

s jE j

longitudinal

N

clusters

p

s E

total

The vector d is the direction of ight of the at the time of decay It is computed

assuming a curved tra jectory originating at the primary vertex

Baryon Pro duction Measurements

The primary vertex as describ ed in Section is constructed from the

measured charged tracks in the event The knowledge of the primary vertex

in all three dimensions is imp ortanttothe constrained t calculations

D Primary Vertex Requirements

Includes tracks with SMD hits

Kalman ltering p erformed on tracks

At least tracks remaining in t

The selection criteria for p can be separated into proton selec

tion photon selection and kinematic selection sp ecic to the

The proton needs to have go o d or at least wellestimated transverse and

longitudinal momentum measurements To preferentially select protons from

longlived decays the probability of the proton to b elong to the primary

vertex P is required to b e small

pvtx

Proton Track Selection

SPAN wires

TEC

SMD measured tan and z

jp j GeV

p

P

pvtx

Not tagged as or K track

s

Photons are identied by the prop erties of their electromagnetic shower

in the BGO barrel calorimeter Most of the electromagnetic selection is

p erformed by an energydep endent cut on a single neutral network output

ei L Note Electron rejection is done by eliminating F YJ P

NN

showers which matchwithacharged track tra jectory

Bump Selection

N

crystals

jcos j

E MeV E is an approximation to E

CORR CORR

The energydep endent cut on F was develop ed byHoward Stone

NN

The pattern of energy dep osition of a photon in the electromagnetic calorimeter has

a lo cal maximum or bump as shown in Section

Measurementofthe Baryon

for E GeV

CORR

F E

NN CORR

for E GeV

CORR

F

NN

if j j

TEC BGO

BGO

then j j

TEC BGO BGO

2 300 Σ+ → p π0

250 L3 data Fit to the data 200 Counts per 3.75 MeV/c

150

100

50

1.05 1.1 1.15 1.2 1.25 1.3 1.35

p π0 invariant mass (GeV/c2)

Fig The Mass Distribution of Candidates

The measured mass distribution has been t with a threshold function

P x P x P x

b

b b

with x x x in addition e P x P x P x

b thr eshol d b

b b

to a Gaussian function describing the signal The op en histogram is

from a Monte Carlo simulation and the solid histogram is the amountof

signal according to the Monte Carlo generator information

The nal kinematics of the p decay is restricted to reduce the

amount of combinatorial bac kground in the signal region of the mass distri

bution In addition to a minimum constraint probability P plotted in svtx

Baryon Pro duction Measurements

Figure the eectiveness of the kinematic constraint is strengthened by

two factors a minimum b o ost and a low probability P that the de

psvtx

cayvertex is equal to the primary vertex The decayframe angles the total

momentum and the transverse decay radius of the are also restricted

Selection

P

svtx

P

psvtx

cos and jp j GeV

r mm r is limited by the SMD inner radius

min max

The determination of the acceptance and eciency for measuring the

for this selection was computed based on a set of realistic Monte Carlo

simulation The mass distribution is shown in Figure

Measurement of the Baryon

The decays electromagnetically to nearly of the time The

can therefore be assumed to decay at the primary vertex Identication of

the is done in the p decay mo de

Σ 0 Λ0 γ

Fig Decay Kinematics

decays at the pri The γ p

Momentum

vertex and the

mary Direction

deca ys at the p oint v s π vs

Primary

Vertex

The kinematic constraints of the p decay are summa

rized by the following equations

d v p v p v

s p s s

Measurementofthe Baryon

m v m

p s

The hadronic event selection and the requirements on the primary ver

tex are the same as that for the baryon measurement as describ ed in

Section To select decays into p requirements are made on the

tracking measurements

Proton and Track Selection

SPAN wires

TEC

jp j GeV

transverse

either the proton or must have

SMD measured tan and z

2 2250 Λ0 → π- 2000 p

1750 L3 data 1500 Counts per 2.5 MeV/c

1250 Fit to the data

1000

750

500

250

1.05 1.075 1.1 1.125 1.15 1.175 1.2 1.225 1.25 1.275 1.3

p π- invariant mass (GeV/c2)

Fig The Mass Distribution of Candidates

Baryon Pro duction Measurements

The kinematics of the decay are summarized into three quantities

P P and P The rst variable is the probability that the de

pvtx zvtx lvtx

cays at the primary vertex The logarithm of the probability is plotted in

Figure The second variable is the probability that the momentumight

kinematics are satised The last variable is the combined probability of the

momentumight kinematics and the mass constraint

Selection

P

pvtx

P

zvtx

P

lvtx

Fig Primary Vertex

225

Probability

200

The track primary ver

probability after a

175 tex

cut of 150 preselection

Candidates

is a falling distribution 0 125

Λ

towards small probabili

100

ties The distribution

wn with the solid his 75 sho

50 togram b ecause of its long

ylength do es not fall

25 deca

o as rapidly

-30 -25 -20 -15 -10 -5 0

log P

pv tx

The distribution of selected candidates without the P prob

lvtx

ability cut is plotted in Figure

The nal kinematic requirements for the decay sp ecify the range of

the photon energy and the range of decayframe angles for the

Selection

MeV E MeV

CORR

cos

The dierence b etween the mass and the mass is plotted in Figure

The twotrackDvertex is also part of the constraint

Pro duction Rates 2 350 L3 300 L3 data 250 Fit to the data

Counts per 5 MeV/c 200

150

100

50

0 0.05 0.1 0.15 0.2 0.25 0.3

M(Λ0γ) - M(Λ0) [ GeV/c2 ]

Fig The Mass Dierence Distribution of Candidates

The photon selection used for Figure is the same as for the

analysis It is p ossible however to increase the purity of the photon selection

by making use of the high photon detection eciency of the BGO calorim

eter There are on average photons per event coming from prompt

pro duction Removing photons found in the p eak reduces the combinato

rial photon background for other decays The increase in photon purity for

selecting decays is shown in Figure This metho d also improves

the signal purity of the photon selection as shown in Figure

Pro duction Rates

The identication of and baryons in Z decay data is based on the

characteristic Gaussiandistributed signal shap e present in the p and

mass distributions resp ectively The extraction of pro duction rate measure

ments requires some way to count the number of baryons found in these

distributions and then to relate this count to the total number of baryons

which were pro duced including those whic h escap ed detection

The energy and measurement width of the photon p eak is rep orted in Section

Baryon Pro duction Measurements

10000

9000

Full

8000

Combinations

Fig Photon Rejection

γγ 7000

The p eak from Fig

6000

ure is more clearly

when the photons

5000 seen

Reduced

from the p eak are elim

4000

inated from the combina

3000 torics

2000

1000

0 0 0.2 0.4 0.6 0.8 1

mγγ (GeV) 2

160 L3

140 L3 data

Photon Rejection

120 Fit to the data Fig

The amount of back

Counts per 5 MeV/c

underneath the

100 ground

photon p eak is re

80

duced when photons se

from the p eak

60 lected

are removed 40

20

0 0.05 0.1 0.15 0.2 0.25 0.3 M(Λ0γ) - M(Λ0) [ GeV/c2 ]

Pro duction Rates

The calculation of the detection eciency and acceptance is based on a

set of realistic JETSET Monte CarloMC simulation for the L detec

tor The simulated events are hadronic decays of the Z and the total MC

statistics is

MC Statistics Events

For quick reference the exact numb ers and calculations are stated in centered

text in the following sections

Rate Calculation

pro Of the Monte Carlo events the p ercentage which have a or a

duced in the Z decay is computed from

Number of MC Pro duced

To determine the number of decays which are present in the Gaussian

signal p eak the signal distribution without background included can b e t

directly in the Monte Carlo This avoids the additional statistical error of

the background distribution With a xed value for the mass of the used

in the t

m GeV Particle Data Group

the number of MC in the nal p mass distribution is roughly

The t result is

Number of in MC Signal Distribution

However b ecause of dierences b etween the MC and data the normalization

of the p candidate distribution when comparing MC and data do es not

agree with the statistical normalization The numb er of selected hadronic Z

decays from and datataking is

Numb er of Selected Hadronic Events in Data Events

The statistical normalization is therefore

Statistical Normalization

The normalization of the p candidate distribution can be determined by

calculating the total area in the sidebands next to the p eak and using

that to normalize This pro cedure yields

Sideband Normalization

Therefore there is a correction factor to the MC numb er of measured events

This corresp onds to the p erio ds of datataking called b c d a and b

Baryon Pro duction Measurements

which changes the eciency

Sideband Normalization

Statistical Normalization

The detection eciency for all pro duced baryons is as seen

The numb er of measured in data with the xed value of m listed ab ove

is determined by a combined t with a threshold function given in Table

and a Gaussian distribution The number determined from the t is

n

Correcting this measurement with the ab ove determined eciency correction

gives the pro duction rate under the assumption of the shap e of JETSET

pro duction distributions The average number of and pro duced per

hadronic Z decay is found to b e

E D

JETSET

N

xed m

stat

e

The contribution from the statisticalstat error is signicantly larger than

the uncertainty in the eciencye calculation under the JETSET mo del

assumption The kinematic extrap olation based on other mo dels and the

systematic errors in the pro duction rate measurement will b e discussed later

in this section

Rate Calculation

The percentage of and pro duced per event in the set of million

Monte Carlo simulated hadronic decays of the Z is computed from

Number of MC Pro duced

To determine the numberofsignalevents b oth the mass and mass resolution

The contribution to the rate measurement error from hadronic event selection is safely less than and can b e neglected

Pro duction Rates

of the are xed to the values

m m GeV Particle Data Group and

GeV Determined from MC

m m

The signal shap e for the photon is describ ed by a Gaussian distribution

The photon resolution is determined primarily by the BGO calorimeter and

the op ening angle measurement between the photon and not the non

Gaussian mass distribution of the The number of MC in the nal

distribution is roughly The t result is

Number of in MC Signal Distribution

The dierence b etween the sideband histogram normalization for the

distribution and the statistical normalization app ears to b e small However

the candidate distribution has a large deviation in sideband to statistical

normalization discussed b elow Therefore the relatively small discrepancy

in normalization in the nal distribution is due to an internal cancella

tion The statistical normalization is

Statistical Normalization

The correction factor is therefore

Sideband Normalization

Statistical Normalization

The detection eciency for all pro duced baryons is as seen

The number of measured in data with the xed value of m and

listed ab ove is determined byacombined t with a threshold function given

in Tableand a Gaussian distribution The number of baryons is

n

The pro duction rate is computed to be

E D

JETSET

N

xed m and

stat

e

From Figure it app ears that there is an excess of baryons measured in data

However after mass selection the number of candidates in data and MC with sideband

normalization agrees to within The signal distribution is a doubleGaussian and

the fraction of signal in the wider Gaussian is larger in MC However this larger resolution

is taken into account in the measurement errors and hence the mass probability selection

Baryon Pro duction Measurements

In addition to the rate measurement the ratio of to pro duction

can be determined from the data The measurement of the ratio of rates

involves a smaller eciency correction and is therefore more accurate In

fact the eciency for selecting the photon once the asso ciated has

already been found is roughly This is to be compared with an overall

eciency for selection

The sideband normalization for the candidate distribution signicantly

diers from the statistical normalization The source of this discrepancy was

found to be the track D vertex probability which is at in data but is

The correction factor is the ratio of the and sideband slop ed in MC

normalizations as seen

Sideband Normalization

Sideband Normalization

The rate measurements were not found to be aected within statistics by

the discrepancy in the vertex probability after the correction technique

is applied

The detection eciency for selecting the photon is

where the eciency is computed based on the number of found in the MC

signal distribution rep orted ab ove and the fraction of baryons coming

from decay namely

Number of from in Selected Distribution

The Monte Carlo is used to determine the purity of the selection The

purity after mass selection was found to b e

Purity of Selection Determined from MC

The ratio of the and pro duction rates is measured by taking the

number of measured in data correcting with the photon eciency and

then normalizing to the number of baryons found in the data

Number of Selected Baryons in Data

The thetarecovery technique using BGO bump information do es not agree b etween

MC and data in v of REL This can aect the theta determination for tracks without

SMD measurements

The kinematic constraint requiring the to come from the primary vertex reduces

 

the numb er of measured baryons coming from and decay Hence the

baryons used in the measurement are referred to as prompt

Pro duction Rates

This calculation results in the following measurement of the ratio of to

prompt pro duction in hadronic Z decays

D E

JETSET

N

xed m and

D E

JETSET

prompt

N

stat

e

Kinematic Extrap olation

If the entire kinematic range of the baryon pro duction sp ectra were mea

surable by the detector then there would be no need to rely in detail on

the baryon kinematics predicted by the JETSET Monte Carlo simulation

However since certain kinematic regions were excluded in the analysis the

prediction of the number of baryons in these regions is crucial

The metho d used for determining the uncertainty in the measured fraction

of baryons is to identify the principal kinematic restrictions on the baryon

selection and then to compute for several Monte Carlo mo dels the spread

in the fraction of baryons predicted inside of these regions

Kinematic Restrictions on the

cos and jp j GeV

r mm r is limited by the SMD inner radius

min max

The consequence of the r and r restrictions is to bias the accep

min max

tance towards a particular range of total momenta

Kinematic Restrictions on the

MeV E MeV

CORR

cos

Kinematic Restrictions

pion jp j GeV for the proton and

transverse

r is limited by the P requirement

min pvtx

r is limited by the SMD inner radius max

Baryon Pro duction Measurements

The fraction of baryons predicted to be inside the measured kinematic

regions was computed for several Monte Carlo mo dels as summarized in

Table The maximum spread in these values is an estimate of the extrap

olation error

E E E D D D

obs obs obs

 

f f f N N N Monte Carlo

 

 

ARIADNE

JETSET

HERWIG

COJETS

Maximum Spread

Tab Estimation of Kinematic Extrap olation Error

The maximum spread in the predicted ratio of to pro duction is

Systematic Errors

The systematic error of the pro duction rate measurements is a combination

of several sources of uncertainty The eciency calculation error from MC

statistics was estimated in the and rate calculation sections The

kinematic extrap olation error was estimated in the previous section What

remains is the accuracy of the MC eciency calculation in terms of mo deling

the detector p erformance and also the particle multiplicity and kinematics

of hadronic decays of the Z

For the most part the level of disagreement in the shap e of MC and data

distributions is within the range of the statistical errors An exception is in

the track D vertex probability calculation for baryons The need for

sideband normalization is due to a discrepancy in the tracking eciencies for

the category of tracks used in this analysis There is also some eect from

the diering size and p osition of the primary vertex in MC and data

These discrepancies have b een studied and they aect mainly the overall

normalization in the candidate distributions as observed In the case of the

constraint on the t makes a change in the the removal of the xed m

rate measurement namely

E D

JETSET

N

m not xed

stat e

Pro duction Rates

The change is less than but indicates a systematic t uncertainty The

total systematic error on the rate measurement is the sum in quadrature

of three contributions

syst

D E

syst

MC

e t

N

In the case of the a second purity of selection was p ossible by means

of the photon rejection technique The pro duction rate was measured

with a higher signal to background ratio and found to b e

D E

JETSET

N

photon rejection

stat

e

The dierence in this rate with the measurement made with a lower purity

selection corresp onds to a p ossible systematic backgroundresolution

uncertainty The total systematic error on the measurement is

syst

D E

syst

MC

e

backres

N

For the measurement of the ratio of to prompt pro duction the two

measurements of the pro duction rate are used to estimate the systematic

error in the background contribution This ratio with a higher purityis

D E

JETSET

N

photon rejection

D E

JETSET

prompt

N

stat

e

syst

The total systematic error denoted on the ratio of to prompt

pro duction is

syst

syst

MC

e

backres

Included in this estimation is the systematic uncertaintyinthe selection and purity

Baryon Pro duction Measurements

Comparison with Other LEP Measurements

The and pro duction rate measurements can be compared directly to

those made by the other LEP exp eriments There is one other measurement

of the and that was p erformed by the OPAL Exp eriment

Production from this analysis

Data Statistics Million Hadronic Z Decays

m GeV

GeV

m

D E

N

stat syst

To be compared with the OPAL measurement

Data Statistics Million Hadronic Z Decays

GeV m

GeV

m

D E

N

stat syst

The technique of detecting the in the OPAL detector diers greatly from

that of the L Exp eriment This dierence is clearly seen in the shap e of

their mass sp ectrum as shown in Figure

400 2 300 Σ+ → pπ0 Monte Carlo

200

OPAL Distribution 300 Fig

100

The mass distribution of p

measured by the 0 candidates

1.2 1.4

AL detector has a char 200 OP

Counts per 10 MeV/c

acteristically dierent shap e

from that measured with the

100 L detector as shown in Fig

OPAL data ure Fit to the data

0 1.1 1.15 1.2 1.25 1.3 1.35 1.4 1.45 1.5 p π0 invariant mass (GeV/c2)

Comparison with Other LEP Measurements

Fig DELPHI Distribution

The photon is measured in the DELPHI detector by rst having it

convert through pair pro duction The momenta of the charged particles

are then measured with their tracking detector

Both OPAL and DELPHI have made rate measurements These de

tectors rely on b eam pip e and tracking material to convert the photon

into an e e pair The momenta of these particles are then measured with

tracking detectors and combined to determine the photon energy

Production from this analysis

Data Statistics Million Hadronic Z Decays

m m GeV

GeV

m m

D E

N

stat syst

To be compared with the OPAL measurement

Data Statistics Million Hadronic Z Decays

m m GeV

GeV

m m

E D

N

stat syst

Baryon Pro duction Measurements

And the DELPHI measurement

Data Statistics Million Hadronic Z Decays

m m GeV

GeV

m m

E D

N

stat syst

The pro duction rate measurement agrees with that measured by

OPAL However the measurement from this analysis is larger than the

DELPHI and OPAL measurements by more than the statistical error The

BGO detector makes it p ossible to measure photons down to lower ener

gies than can be measured by other detectors Thus the discrepancy in the

rate measurements could be due to the kinematic extrap olation term in the

systematic error

P olarization

Quarks coming from Z decay are highly p olarized Antiquarks are p olarized

by the same amount but in the opp osite direction The p ercentage of p olar

ization dep ends on the electroweak interaction as expressed in equation

These evaluate to

u c

P P

q q

d s b

for the dierent quark avors listed

Heavy baryons formed from primary quarks are predicted to retain this

p olarization while lighter baryons are not However lightbaryons pro

duced in heavy baryon decay such as the may inherit some of this

baryons and p olarization Therefore a longitudinal p olarization in

the opp osite p olarization for would indicate b oth that heavy baryons

are p olarized and that a fraction of which decay into the

antibaryon decay As describ ed in Section the baryon and the

via the parityviolating chargedcurrent interaction Therefore if there were

The parameter for twobody decays of heavy baryons is predicted to be near

unity This would cause light baryons pro duced in heavy baryon decay to have a longitudinal p olarization

Polarization

a longitudinal p olarization of the it would be present in the p decay

angular distribution In fact the value of determining the co ecient of

the cos dep endent part of the dierential crosssection is maximal for the

p

as shown in Table

The dierence in the and rates for equal values of the decay

frame angle of the proton and antiproton resp ectively is a way to lo ok for

p olarization This is expressed in the quantity

n n

A

n n

where is the fraction of and signal presentineach bin of cos The

error on is a binomial error

s

n

signal

n n

signal total

is computed in bins of cos and plotted in Figure The value of A )

* 2

θ 0.9166 / 4 1.5 P -0.2247 0.2996 /d(cos

+ 1 Σ

dA 0.5 0 -0.5 -1 -1.5 -2 -1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4

cosθ* of the proton with respect to the Σ+ flight direction

Fig Longitudinal Polarization Measurement in Decays

No statistically signicant p olarization is observed in baryons pro

duced in Z decay The value is taken from the t of Figure divided

by as the proton and not the ight direction is b eing measured The

result obtained is

P

Baryon Pro duction Measurements

This measurement has not b een p erformed by the other LEP exp eriments

It is a p otentially interesting way to infer the p olarization of charm baryons

pro duced from Z decay esp ecially if the from charm sample could be

enhanced in some way

Summary and Outlo ok

The pro duction rates of two baryons the and have been measured

in hadronic Z decays using the L detector at LEP These baryons come

from the same isospin multiplet and therefore are predicted to be pro duced

at nearly equal rate The ratio of the and rates and the corresp onding

estimates for the statistical and systematic errors were measured to be

D E

N

D E

Measured

stat syst

N

while the predicted value of this ratio is

D E

N

E D

Predicted

N

The measurement and prediction are in agreement A summary of several

baryon and meson pro duction measurements taken at three dierent e e

accelerators is plotted in Figure Included in this gure are the two

measurements made by this analysis

A large fraction of and baryons come from heavier baryon decays

or contain a primary quark from Z q q decay and resp ec

tively Deviations from the trend set by the pro duction rate curve of

Figure could indicate unaccounted for heavy baryon decays In partic

ular both the and pro duction rates are greater than one standard

deviation ab ove the predicted rate One p ossible explanation is that this

excess comes from cbaryons whose decays are not yet wellcatalogued

The ratio of to prompt pro duction was also measured in this anal

ysis The and baryons have the same quark content and yet their

rates are predicted to be dierent This is due to the mass dierence of the

and measured to be m m GeV and to the

Summary and Outlo ok

√s=91 GeV √s=29-35 GeV √s=10 GeV 1 Fit (2J+1)) s N s γ /( B C

> -1 10 primary N <

-2 10 + 0 Σ , Σ Measurements

-1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.8 1

Ebind(GeV)

Fig Pro duction Rate Measurements As a function of the hadron

binding energy describ ed in Section baryon and meson pro duction

rates excluding primary quark contributions and feeddown from other

hadron decays lie on a single curve for dierentcenterofmass energies

The and measurements from this analysis are included with the

p

s GeV data

diering amount of feeddown contribution from other baryon decays The

measurement of to prompt pro duction found to b e

E D

N

E D

Measured

stat syst

prompt

N

can be used to infer the temp erature T in equation

For T GeV trillion degrees centigrade the predicted value

for this ratio is

D E

N

E D

Predicted

prompt

N

T GeV

Baryon Pro duction Measurements

The prediction is lower than the value measured ab ove This indicates that

the mass dep endence of baryon pro duction is not as strong and implies

a corresp ondingly higher value for T As can be seen in Figure the

nal determination of T requires a combined t of all baryon and meson

pro duction rate data from many exp eriments and collision energies

The hadronization temp erature if indeed that is what the parameter

T describ es is p otentially an imp ortant physical quantity The impact of

baryon pro duction measurements in Z decay might one day inuence the

description of the fundamental interaction resp onsible for quark connement

in addition to applications outside of collider exp eriments

From PJE Peebles Principles of Physical Cosmology page

In the standard mo del the universe at redshifts z has

to expand in a nearly homogeneous way with few of the com

plications that characterize recent ep o chs There are departures

from near thermal equilibrium at the ep o ch of pro duction of light

elements at the earlier phase transitions of the particle physics

that pro duced ordinary baryonic matter out of quarks separated

the electric and weak interactions and mayb e adjusted the lo

cal value of the entropy per baryon and p erhaps still earlier at

the phase transitions that pro duced cosmic strings or textures or

nonbaryonic dark matter We have relicts in the light elements

it would b e exceedingly interesting to nd others

A BGO RESOLUTION FUNCTIONS

This app endix presents the resolution functions for electromagnetic showers

measured in b oth the barrel and endcap regions of the BGO calorimeter

Energy Resolution Functions

Barrel

Gaussian

p

A E E

E

E

E

Full

p

A E E exp

E

E

Endcap

Gaussian

p

E E A

E

E

E

Full

p

A E E exp

E

E

Modication for Electronic Noise and Calibration Errors

Full Full

E E N N E A

correlated calibration

E E intrinsic

with MeV MeV and in

intrinsic correlated calibration

datataking The value of N is the number of crystals ab ove threshold in a

array centered on the electromagnetic shower

Resolution Functions

Barrel

mrad

B

p

mrad A E

E E E

c

Below MeV the tailing eect in the endcap energy measurement b ecomes extreme

Photons in the tail are lost

A BGO Resolution Functions

E

h i

E E E GeV

c

E E

exp

E

Endcap

j tan j

E B

E E mrad A

j tan j

ref

with tan mm mm taken to be the intersection of the barrel

ref

and endcap volumes

Resolution Functions

Barrel

sin

B B

A E E

sin

Endcap

j cos j

E B

E E mrad A

j cos j

ref

with tan mm mm taken to be the intersection of the barrel

ref

and endcap volumes

The resolution functions were determined assuming the smearing of the primary

vertex p osition is removed as would b e the case if the D primary vertex were used In

addition the correction to for a nonzero vertex p osition must b e applied

B BGO NOISE DECORRELATION ALGORITHM

The presence of correlated noise in the BGO analog electronics has a pro

nounced eect on low energy measurements and shower shap e parameters

A metho d was develop ed to recompute eventbyevent for each correlated

region a new p edestal baseline This metho d is known as the BGO Noise De

Correlation Algorithm and can b e found in the ECL Reconstruction co de in

the routine ECCORNO This app endix rep orts on the principles and draw

backs of this technique as well as simulation results and noise calculations

that measure its p erformance

Intro duction

Many analyzes in L are based on measurements made by the BGO calo

rimeter Typically distributions of the number of BGO bumps ab ove some

energy cut the ratio of an energy estimate based on crystals to an estimate

based on crystals or an even more elab orate neural network analysis us

ing the measurementofevery crystal are useful handles for identifying event

top ologies and single particle showers Fundamental to all these techniques

is the basic knowledge of the working setthat is which crystals were read

out why they were readout and how useful is the information they contain

Noise plays an imp ortant part in determining this set as do es the general

organization of the BGO readout electronics

Corresp ondingly noise decorrelation mo dies the BGO w orking set The

noise decorrelation algorithm is nothing but a pattern recognition technique

for deciding whether particular channels of a correlated group reside within

the p edestal baseline and then subtracting the mean value of those channels

found in the baseline As is easily seen in the noise calculations presented

in this pap er what the noise decorrelation algorithm do es barring pattern

recognition failures is to guarantee that the correlated noise level in the

worst case is equal to the intrinsic noise of a single channel What is also

clear is that the most reliable way to reduce the noise down to this level is

B BGO Noise DeCorrelation Algorithm

to improve the grounding connections at the analog electronics and this was

achieved during the running p erio d giving the total average noise levels

for the whole detector the value of MeV

BGO Readout System

The BGO analog electronics or Princeton level boards are mounted in

aluminum b oxes lo cated at the end of the barrel hadron calorimeter There

are Lausanne b oxes on eachside The general layout of the readout b oards

within each box is displayed in Figure B A A A A A A A A A A A A AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA A A AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA AAAA

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AAAA AAAA

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AAAA AAAA

Barrel Aluminum AAAA AAAA AAAA AAAA AAAA ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú ú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú úú AAAA AAAA AAAA

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Boards

Fig B General Layout of BGO Readout Electronics within of the Lausanne

Boxes

As far as correlated noise is concerned the most imp ortant b oard is the

power distribution b oard Three separate p ower supplies eachproviding three

voltages are given a common ground connection on this b oard the socalled

box ground The box ground for each of the Lausanne boxes per side

is connected directly to a thick copp er braid mounted on the barrel hadron

calorimeter If the box ground is damaged the box will oat with an AC

ground level dierent from that of the copp er braid This is the rst source

of correlated noise

Each Princeton lev el b oard has complete BGO channels meaning

each channel has its own pro cessor and can be given separate readout

instructions In the barrel of the channel b oards have their pin

connectors cabled together forming one linear chain of pro cessors each of

which is communicated to one after the other the socalled BGO ring Each

ring is connected to one of the driverreceiver pin connectors The endcap

rings have of the channel b oards cabled together If each micropro cessor

did not have its own reading event buer then the length of the BGO

ring would imp ose a sp eed limitation in the BGO readout and subsequent

dead time for the whole detector

Historically in fact the BGO in bunch timing was never run in buered

mo de The reason for this is that buer transfersreading from each mi

cropro cessor and transferring digital data over the at cables through the

ould cause ground level driverreceiver to the level micropro cessors in Pw

shifts for the analog electronics while the BGO was liveintegrating the sig

nal of a new trigger Much analysis p erformed byPeter Denes of Princeton

was done to overcome the problem of mixed mo de readout b oardsthat is

the presence of digital and analog electronics on the same PCB The solution

comes from the completely synchronous op eration of the exp eriment In ad

dition the driverreceiver boards now have an optical isolation b etween the

direct micropro cessor reading and the driving of the signal to level which

is done on a separate power supply not connected to the box ground

Nevertheless mixedmo de is mixedmo de and digital activity will in

general cause ground level AC shifts within each ring This gives the nal

grouping of the correlated noise pattern For an overall summary there are

barrel rings and endcap rings in each Lausanne box Each level p ower

supply powers BGO rings The channel preamp b oards are group ed

from two channel level boards in separate rings powered by the same

supply The preamp shields are separately connected to the copp er braid

but the lowest imp edance ground for a given channel is still the ring ground

Sparsed Mo de

The BGO electromagnetic calorimeter consists of rings barrel and

endcap giving total channels In addition there are Lumi Rings

ALR Rings and EGAP Rings A threshold setting system called BASE

in combination with the micropro cessor co de was develop ed to reduced

the amountofreadings transferred from level to level of the BGO

In a BASE reading each level pro cessor sends triggers to the ring it

communicates with and histograms all the p edestal readings which are made

B BGO Noise DeCorrelation Algorithm

The level pro cessor then do es a running integration from the upp er edge

of the histogram until it nd of the numb er of triggers This ADC value

which can b e at maximum the full range of the highest gain part of the ADC

comparator is the sparsed threshold If the micropro cessor instruction

byte is set to sparsed mo de then in normal data taking if the ADC reading

is equal to or ab ove this value then the ADC value is transferred up to level

The lowest threshold value is therefore ADC readings from negative

p edestals are suppressed Some channels are chosen to b e read unsparsed

The unsparsed channels were used to monitor the functioning of the dig

ital connection to the ring Without unsparsed channels no readings from

a ring in a given event would be p ossible even though this could also o ccur

from a broken ring cable Through mid only one unsparsed channel

was given to each ring but with the advent of noise decorrelation there are

currently barrel unsparsed channels and endcap unsparsed channels

As an aside the sparsed thresholds may or may not corresp ond to a

particular number of BASE RMS ab ove the nominal p edestal that dep ends

on the exact p edestal sp ectrum The thresholds are recorded in the BGO ini

tialization vector which is attached to the end of events with hardware event

number By direct comparison the dierence between the threshold and

nominal p edestal for one particular BASE run corresp onds to a mean value

of times the RMS noise measurement as shown in Figure B Online

monitors constantly monitor the readout p ercentage of the BGO during data

taking This value is consistently

BGO Noise Levels

Intrinsic Noise

The ADC alone with no preamp connected has V of noise referenced

to input The Lyon preamp has a noise level of V which in quadra

ture with the ADC noise gives a total intrinsic noise of V per channel

this corresp onds to roughly MeV of signal Anomalously low noise levels

indicate that something is broken or disconnected In the case of Endcap

Ring or in ECCORNO convention Ring the pin carrying one of the

ADC timing signals was broken This had resulted in noise levels of V

which is even below the noise level for a functioning ADC Another source

of low noise readings comes from negative p edestals

Negative p edestals are a concern These channels have no noise measure

1200 Entries 10173 Mean 1.632 RMS .1002 UDFLW 1.000 1000 OVFLW 38.00

800

600

400

200

0

0 0.5 1 1.5 2 2.5 3 3.5 4

Fig B Distribution of Thresholds in Numb er of BASE RMS ab ovePedestal

ments The DC feedback of the low energy ADC channel to the preamp is

set so that the integration of a voltage over the timing gate is a p ositive

value The digitizing DAC only go es from V to V which is the same

dynamic range as the Lyon preamp However in a synchronous environment

negative spikes which come exactly at the same frequency as the LEP cross

ing time or in an integer multiple will integrate to a net negativevaluethe

equal and opp osite p ositive part b eing injected during nonintegration times

One unpleasant example of synchronous noise was the doubleheaded BGO

p edestals in a ratio of This came from the SMD switching p ower supplies

which ran at the LEP crossing time This noise source was eventually re

y Italian ingenuity and additional ground cables from the b ox ground moved b

to the copp er braid for boxes with preamp cables lo cated in the vicinity of

SMD power cables

B BGO Noise DeCorrelation Algorithm

Correlated Noise

If the noise in the calorimeter were dominated by intrinsic noise then the

probability that in sparsed readout mo de that n crystals in a ring are readout

would b e a monotonically decreasing function of n By direct measurement

as shown in Figure B there is a spike present at readout p ercentage

In fact a detailed lo ok at the time dep endence of the p edestal readings of

any two channels in a ring shows that their uctuations are nearly identical

for BASE measured RMS values ab ove MeV as in Figure B

Box Killing Statistics (Fill 2313) Box Killing Statistics (Monte Carlo) Entries 7184448 Entries 1151616 22500 900 20000 800 17500 700 15000 600 12500 500

10000 400

7500 300

5000 200

2500 100

0 0

0 0.2 0.4 0.6 0.8 1 0 0.2 0.4 0.6 0.8 1

Fig B BGO Ring Readout Fraction for Data Fill and Monte Carlo

Supp ose that after a ll of data were taken one were to go back and

correct the eventbyevent p edestal values for each channel in every ring

There would still b e the remaining problem of the readout thresholds Even

if the noise level were measured to be MeV from correlated noise in

stead of the MeV of intrinsic noise the eective threshold would not be

BASE for every event If there were a negative baseline MeV T

swing of MeV in a ring then the readout threshold for channels in that

ring would b e MeV T BASE Similarly for upward swings the eective

thresholds are reduced This kind of b ehavior is in general not mo deled by

shower shap e parameters that do not take into account the eventbyevent

thresholds for each crystal

Another imp ortant point ab out correlated noise is that since it is in

general coming from an external source its average eect on p edestals can

change b etween the time the BASE was taken and when data taking actually

b egins This is also a natural consequence of BEAM PICKUPBGOMARK

phase lo cking which only o ccurs once b eam is in the machine Therefore the

BGO InBeam Pedestals(MeV) vs. Time of Day in Box M RB26 BGO InBeam Pedestals(MeV) vs. Time of Day in Box M RB26

10 10

0 0 Events/sec 10 Events/sec 10 0 0 -10 -10 10 10 0 0 -10 -10 10 10 0 0 -10 -10 10 10 0 0 -10 -10 10 10 0 0 -10 -10 10 10

One Crystal Plotted Each for of the 6 Rings (MeV)

One Crystal Plotted Each for of the 6 Rings (MeV) 0 0 -10 -10 9.75 9.78 9.819.84 9.87 9.9 9.75 9.78 9.819.84 9.87 9.9

Time of Day (hours) 24/8/94 Time of Day (hours) 24/8/94

Fig B Example of TimeDep endent Pedestal Fluctuations for Two Sets of

Channels Lo cated in Each of the Rings in a Box Correlation of the

Horizontally Arranged Plots is the Ring Ground of the Vertical Plots

is the Box Ground and PairWise in the Vertical is the PowerPreamp

Ground The topmost plots are the number of events p er second

mean value of the p edestal for all p edestals in a ring may have a constant

shift This is exhibited by rings that have an abnormally high or low readout

frequency during a ll Fortunately a constant shift is corrected in the same

way as an eventbyevent shift

DeCorrelation Pattern Recognition Noise

The decorrelation of the p edestals in a ring is a misnomer In fact if one

computes based on the readings within a ring a new p edestal baseline then

the error on the calculated mean b ecomes the new level of correlated noise

When using a single unsparsed channel to restore the baseline the intrinsic

noise uctuations on that channel now b ecome common to all the channels

from which it was subtracted Therefore if the total noise levels for all

p

channels fell b elow MeV and only single channel subtraction were being

p erformed then the noise decorrelation routine would become the noise

correlation routine Calculations b elow show that even for data the

B BGO Noise DeCorrelation Algorithm

routine is estimated to still improve the average noise level in a x matrix

of crystals

Preparation The algorithm begins by computing the average RMS

noise levels p er ring of the crystals whichhave b een readout The RMS read

ing of a single crystal is sucient however care must b e taken to remove the

readings of crystals whose channels have b een marked as nonfunctioning A

minimum required RMS cut of V is the only means of remov

ing broken channels In the database nonfunctioning channels are given

a negative RMS Disconnected channels and negative p edestal channels are

also removed by this cut

Readout Percentage Breakup Based on Figure B the dieren t ap

proaches to decorrelation are split up Ab ove readout fraction enough

crystals are present to attempt Box Killing describ ed below If the un

sparsed channel is reading a voltage less than its nominal p edestal plus

BASE RMS then both the Lo cal Flatness Test of YFWang and the

Ring Readout Fraction Test are applied Ab ove this range only the

Ring Readout Fraction Test is applied

Lo cal Flatness Test of YFWang One approach for eliminating

the use of unsparsed channels whichhav ehadenergy dep osited within

the crystal is to lo ok at neighb oring channels even if the channels are

lo cated in a dierent ring in the same b ox A computation is made of

the RMS of the readings in the unsparsed channel and in neighb oring

channels and if this RMS is less than times the average ring RMS

and the mean value is less than times the average ring RMS ab ove

the nominal p edestal then the unsparsed channel under test is marked

as being in the p edestal baseline

Ring Readout Fraction Test Another approach is to make use of

the very low levels of intrinsic noise present in each channel approx

imately MeV First of all if the unsparsed channel reading is over

BASE RMS ab ove the nominal p edestal and the ring readout frac

tion is less than then the channel is considered to have energy in

it If in a window of MeV around the reading of the unsparsed

channel over of the fraction of channels readout are present then

the unsparsed channel under test is marked as being in the baseline

This window increases slightly with voltage but go es to a maximum of

MeV for MeV baseline shifts and ab ove

Box Killing In the case where over of a ring has been readout

then the same Ring Readout Fraction Test is p erformed but for

every crystal that has been readout A limit is then placed on the

minimum numb er of crystals that must to b e found in the baseline at

least and the RMS spread of the channels found in the baseline

as a function the computed baseline correction Figure B shows the

number of crystals used in Box Killing in data with a peak just

b elow crystals for the endcap and just below crystals for the

barrel Figure B shows the maximum allowed RMS spread curve

overlayed on top of data and Monte Carlo for Box Killing candidates

Data p oints ab ove this curve are considered to be energy dep ositions

and not noise What is imp ortant ab out this curve is that the slop e is

less than to avoid large lo calized energy dep ositions from mimicking

upward p edestal shifts The slop e of the curve for large p edestal shifts is

Entries 2746752 7000

6000

5000

4000

3000

2000

1000

0

0102030405060

Fig B Numb er of Crystals Used in Box Killing Algorithm for Data

B BGO Noise DeCorrelation Algorithm

Monte Carlo Simulated with Correlated Noise 1995 Data 500 500 V) V) μ μ 450 450

RMS ( 400 RMS ( 400

350 350

300 300

250 250

200 200

150 150

100 100

50 50

0 0 0 500 1000 1500 2000 2500 0 500 1000 1500 2000 2500

Pedestal Shift (μV) Pedestal Shift (μV)

Fig B RMS Spread for Box Killing Candidates in Data and Monte Carlo

Remarks

The Lo cal Flatness Test was tuned by the Multiphoton Group to

give the best p erformance for their signals In the absence of a noise

simulation in the Monte Carlo it was believed that this routine had

a low failure rate which is not the case as seen in Figure B Im

provement could p ossibly be made by restricting the computed RMS

to within the ring and then comparing it with something characteristic

of the intrinsic noise not the average ring RMS

The Ring Readout Fraction Test used to check that the fraction of

readings lying b elow the windowed baseline did not exceed the fraction

found in the baseline This was somehow lost

Box Killing do es not iterate to remove stray baseline estimators and

then to recheck the minimum numb er of estimators requirement b efore

recomputing an average baseline This was a mistake

The original purp ose of Box Killing was to remove large noise spikes

whichwere aecting the summed energy in the event hence the forceful

name When p ossible it is the most accurate means for computing

the p edestal

Results

In the case where all channels are read unsparsed the correlated noise can b e

very accurately removed as demonstrated in Figure B using the unsparsed

ll data However in normal sparsed data mo de the amount of correlated

noise removed is a function of how many channels were used to decorrelate

and for particular BGO bumps the distribution of bump crystals among

dierent rings

RMS Noise Levels for All BGO Channels

1800

1600

els 1400 DeCorrelated Noise Lev

1200

1000 Number of Channels/bin

800

BASE Noise Levels

600

400

200

0 123456

Energy (MeV)

Fig B Noise Levels After DeCorrelation Compared to BASE Noise Levels

A routine ECNOISE was written to do the explicit calculation of the total

noise present in a bump based on which crystals in an array of were

readout The distributions for and Data are presented separately in

Figure B The spikes in the decorrelated distributions corresp ond to how

many of the crystals of the bump were present in the same ring There is still

a tail of uncorrected p edestal baselines going ab ove MeV but the p eak of

p

MeV the the calculated noise sp ectrum for crystals is shown to be at

ideal uncorrelated case

B BGO Noise DeCorrelation Algorithm

1994 Data 1995 Data

Entries 55647 Entries 86573 Mean 5.208 10000 Mean 4.286 7000 RMS 3.651 RMS 2.373 UDFLW .0000E+00 UDFLW .0000E+00 OVFLW 142.0 OVFLW 34.00 6000 8000

5000

6000 4000

3000 4000

2000 2000 1000

0 0 0 2.5 5 7.5 10 12.5 15 17.5 20 22.5 25 0 2.5 5 7.5 10 12.5 15 17.5 20 22.5 25

Noise in Sum 9 (MeV) Noise in Sum 9 (MeV)

Fig B Calculated Noise in the Sum of Crystals for and Data

The detailed study of the decorrelation algorithm rst required accurate

noise simulation to be included in the Monte Carlo The routines to do

this were written based on the QE simulation parameters Previously

the Monte Carlo was simulated with MeV thresholds MeV of global

correlated noise and only added intrinsic noise to channels readings

The QE Monte Carlo is simulated with no noise and no thresholds

Then within the ECRWMC routine the digitization bank is expanded to

include unsparsed channels and then intrinsic and correlated noise is added

to all channels The event is then pro cessed by an exact replica of the

ECCORNO routine running within the Monte Carlo reconstruction routine

ECENMC The noise was added assuming only b ox ground correlations and

tuned to match roughly the observed data p erformance with the same reso

lution and eciency improvements on the sp ectrum Figure B shows a

comparison of QE with noise and threshold simulation with the ll

There will always b e some discrepancy with the Monte Carlo b ecause

it is dicult to mo del accurately the large nonGaussian p edestal swings

which o ccur in data see Figure B

In the sp ectrum is much improved as seen in Figure B

rescaled mass This resolution is to be compared with an ideal Monte

Carlo resolution of MeV no noise no thresholds and p erfect energy cali

bration and linearity However the large variation b etween the twoyears in

Monte Carlo π0 Mass Distribution with Noise π0 Mass Distribution (Fill 2313) Box Killed

Entries 43234 Entries 16631 1000 87.98 / 64 66.24 / 68 P1 .7854E+05 5438. 350 P1 0.1769E+05 2171. P2 .9992 .3034E-03 P2 1.003 0.1113E-02 P3 -7.441 .1423E-01 P3 -6.797 0.3196E-01 P4 -7.614 .6715E-02 P4 -7.062 0.1699E-01 300 800 P5 .1335 .2634E-03 P5 0.1300 0.4935E-03 P6 .6685E-02 .2757E-03 P6 0.6796E-02 0.4972E-03 P7 10.01 .3599 P7 3.363 0.2222 250 Mπ = 130.0 ± 0.5 MeV 600 M = 133.5 ± 0.3 MeV π 200 σ = 6.8 ± 0.5 MeV σ = 6.7 ± 0.3 MeV Nπ = 672 400 150

100 200 50

0 0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4

Mass (GeV) Mass (GeV)

Fig B Comparison of QE Monte Carlo with Noise and Fill

noise levels warrants statistical use of the database entries from b oth years

instead of hardwired values in the Monte Carlo noise simulation

The general eects of the noise decorrelation routine on low energy data

is to improve the ratio of the corrected sum of to the corrected sum of

towards higher values for isolated photons and to improve the accuracy of

the energy measurements In Table B the result of the routine on data

and QE Monte Carlo with and without noise is shown

Data Typ e Uncorrected DeCorrelated Box Killed

Unsparsed Fill

Data Fill

Data

Monte Carlo noise

Monte Carlo noise

Monte Carlo no noise

Tab B Mass Resolution Eciency Increase from Noise DeCorrelation

A detailed picture of the routines eect comes from plotting the energy

sp ectrum of subtracted channels As shown in Figure B the failure rate

of the routine from the Lo cal Flatness Test is fairly large where large

is ab out at MeV With decisions per event this rate means

B BGO Noise DeCorrelation Algorithm

700

600

± 500 Mπ = 134.9 0.2 MeV σ = 7.0 ± 0.1 MeV 400

300

200

100

0 0 0.1 0.15 0.2 0.25 0.3 0.35 0.4

Mγγ (GeV)

Fig B Mass Sp ectrum Compared to an Ideal Monte Carlo Resolution

of MeV

that once every events at most of the crystal readings have b een

overcorrected by MeV however this may have still b een b etter than

leaving a MeV correlated shift for example Clearly the main concern is

to keep the failure rate down and most imp ortantistomake sure the energy

sp ectrum of failed subtractions dies o quickly with energy

Both single crystal decorrelation tests die o at failure rates ab ove

MeV Box Killing is applied less frequently in Monte Carlo as shown

is that in roughly k nonoise Monte in Figure B A notable comparison

Carlo events corresp onding to million decorrelation decisions Box Killing

is run ab out times subtracting an average of MeV from a single ring In

data Box Killing o ccurs on average times p er event with energy sp ectra

going well into the tens of MeV in and hundreds of MeV in

As mentioned in the intro ductory remarks on correlated noise the eec

tive readout threshold for each crystal varies from eventtoevent However

with the information from the noise decorrelation routine the thresholds

can be estimated This technique has been implemented in the routine EC

THRES The distribution of thresholds for a sample of crystals in a

data ll is shown in Figure B

Lo cal Flatness Test

10 4

Box Killing

Readout Fraction Test

10 3 Ring

10 2 Failures in 2 Million Decisions

10

1

0 2 4 6 8 10 12 14 16 18 20

Subtracted Energy (MeV)

Fig B Subtracted Energy Sp ectrum for Noise DeCorrelation Pattern Recog

nition Failures

104

103

102

10

1

0 2 4 6 8 10 12 14 16 18 20

Readout Thresholds (MeV)

Fig B Readout Thresholds for Data Fill showing Unsparsed Channels

designated by Zero Threshold and the Software Cut for PP Bank Cre ation at MeV

B BGO Noise DeCorrelation Algorithm

Conclusions

Calculation and simulation techniques have b een develop ed for the BGO

Noise DeCorrelation Routine ECCORNO With these new to ols any po

tential faults or biases with the algorithm can be studied The calculated

noise contribution in the sum of crystals can go directly in an energy res

olution function such as ECEMRES and the threshold calculations from

ECTHRES can be used to make b etter sense out of shower shap e parame

ters The improvement on the readout p ercentage threshold mo deling and

give b etter agreement between data and Monte noise contributions should

Carlo comparisons on a wide variety of computed quantities The general

structure of the ECCORNO routine as well as a few comments are provided

for p otential future development and tuning of the algorithm

C CONSTRAINED FIT DETAILS

This app endix discusses the mathematical details of the constrained kine

matic t The tter was written by Scott S Snyder Excerpts of his thesis

are included here for reference

m

The problem to be solved is this given a set of measurements x and

m m

their error matrix G hx x i what is the smallest change one can

i j

ij

make to x to make them satisfy agiven set of constraints F x

i

m T m

x x Gx x sub ject to the That is minimize the quantity

constraints Fx The algorithm which is based on SQUAW kinematic

tting program is develop ed in this section

C Denitions

Divide the set of variables into wellmeasured and p o orly measured sets

Let x and y be column vectors of the wellmeasured and p o orlymeasured

variables resp ectively Whole vectors and matrices are denoted by b old

face symb ols and their elements by subscripted plain symbols Denote the

m m

measured values of the variables by x y the true values of the variables

t t

y x y their values after iteration by x y andtheirvalues at the end b

f f

of the t by x y The error matrices are given by

m m

G hx x i

i j

ij

C

m m

Y hy y i

i j

ij

m m m m t

where it is tacitly assumed that hx y i Here x x x

i j

The tting algorithm will be designed to reference only the arrays G

and Y not their inverses This p ermits one to sp ecify that a wellmeasured

variable is constant by setting the appropriate diagonal element in G to

The metho d of convergence testing was changed following the removal of cut steps

C Constrained Fit Details

zero One can also sp ecify that a p o orly measured variable is completely

unknown by setting the appropriate element in Y to zero

It is convenient to dene the displacementvectors

m

c x x

C

m

d y y

The constraints which must be satised are given by the row vector

Fx y F C

with gradients

F

B x y B

xi

xi

x

i

C

F

B x y B

y i

y i

y

i

A column vector of Lagrange multipliers will also b e needed

The quantitywhich should b e minimized sub ject to the constraints F

is

T T

c Gc d Yd C

C Fit

In order to minimize the sub ject to the constraints F use the metho d

of Lagrange multipliers and minimize the quantity

T T

M c Gc d Yd F C

At the minimum it must b e the case that

M

F C

M

Gc B C

x

x

M

Yd B C

y

y

Write C in terms of x y and linearize around x y

T T

F x x B y y B

x y

T T

C

F c c B d d B

x y

C Calculation

Make the denitions

E G B C

x

T T

H E B B G B C

x x

x

T T

r c B d B F C

x y

T

Note that H is symmetric H H

Then C yields

T T

C d B r c B

y x

From C one gets

c E C

so

T T

r H d B C

y

or

T T

r H B d C

y

Combining this with C yields

T T

H B r

y

C

B Y d

y

Thus for each iteration given x and y evaluate F B andB Then

x y

calculate E H andr andnd and d by solving C Finally

c follows from C

C Calculation

Dene

T T

W V H B

y

C

V U B Y

y

Note that since b oth H and Y are symmetric W and U are also symmetric

Multiplying out C yields

T

HW B V

B W YV

y

y

C

T

T T

B V YU

HV B U

y y

C Constrained Fit Details

From these relations one can derive the identities

T T T

WHW V YV V B W V B W

y y

C

W

T T T

VHV UYU UB V U B V

y y

U C

and

T T T T T T

V YU WHV V B V V B V

y y

C

Now combining C with C yields

T T

W r V

C

d V U

or multiplying it out

T

W r C

and

T

d V r C

Also from C

T

c E W r C

Pulling these all together and plugging them into the denition C the

result is suppressing sup erscripts

T T

c Gc d Yd

T T T T

rWE GEWr rV Y Vr

T T

rWHW V YV r

T

rWr

r

Thus

r C

C Convergence

C Convergence

The t is deemed to have converged if the following two criteria are satised

for two iterations in a row

X

jF j C

j j or j j C

That is when the constraints are satised and the has stopp ed changing

P

jF j is not decreasing If after several iterations the constraint sum

and the convergence conditions have not b een met then convergence is aided

with the use of directed steps If a directed step is not able to reduce the

constraint sum then the constraint problem undoubtedly has a very large

and no further iterations are made If the constraint sum is reduced then

normal iteration of the constraint problem is continued

C Directed Steps

For a directed step try to take the smallest step which satises the con

straints ie minimize

T

T

N G Y F C

by stepping to x y where

x x y y C

After linearizing this gives

T

T

F B B C

x y

G B G B C

x x

Y B Y B C

y y

Putting together C and C yields

T T

H B F C

y

Combining this with C

T T

F H B

y

C

B Y y

C Constrained Fit Details

This can be solved to nd and and thence

Using C the result is

T T

F W V

C

V U

or

T T

W F V F C

Then calculate the resulting using C

T T

c Gc d Yd

T T

c G c d Y d

T T

T T T T

G Y Gc Yd c Gc d Yd

T T

T T

B G GG B B Y Y

x x y

T T

T T

B G Gc B Y Yd

x y

T T T

T T T

B c B d H B

y x y

T T

T T T T

H W F B V F r F

y

F r F

r F C

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