Linearity Studies of the TileCal detector PMTs of ATLAS ... · PDF fileLinearity Studies of...

54
Linearity Studies of the TileCal detector PMTs of ATLAS/LHC experiment, with the Laser monitoring system by Bruno Miguel Leonardo Galhardo Dissertation submitted in partial fulfillment of the requirements for the Masters Degree in Nuclear Particles and Physics in the Faculdade de Ciˆ encias e Tecnologia da Universidade de Coimbra Departamento de F´ ısica Supervisor: Professor Doutor Jo˜ ao Carlos Lopes Carvalho July 2010

Transcript of Linearity Studies of the TileCal detector PMTs of ATLAS ... · PDF fileLinearity Studies of...

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Linearity Studies of the TileCal detector

PMTs of ATLAS/LHC experiment, with

the Laser monitoring system

by

Bruno Miguel Leonardo Galhardo

Dissertation submitted in partial fulfillment of the requirements for the

Masters Degree in Nuclear Particles and Physics

in the

Faculdade de Ciencias e Tecnologia da Universidade de Coimbra

Departamento de Fısica

Supervisor: Professor Doutor Joao Carlos Lopes Carvalho

July 2010

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UNIVERSIDADE DE COIMBRA

Abstract

Faculdade de Ciencias e Tecnologia da Universidade de Coimbra

Departamento de Fısica

Masters Degree in Nuclear Particles and Physics

by Bruno Miguel Leonardo Galhardo

An important parameter of the performance of a detector is its linear response. In

TileCal, an hadron calorimeter of scintillating tiles, the light is transmitted by optical

fibers wavelength shifting to be readout by photomultiplier tubes (PMT). They must

have a response that increases linearly with the intensity of light received, which is

proportional to the energy deposited by particles in the calorimeter. To measure the

linearity of the PMT one uses a laser system that sends both a well-defined quantity of

light, monitored by PMT and photodiodes installed inside the laser box, to all of the

approximately 10 000 PMT in TileCal. In this study was developed software for data

analysis, using the ROOT program, to study the linearity of the response of the PMTs.

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UNIVERSIDADE DE COIMBRA

Abstract

Faculdade de Ciencias e Tecnologia da Universidade de Coimbra

Departamento de Fısica

Masters Degree in Nuclear Particles and Physics

by Bruno Miguel Leonardo Galhardo

Um parametro importante para a medida do desempenho de um detector e a sua lineari-

dade de resposta. No TileCal, um calorımetro hadronico de telhas cintilantes, a luz de

cintilacao e transmitida por fibras opticas, com mudanca do comprimento de onda, para

leitura por tubos fotomultiplicadores (PMT). Estes tem de ter uma resposta que au-

menta linearmente com a intensidade de luz recebida, a qual sera proporcional a energia

depositada pelas partıculas no calorımetro. Para medir a linearidade dos PMT recorre-

se a um sistema laser que envia, simultaneamente, uma quantidade bem definida de luz,

monitorizada por PMT e fotodıodos instalados dentro da caixa do laser, para todos os

cerca de 10000 PMT do TileCal. Neste trabalho desenvolveu-se software de analise de

dados, recorrendo ao programa ROOT, para o estudo da linearidade de resposta dos

PMT.

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Acknowledgements

First of all i would like to thank my supervisor, Joao Carvalho, for his outstanding

guidance and dedication. I also want to thank my office colleagues and friends Susana

e Ines for their availability in helping me.

A big thanks to Miguel, for his huge help and hospitality in Switzerland, without it, i

would had a hard time adapting there.

I thank all my friends for for all the fun, fellowship and motivation especially Angela for

her true friendship, support and also some patience.

Finally i would like to thank my family for their continual and unconditional support

and affection.

iii

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Contents

Abstract i

Resumo ii

Acknowledgements iii

List of Figures vi

List of Tables viii

1 Introduction 1

2 ATLAS Detector 3

2.1 LHC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

2.2 ATLAS Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

2.2.1 Inner Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

2.2.2 Calorimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

2.2.3 Muon spectrometer . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

2.2.4 Magnet system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

2.2.5 Trigger and data acquisition systems . . . . . . . . . . . . . . . . . 11

2.2.6 GRID . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

3 TileCal and its calibration 13

3.1 Calibration of TileCal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

3.1.1 Cesium System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

3.1.2 LASER system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

3.1.2.1 LASER box . . . . . . . . . . . . . . . . . . . . . . . . . 16

3.1.2.2 Light Distribution System . . . . . . . . . . . . . . . . . 18

3.1.3 CIS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

4 Linearity studies using one LASER intensity and different wheel posi-tions 21

4.1 PMT1 vs diode 1 as references . . . . . . . . . . . . . . . . . . . . . . . . 25

4.2 rms vs gaussian error . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

4.3 Different intensities . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

iv

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Contents v

5 Linearity studies using a single filter wheel position and different in-tensity runs 33

5.1 PMTs vs PMT1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34

5.1.1 Linearity of the PMTs in the LASER box . . . . . . . . . . . . . . 34

5.1.2 Comparing runs with the same intensity . . . . . . . . . . . . . . . 36

5.1.3 Different intensities with temperature . . . . . . . . . . . . . . . . 38

5.2 Using diode 4 as reference . . . . . . . . . . . . . . . . . . . . . . . . . . . 39

5.3 Using the 1st PMT of the TileCal as reference . . . . . . . . . . . . . . . 40

5.4 Using the 1st PMT of the same fiber . . . . . . . . . . . . . . . . . . . . . 40

6 Conclusions 44

Bibliography 45

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List of Figures

2.1 LHC acceleration stages . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

2.2 Pseudorapidity Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

2.3 ATLAS detector scheme . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

2.4 Inner Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

2.5 Calorimeter sub-detectors . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

2.6 Muon spectrometer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

2.7 Magnet system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

3.1 Module of TileCal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

3.2 Section of a TileCal Module . . . . . . . . . . . . . . . . . . . . . . . . . . 14

3.3 Hardware calibration chain . . . . . . . . . . . . . . . . . . . . . . . . . . 15

3.4 Cesium passage through the cells . . . . . . . . . . . . . . . . . . . . . . . 16

3.5 The Laser box . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

3.6 Beam expander . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

3.7 The light distribution system . . . . . . . . . . . . . . . . . . . . . . . . . 19

3.8 Calibration event during a gap . . . . . . . . . . . . . . . . . . . . . . . . 19

4.1 Example of a gaussian fit . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

4.2 Attenuation factors histograms . . . . . . . . . . . . . . . . . . . . . . . . 23

4.3 Linearity Plots . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24

4.4 χ2/ndf comparison between 1 run fit and 3 run fit . . . . . . . . . . . . . 24

4.5 χ2 probability comparison between 1 run fit and 3 run fit . . . . . . . . . 24

4.6 χ2probability comparison using as references diode 1 and PMT1 . . . . . 26

4.7 χ2 probability comparison using rms error and gaussian ones . . . . . . . 27

4.8 15k run histograms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28

4.9 20k run histograms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

4.10 25k run histograms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

4.11 15k run histograms - set 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

4.12 20k run histograms - set 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

5.1 Example of a fit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34

5.2 PMT vs PMT1 plots . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35

5.3 Linearity of the PMTs in the LASER box . . . . . . . . . . . . . . . . . . 36

5.4 Fluctuations in the Signal for the same intensity . . . . . . . . . . . . . . 36

5.5 Temperature evolution in consecutive runs . . . . . . . . . . . . . . . . . . 37

5.6 Signals for PMT1 and PMT0 versus time for intensity 14k . . . . . . . . . 37

5.7 Signals for PMT1 and PMT0 versus the temperature for intensity 14k . . 37

5.8 Correlation between the ratios and temperature . . . . . . . . . . . . . . . 38

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List of Figures vii

5.9 Linearity plot for the 1st PMT of the Tilecal . . . . . . . . . . . . . . . . 38

5.10 Change in temperature along the runs . . . . . . . . . . . . . . . . . . . . 39

5.11 PMT vs diode 4 plots . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40

5.12 PMT vs 1st PMT of the TileCal plots . . . . . . . . . . . . . . . . . . . . 41

5.13 PMT vs 1st PMT of the fiber plots . . . . . . . . . . . . . . . . . . . . . . 42

5.14 Chi-square probability excluding the 1st point . . . . . . . . . . . . . . . . 43

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List of Tables

2.1 General Detector Performance . . . . . . . . . . . . . . . . . . . . . . . . . 7

3.1 Filter wheel attenuation factors . . . . . . . . . . . . . . . . . . . . . . . . 17

6.1 Summary of the results of the various methods . . . . . . . . . . . . . . . 44

viii

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Chapter 1

Introduction

At present, all the observable phenomena can be explain by four fundamental interac-

tions: the gravitation has a very weak intensity and acts on all matter; its importance is

taken into account on large systems but is negligible in particle physics (its incorporation

in particle physics remains a problem unsolved by theoretical physics). The electromag-

netic interaction is responsible for the cohesion of the atoms and a large portion of the

phenomena observable at our scale; the strong and weak interactions are responsible for

the cohesion of the atomic nuclei and radioactivity, respectively. The ultimate goal of

particle physics is to find a theory that explains and unifies all these interactions.

The Standard Model is a theory comprising: first, the electroweak theory (electromag-

netic interaction and weak interaction) and, secondly, the strong interaction. To this

day, all observed experimental particle physics phenomenon are explained by this the-

ory. All the particles in this theory (3 families/generations of fermions with 2 quarks, a

lepton and its neutrino, and 4 boson mediators) were found by experiments except one,

the Higgs boson.

With the purpose of testing the Standard Model and eventually alternative models

beyond the Standard Model, the Large Hadron Collider (LHC), was built at CERN

(European Organization for Nuclear Research). It is a proton-proton collider and will

reach a maximum energy of 14 TeV. In order to study the particle collisions, four detec-

tors are placed on LHC. One of them is ATLAS (A Toroidal LHC ApparatuS) and its

sub-detector TileCal is the one of interest in this work.

In order to provide the best possible physics input, the TileCal response must be perfectly

understood and optimized, so that the difference between the energy of the particle and

the energy we are reconstructing should be as small as possible. This is the role of the

calibration.

1

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Chapter 1. Introduction 2

One of 3 systems used to calibrate the hardware in TileCal is the LASER system.

It is used to calibrate and monitor all 9852 photomultipliers tubes (along with their

associated electronics) within the detector. The focus of this work will be an analysis of

the linearity response of those TileCal PMTs using this LASER system.

This thesis is structured as follows. In the second chapter, the accelerator (LHC) and the

ATLAS detector are presented. On the third chapter is described the calibration tools,

in particular the LASER system used in TileCal. On the fourth chapter is presented the

analysis and results of the linearity of the PMTs using the LASER system with runs

having only one intensity at a time. On chapter five is shown the analysis and results,

this time using different intensity runs. Lastly, chapter 6 is left for the conclusions and

comments about this study.

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Chapter 2

ATLAS Detector

2.1 LHC

With the purpose of studying the physics of particles under the framework of the Stan-

dard Model and other models beyond the Standard Model, the LHC was built. It is

a proton-proton collider located at CERN, near Geneva, Switzerland. This accelerator

will allow to access masses in the interval of a few GeV and several TeV. The motivation

behind the construction of this machines are the following:

• Comprehension of the origin of masses of the particles: currently, the Standard

Model explains this by the Higgs Mechanism which assumes a neutral boson called

Higgs boson. This particle could have a mass of 120GeV or all the way to 1TeV.

• Physics beyond the Standard Model: although the Standard Model gives predic-

tions verified to a level of 0.1%, some of its theoretical flaws (unification of coupling

constants, number of families, ...) suggest that this model is an approximation,

at low energy, of some more general model. So, the LHC will allow to observe

manifestations of these eventual new theories until energies of order of a TeV.

• Answering some open questions such as: are quarks and leptons the elementary

particles? What is the origin of the asymmetry between matter and anti-matter?

What is the origin of confinement of quarks?

• Precision measurements (Top mass, W width): due to the high luminosity of

LHC, measurements involving a large statistics can be made. They will test more

thoroughly the predictions of the Standard Model.

The accelerator was built in the LEP (Large Electron Positron collider) tunnel and

is 27km long and is placed 50-175m underground. The particles are accelerated by

3

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Chapter 2. ATLAS Detector 4

intense electric fields. An intense magnetic field of 8.4T will maintain the trajectory

of the protons in the ring. The acceleration of protons will be made in several stages

of accelerations, in various accelerators, to achieve the nominal energy. This chain is

represented in 2.1. The Linac2 will accelerate protons up to an energy of 50MeV. The

Booster (PSB) will reach an energy of 1GeV. The protons will be sent to PS bringing

their energy to 26GeV. Finally, the SPS will provide, as output, a beam of protons of

450GeV, which is injected into the LHC and where it reaches its nominal energy of

7TeV.

Figure 2.1: LHC acceleration stages

Four main experiments are installed at LHC: ATLAS and CMS (Compact Muon Solenoid)

are generalist experiments aiming to discover the Higgs boson or evidences of supersym-

metry among other things. Then there is ALICE (A Large Ion Collider Experiment)

which is focused in the study of heavy ion collisions (Pb-Pb). Its researches will search

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Chapter 2. ATLAS Detector 5

for evidence of a plasma of quarks and gluons. Lastly is LHCb which is dedicated to the

study o the violation of CP symmetry.

2.2 ATLAS Detector

The ATLAS detector is constituted of a set of sub detectors of cylindrical shape placed

around the beam pipe. The sub-detectors form layers around the collision point. In this

way, the particles emitted transversely pass through three types of sub-detectors:

• The inner tracker: it measures charged particles tracks and their momentum. The

curvature of the tracks is obtained thanks to the magnetic field of 2T produced

by a magnetic solenoid. It allows the determination of primary and secondary

vertices.

• The Calorimeters: two types of calorimeters are being used, the electromagnetic

followed by the hadronic. The electromagnetic calorimeter was designed to mea-

sure the energy of charged particles and photons through the electromagnetic in-

teraction, while the hadronic calorimeter measures the energy of hadrons that

interact via the strong interaction.

• The muon spectrometer: identifies and measures the momentum of muons. The

curvature of the trajectory of these particles is obtained by a toroid magnet.

Besides this, there are the two magnetic systems: a solenoid surrounding the Inner

Detector and the toroid magnets. The toroid magnets surround the calorimeters and

generate the magnetic field for the muon spectrometer.

One important variable used in ATLAS is the pseudo-rapidity, and is defined as

η = −ln(tan

2

)) (2.1)

Where θ is the polar angle (the azimuthal angle is φ). η is then related with the angle

between the object momentum and the beam pipe (z-axis). Its variation with θ is plotted

on Figure 2.2.

To achieve its goals, the detector needs to fulfill a set of requirements[1]:

• Fast electronics, resistant to the radiation, and high granularity to reduce events

overlap.

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Chapter 2. ATLAS Detector 6

Figure 2.2: Pseudorapidity (η) as a function of the polar angle (θ).

• Large acceptance in pseudo-rapidity, with a very large coverage in the azimuthal

angle.

• Good resolution in the charged particles momentum and reconstruction efficiency

in the Inner Detector. Pixel detectors close to the interaction point are required

for an efficient triggering and offline tagging of τ ’s and b-jets by observation of

secondary vertices.

• An electromagnetic calorimeter with an excelent capability of identification and

measurement of photons and electrons and an accurate hadronic calorimeter to

measure jet and missing transverse energy with precision.

• An independent muon identification with good momentum resolution to determine

unambiguously the charge of high pT muons.

• A triggering system for low pT particles with sufficient background rejection to

allow the observation of most of the physics processes of interest at the LHC.

The structure of the detector is shown on Figure 2.3 and the general performance goals

of ATLAS detector are on Table 2.1 [1]

2.2.1 Inner Detector

The inner detector determines the trajectories of the charged particles, their momentum

and the primary and secondary vertices. It allows the identification of electrons, labeling

of b-jets, τ leptons and the rejection of light jets. The objectives in terms of performance

of the sub-detector are [2]:

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Chapter 2. ATLAS Detector 7

Figure 2.3: ATLAS detector scheme

component Resolution η trigger (η)

Tracking σpT /pT = 0.05%× pT ⊕ 1% |η| < 2.5 -

EM calorimeter σE/E = 10%√E ⊕ 0.7% |η| < 3.2 |η| < 2.5

Hadronic calorimetry

barrel and end-cap σE/E = 50%√E ⊕ 3% |η| < 3.2 |η| < 3.2

forward σE/E = 100%√E ⊕ 10% |η| < 4.9 |η| < 4.9

Muon spectrometer σpT /pT = 10%@pT = 1TeV |η| < 2.7 |η| < 2.4

Table 2.1: General Detector Performance

• Reconstruction of tracks for |η| < 2.5.

• The angles θ are measured with a precision of, at least, 2 mrad.

• The primary vertex is found along the z axis with an accuracy better than 1mm.

• The identification of electrons with pT ≥ 7 GeV is greater than 90%.

• Identification of photons combined with the electromagnetic calorimeter

• Identification of jets from b-quark.

The Inner Detector has three parts, the Pixel Detector, the Semiconductor Tracker

(SCT) and the Transition Radiation Tracker (TRT). All contained on a 2T magnetic field

that bends charged particles trajectory to allow measurement of the particles momenta

(Figure 2.4).

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Chapter 2. ATLAS Detector 8

Figure 2.4: Inner Detector

2.2.2 Calorimeters

There are two calorimeters in the ATLAS detector: the electromagnetic and the hadronic,

covering the regions |η| < 3.2 and |η| < 4.9, respectively (Figure 2.5). The electromag-

netic calorimeter allows a precise measure of the energy and position of the electrons

and photons that interact through electromagnetic force while the hadronic absorbs the

energy of particles that interact through the strong force, after crossing the electro-

magnetic calorimeter. The hadronic calorimeter is meant to detect the particle shower

resulting from the hadronization of the quarks, also known as jet, allowing to measure

the energy of the original particle after calibration.

The EM calorimeter [3, 4] is a sampling calorimeter made of layers of lead (used as the

passive material). Between the layers, liquid argon (LAr) is used as the active material.

The accordion geometry provides complete φ symmetry without azimuthal cracks. It is

divided into three regions: the barrel (|η| < 1.475) and two end-caps (1.375 < |η| < 3.2).

It has the following properties:

• An angular coverage as large as possible to collect a maximum of rare events and

to measure the missing energy.

• An excellent resolution on the energy in the order of 1%.

• A precise measurement of the direction of electromagnetic showers.

• An excellent separation of γs.

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Chapter 2. ATLAS Detector 9

Figure 2.5: Calorimeter sub-detectors

The hadronic calorimeter is composed by three sub-detectors: the tile calorimeter (Tile-

Cal), the LAr hadronic end-cap calorimeter (HEC) and the LAr forward calorimeter

(FCal). The TileCal [5, 6] is a sampling calorimeter using steel as the absorber and

scintillator as the active medium. It is located in the region |η| < 1.7, behind the LAr

EM calorimeter, and it is subdivided into a barrel central region (|η| < 1.0) and two

extended barrels (0.8 < |η| < 1.7). The light produced in the scintillating tiles is col-

lected at the edges of each tile using two wavelength shifting fibers that conduct the

light to photomultipliers. The HEC covers the region 1.5 < |η| < 3.2 overlapping the

forward calorimeter. Each HEC consists of two wheels with a radius of 2.03m, each with

32 modules, and is divided in two longitudinal segments. Finally, the FCal is located

at 4.5m from the interaction point covering the region 3.1 < |η| < 4.9 with the main

purpose of minimising the loss of energy and reduce background radiation levels in the

muon spectrometer. FCal and HEC use cooper as the absorber and LAr as the active

material. Its properties are:

• The identification of jets, the measurement of their energy and their direction.

• Good coverage in η to measure precisely the missing transverse energy.

• A good granularity.

• A linear response in energies for |η| < 3.

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Chapter 2. ATLAS Detector 10

2.2.3 Muon spectrometer

The muon spectrometer is the last layer of ATLAS detector, has a cylindrical shape and

measures 22m of diameter and 46m long. It has a full coverage in the region |η| < 2.7,

with the exception of a region around η = 0, where a 300mm gap is present, allowing for

the passage of the services for the ID detector, solenoid and calorimeters. This gap leads

to a significant degradation of the muon reconstruction efficiency in that region. The

Superconductors generate a magnetic field perpendicular to the trajectory of muons.

The spectrometer measures the deviation to determine the momentum of muons.

To efficiently identify and measure muons, the Muon Spectrometer is composed by four

different tracking detector technologies: Monitored Drift Tubes (MDT) and Cathode

Strip Chambers (CSC) precision detectors in the barrel and end-cap regions; Resistive

Plate Chambers (RPC) and Thin Gap Chambers (TGC) that provide fast trigger signals

in the barrel and end-cap regions (Figure 2.6).

Figure 2.6: Muon spectrometer

The goals of this sub-detector are:

• A good resolution on the measurement of the transverse momentum for 5GeV<E

<1 TeV.

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Chapter 2. ATLAS Detector 11

• A good reconstruction of the muons tracks.

• Good angular coverage (|η| < 3).

• Ability to function in standalone mode (without the tracker).

2.2.4 Magnet system

Apart from the three main sub-detectors, ATLAS, has a system of four large super-

conducting magnets with the purpose of bending the charged particles produced in the

events, allowing to measure their momentum and charge sign. The ATLAS magnet sys-

tem consists of a solenoid, aligned with the beam axis, providing a 2T axially symmetric

magnetic field for the inner detector; a barrel and two end-cap toroids, which produce a

toroidal magnetic field of 0.5T and 1T, respectively, for the muon detectors. Figure 2.6

shows the geometry of the magnet system.

Figure 2.7: Magnet system

2.2.5 Trigger and data acquisition systems

The selection of events in ATLAS is done on three levels of trigger, based on the signa-

tures of high-pT particles and missing transverse energy. Each level allows to refine the

selection in order to pass from a frequency of events of 109Hz to a frequency of storage

of 100Hz. The trigger will therefore provide a factor of rejection of about 107.

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Chapter 2. ATLAS Detector 12

The level 1 trigger will select high pT muons, electrons, photons, jets and τ leptons

decaying in hadrons. The decision time of 2µs includes the transmission of signals

between the detector and the trigger electronics. After the 1st has accepted an event,

the data is read out, formatted and stored in buffers, being available to the next levels.

The level 2 trigger uses about 2% of total event data at full granularity and precision,

and it will reduce the trigger rate to 3.5kHz. At this stage, the processing time for an

average event is 10ms. At final stage the rate will be reduced to 100Hz.

2.2.6 GRID

The LHC computing Grid is a distribution network designed to handle the massive

amounts of data produced by the Large Hadron Collider (LHC). It incorporates both

private fiber optic cable links and existing high-speed portions of the public Internet.

The data stream from the detectors provides approximately 300 GB/s, which is filtered

for ‘interesting events’, resulting in a ‘raw data’ stream of about 300 MB/s. This makes

more than 1PB of data per year. The storage and offline reconstruction of this amount

of data require the use of a large storage and computing resources. The Grid sites

are organized in Tiers: the Tier-0 is located at CERN (where the data is produced)

and it is connected via high-speed networks to eleven Tier-1 sites (located in different

countries), which will store the output of event reconstruction. The Tier-1 centres

will make data available to more than 150 Tier-2 centres, each consisting of one or

several collaborating computing facilities, which can store sufficient data and provide

adequate computing power for specific analysis tasks. Individual scientists will access

these facilities through Tier-3 computing resources, which consist of local clusters (or

even individual computers).

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Chapter 3

TileCal and its calibration

The TileCal is a sub-detector of ATLAS as explained in the previous chapter. It is

made of three aligned barrels. Both barrels on the exterior are the extended barrels.

They measure 2.91m in length and cover the following range of pseudo-rapidity: 0.8 <

|η| < 1.7. The central barrel is called the Long Barrel and is 5.64m long, covering the

pseudo-rapidity range |η| < 1. All three sections are subdivided into 64 independent

modules. Each module covers a portion of 2π/64 angle in φ that gives the granularity

in φ. Radially, the modules are divided into three layers (Figure 3.1): A, BC and D.

They correspond, respectively, at 1.4, 3.9 and 1.8 interaction length. The granularity

∆η×∆φ of the TileCal is 0.1×0.1 for the first two layers and 0.2×0.1 for the third layer.

Figure 3.1: Different layers of a module of TileCal

The calorimeter measures only a fraction of the energy deposited by the incoming parti-

cles (it is a sampling calorimeter). The absorber plate is iron, while the active medium is

constituted of scintillating tiles. The particles deposite a fraction of their energy in the

scintillating tiles, which is converted into light. The light is transported by wavelength

shifting fibers, placed on each side of scintillating tiles. The absorption spectrum of

13

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Chapter 3. TileCal and its calibration 14

the fiber is adapted to the wavelength of light produced in the scintillating tiles. The

emission spectrum has been tailored to the absorption efficiency of the Photomultipli-

ers (PMTs). PMTs are placed on the other end of the fiber converting the light into

electrical signals. The charge collected by each PMT is then digitized and passed to the

ATLAS readout system, allowing to double reading each cell. The scintillating tiles are

placed in a plane perpendicular to the beam, and this geometry allows for the connection

of optical fibers on the side outside of the module. Figure 3.2 represents a section of a

TileCal module.

Figure 3.2: Section of a TileCal Module

3.1 Calibration of TileCal

In order to reach good physics analysis, the difference between the energy of the particle

and the energy we are reconstructing should be as small as possible. This is the role of

the calibration which can be made in two ways[11]:

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Chapter 3. TileCal and its calibration 15

• Hardware: a quantitative understanding of the TileCal response requires moni-

toring and control of a large number of parameters such as electronic noise, PMT

gain, among others, which in turn depend on a large number of variables (time,

temperature,...). All such parameters must be known precisely in order to cor-

rectly interpret the data collected. Consequently, all these parameters have to be

measured precisely and integrated into the calibration system.

• Software: once the hardware calibration has been performed, one still has to

correctly estimate the shower energy. The calorimeter finite granularity will lead

to a non-exact estimation of the shower energy, even with a perfect hardware

calibration. This is sorted out using specific software corrections.

There are three main components in the TileCal calibration scheme (Figure 3.3) - the

Cesium system, the LASER system and the charge injection system (CIS). With those

3 systems we achieve a complete calibration of the hardware chain, from the active

modules to the read-out electronics.

Figure 3.3: Hardware calibration chain

3.1.1 Cesium System

A 137Cs source is moved inside the calorimeter modules during ATLAS shutdown periods

via a complex network of pipes filled with water. The light thus produced is collected

and measured for each cell, leading to the comparison of each TileCal cell response. In

Figure 3.4 is shown the response of 5 cells during the passage of the Cesium source.

Each secondary peak represents the passage of the source through a tile. In this case,

for the second cell, there is an absence of a peak. This is due to poor coupling between

the fiber and the scintillating tile. With the detection of such a flaw one can make a

repair. However since the signal passes through the full data aquisition chain if the

Cesium sees a drop in one cell efficiency, it could be due to different sorts of problems,

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Chapter 3. TileCal and its calibration 16

for example a gain variation in the PMTs. We thus need other systems in order to solve

this uncertainty.

Figure 3.4: PMT current as a function of source position for 5 adjacent cells

The Cs system provides a calibration of the full readout chain.

3.1.2 LASER system

The LASER system is the next in the chain and was designed to calibrate and monitor

the PMTs response with an accuracy better that 0.5%. The LASER pulse produces a

similar PMT response as a signal generated by a particle in the TileCal. The major

difference is that the initial energy of the light pulse is known precisely (better than

1%). This enables accurate monitoring of PMT gains and linearity.

The LASER system is divided into two main parts: the LASER box and the light

distribution system.

3.1.2.1 LASER box

The LASER box (in Figure 3.5) contains not only the LASER head, but also two PMTs

used for triggering and monitoring purposes, four Si PIN photodiodes (inter-calibrated

by a 241Am source) used for the absolute measurement of the light intensity emitted by

the LASER, and the optical circuitry necessary for changing the LASER beam intensity.

The humidity and temperature in the box are constantly monitored and controlled.

The LASER light is transmitted to the photodiodes via four optical fibers connected

to the box. One out of the four fibers (the one linked to diode number 1) is receiving

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Chapter 3. TileCal and its calibration 17

Figure 3.5: The Laser box

light collected directly in the LASER box, whereas the others are getting information

at another level of the system. Diode 1 and the two PMTs (which are similar to the

PMTs installed in the TileCal) receive light via a semi-reflecting mirror.

The light that is not reflected by the mirror passes through a filter wheel with 8 holes.

One of them is empty (position 5) while the others contain filters providing beam atten-

uation with a factor 3 to 1000. The design values of the filter attenuations are in Table

3.1. These filters were chosen to provide full coverage of the entire TileCal dynamic

range, from a few hundred of MeV to around 1TeV.

Position 1 2 3 4 5 6 7 8

Attenuation 1050±350 103±23 32±6 10±1 1 3.1±0.2 103±23 330±100

Table 3.1: Filter wheel attenuation factors

In the Laser box there is also a shutter, which was installed for safety reasons and is

closed when the LASER is not in use. It can be used to make tests without sending

light to the TileCal.

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Chapter 3. TileCal and its calibration 18

3.1.2.2 Light Distribution System

If a LASER pulse is emitted when the shutter is opened, the light exits the LASER box

and enters into a 1m long liquid light guide. It links the LASER box output to the first

component of the light distribution system - the beam expander (Figure 3.6). It is a

system composed of two lenses that expand the beam diameter. It also has a diffuser in

order to prevent effects due to LASER light coherence. The Coimbra box in turn sends

the primary beam toward a bunch of 384 clear fibers (128 for each end-cap barrel, and

128 for the long barrel).

Figure 3.6: Beam expander

Each fiber is glued to an adjustable connector that is held in a big patch panel located

immediately behind the LASER box. The role of the connectors is to equalize the light

sent by all the fibers to the TileCal. The fact that all PMTs receive roughly the same

light amount simplifies the calibration work.

At the other side of the connectors, long clear fibers take the light individually to TileCal

drawers where they are split a last time in order to reach all the PMTs. Each extended

barrel is fed by two fibers (17 PMTs per fiber) and each barrel module (two partitions)

is fed by two fibers (45 PMTs per fiber). This is summarized in Figure 3.7.

Again, not all of the fibers coming out of the Coimbra box go to the TileCal. Around

20 fibers are either kept as spares, or used to feed the three remaining diodes in the

LASER box.

This system is fast enough to be used in the acquisition phase. During each acquisition

run the LASER will send pulses in the gaps of beam particle crossing. This is used to

check, for example, the status of the PMTs during all the data acquisition run (Figure

3.8).

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Chapter 3. TileCal and its calibration 19

Figure 3.7: The light distribution system

Figure 3.8: Calibration event during a gap

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Chapter 3. TileCal and its calibration 20

3.1.3 CIS

Change impulses of known intensity are pulsed into the readout electronic chain. These

mimic the response of the PMTs in the electronics located ahead of the PMTs. It leads

to a precise estimation of the electronic noise and linearity. Its objective is an accuracy

of around 1%. In ATLAS there will be periodic CIS runs over the full dynamic range

during maintenance periods. Also, in data acquisition phases, a fixed amplitude signal is

injected when there are no crossings of particles, for calibration purposes. CIS calibrates

the end side of the readout chain.

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Chapter 4

Linearity studies using one

LASER intensity and different

wheel positions

The files being analyzed are ntuples coming from LASER runs with all sorts of infor-

mation, such as the signal of TileCal PMT, the ADC of the LASER box four diodes

and the two PMTs and respective pedestals, intensity of the LASER, temperature, etc.

The runs used are: 129566, 129570, 129574, 130425, 130430, 130435 corresponding to

the LASER intensities: 15k, 20k, 25k, 15k, 20k, 25k respectively.

The linearity plots will be made plotting the signal of a PMT of the TileCal against the

reference signal (Diode 1 or PMT 1). Since the signal from the references comes from

the LASER light reflected by the mirror that is never attenuated by the filter wheel (as

explained in chapter 3), that attenuation factor needs to be taken into account to scale

the reference signal and make the plot.

The first thing to do is to convert the histograms from each TileCal PMT and the

reference signal used (Diode 1 or PMT 1 of the LASER box) to a mean value. This is

done fitting a gaussian function to the histogram and taking the p1 parameter (mean) as

shown in Figure 4.1. Selecting only the signals in the interval 0.1-700pC and 50-2050ADC

for the TileCal PMTs and the PMTs or diodes of the LASER box respectively.

f(x) = p0e− 1

2

(x−p1p2

)2

(4.1)

The attenuation factors are computed as the ratio between the mean signal (from the

fit described above) of a PMT using filter 5 (no attenuation) and the filter in question.

21

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Chapter 4. Linearity studies using one LASER intensity and different wheel positions22

Entries 2373Mean 64.64RMS 5.935

Signal (in pC)45 50 55 60 65 70 75 80 85

Nu

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er o

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40

50

60

70

80Entries 2373Mean 64.64RMS 5.935

Figure 4.1: Gaussian fit for the signal of PMT000 for filter 5 and intensity 15k.

E5 = FiEi ↔ Fi =E5

Ei, i = filters wheel positions (4.2)

Making an histogram with all the PMTs calculated factors for a given filter, one can

fit a gaussian function again to get the mean value. The histograms for each filter are

shown in Figure 4.2.

These values are within the ones provided by the manufacturer (Table 3.1).

Now, having the values for the PMTs signal and the reference signal (scaled with the

attenuated factor) it is possible to make the linearity plot.

The plots with one and all the three runs were done (Figure 4.3) and it is evident that

when we mix the three runs there are sources of systematic errors that increase the chi-

square probability (χ2/ndf and χ2 probability plots in Figures 4.4 and 4.5 respectively).

These problems will be addressed in chapter 5.

It is worth noting that even using only one run, the fit does not give good a χ2 probability

because the errors coming from each point are so small. In fact, looking at Figure 4.1

it is clear that the fit is done from a large sample of data, which makes the statistical

errors very small. The errors used so far are rms/√n and, as one can see, with such a

large n the errors are very small.

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Chapter 4. Linearity studies using one LASER intensity and different wheel positions23

Entries 9551Mean 928.4RMS 20.74

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Entries 9551Mean 928.4RMS 20.74

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Entries 9552Mean 10.07RMS 0.09457

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Entries 9552Mean 242.2RMS 1.793

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600

700Entries 9552Mean 242.2RMS 1.793

(g)

Figure 4.2: Histograms obtained from the attenuation factors from all the PMTs.a)Attenuation factor for filter 1, b) for filter 2, c) for filter 3, d) for filter 4, e) for filter

6, f) for filter 7, f) for filter 8.

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Chapter 4. Linearity studies using one LASER intensity and different wheel positions24

PMT 1 signal (in ADC)20 40 60 80 100 120 140 160 180 200 220

PM

T s

ign

al (

in p

C)

0

10

20

30

40

50

60

70

/ ndf 2χ 3655 / 6p0 0.0007401± -0.05545 p1 0.0003563± 0.3062

/ ndf 2χ 3655 / 6p0 0.0007401± -0.05545 p1 0.0003563± 0.3062

(a)

PMT1 signal (in ADC)100 200 300 400 500 600

PM

T s

ign

al (

in p

C)

0

50

100

150

200

/ ndf 2χ 8985 / 22p0 0.0004576± -0.02608 p1 0.0001226± 0.3147

/ ndf 2χ 8985 / 22p0 0.0004576± -0.02608 p1 0.0001226± 0.3147

(b)

Figure 4.3: Linearity plots for PMT000 with a) 8 points using 1 run b) 24 points, 3runs.

Entries 9619

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40

50

60

70

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90

(b)

Figure 4.4: χ2/ndf a) using 1 run b) using 3 runs.

Chi-square probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Nu

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Figure 4.5: χ2 probability a) using 1 run b) using 3 runs.

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Chapter 4. Linearity studies using one LASER intensity and different wheel positions25

4.1 PMT1 vs diode 1 as references

Another fact to note is that it was used so far the PMT1 as reference (instead of diode 1)

because the diodes are affected by the light crosstalk effect [10] meaning so that the four

of them are close enough to affect the signals of each other. While this is not a problem

when making stability analysis, it becomes more serious for the linearity because the

diodes signal will not be linear anymore.

Comparing the fits coming from plots with the PMT1 and the diode 1 as reference, one

ends up with Figure 4.6.

From this results it cannot be observed the crosstalk effect as both references give very

similar probabilities in the fit.

4.2 rms vs gaussian error

Another comparison that can be done is between using rms errors or the error from the

gaussian fit in the mean parameter p1. As shown in Figure 4.7, there is some difference

between the methods of errors used. However, it seems that there are no systematic

effect.

4.3 Different intensities

Now, using PMT1 as reference (that does not suffer from the crosstalk), one could

compare runs 129566, 129570, 129574 (15k, 20k and 25k) parameters plotted in Figures

4.8, 4.9 and 4.10. Although the probability plots do not seem to follow any pattern, since

the fits continue to appear very bad, due to the very small statistical errors, there is an

improvement in the fit, looking at the residuals. Low intensities, such as 15k (Figures

4.8 and 4.11) filters 1 and 7 and, to some extension, filter 8 (corresponding to larger

filter attenuations or, in another way, weaker signals) give the bigger deviations from

the fit. This is due to the non-linearity of the electronics[10] that occurs for signals

<100pC. Since the signals are selected in the interval from 0.1 to 700pC the results

show that effect. In the next chapter those values will not be considered. It is worth to

point out that all the residuals are around zero meaning that they are not biased. The

offset parameter is also around zero as expected. Looking at the residual values, and

disregarding filter 1, 7 and 8 at low intensity, they are between around 1% to 2%.

Also comparing both 15k runs 129566 (Figure 4.8) and 130425 (Figure 4.11), and 20k

run (Figure 4.9) and 130425 (Figure 4.12) the results are similar as it was expected.

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Chapter 4. Linearity studies using one LASER intensity and different wheel positions26

Entries 9619

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Figure 4.6: χ2probability comparison using as references diode 1 and PMT1 a) 15krun using diode 1 as reference b) 15k run using PMT1 c) 20k run using diode 1 d) 20k

run using PMT1 e) 25k run using diode 1 and f) 25k run using PMT1.

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Chapter 4. Linearity studies using one LASER intensity and different wheel positions27

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qui-squared probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Nu

mb

er o

f en

trie

s

0

1000

2000

3000

4000

5000

6000

Entries 9552Mean 0.06101

RMS 0.1578

(d)

Entries 9477

Mean 0.02728

RMS 0.1036

qui squared probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Nu

mb

er o

f E

ntr

ies

0

1000

2000

3000

4000

5000

6000

7000

8000Entries 9477

Mean 0.02728

RMS 0.1036

(e)

Entries 9477

Mean 0.01878

RMS 0.08622

qui-squared probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Nu

mb

er o

f en

trie

s

0

1000

2000

3000

4000

5000

6000

7000

8000

Entries 9477

Mean 0.01878

RMS 0.08622

(f)

Figure 4.7: χ2 probability comparison between rms error and gaussian a) 15k runusing rms error b) 15k run using gaussian error c) 20k run using rms error d) 20k runusing gaussian error e) 25k run using rms error and f) 25k run using gaussian error.

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Chapter 4. Linearity studies using one LASER intensity and different wheel positions28

Entries 9619Mean 0.09411

RMS 0.1905

qui squared probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

nu

mb

er o

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trie

s

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1000

2000

3000

4000

5000

Entries 9619Mean 0.09411

RMS 0.1905

(a)

Entries 9619

Mean 0.002103

RMS 0.007636

offset-0.05 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 0.05

nu

mb

er o

f en

trie

s0

100

200

300

400

500

600

Entries 9619

Mean 0.002103

RMS 0.007636

(b)

Entries 9619Mean 0.6134

RMS 0.2021

Slope0 0.5 1 1.5 2 2.5

Nu

mb

er o

f en

trie

s

0

50

100

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350

Entries 9619Mean 0.6134

RMS 0.2021

(c)

Entries 9607Mean -0.3391

RMS 5.104

Normalized residual of point corresponding to filter 1 (in %)-20 -15 -10 -5 0 5 10 15 20

nu

mb

er o

f en

trie

s

0

50

100

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300

Entries 9607Mean -0.3391

RMS 5.104

(d)

Entries 9619Mean -0.387RMS 1.051

Normalized residual of point corresponding to filter 2 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f ev

ents

0

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250

Entries 9619Mean -0.387RMS 1.051

(e)

Entries 9619Mean -0.1566

RMS 0.6585

Normalized residual of point corresponding to filter 3 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

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300

350

400

450

Entries 9619Mean -0.1566

RMS 0.6585

(f)

Entries 9617Mean 0.3174

RMS 1.259

Normalized residual of point corresponding to filter 4 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

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300

Entries 9617Mean 0.3174

RMS 1.259

(g)

Entries 9619

Mean 0.09115

RMS 0.7186

Normalized residual of point corresponding to filter 5 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

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300

350

400

Entries 9619

Mean 0.09115

RMS 0.7186

(h)

Entries 9618

Mean 0.09676

RMS 0.7602

Normalized residual of point corresponding to filter 6 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

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250

300

350

400

Entries 9618

Mean 0.09676

RMS 0.7602

(i)

Entries 9601Mean 0.766RMS 5.688

Normalized residual of point corresponding to filter 7 (in %)-20 -15 -10 -5 0 5 10 15 20

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

Entries 9601Mean 0.766RMS 5.688

(j)

Entries 9617Mean -0.3783

RMS 1.793

Normalized residual of point corresponding to filter 8 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f ev

ents

0

20

40

60

80

100

120

Entries 9617Mean -0.3783

RMS 1.793

(k)

Figure 4.8: 15k run histograms (run 129566) a) the χ2 probability, b) the offsetparameter, c) the slope and d-k) the normalized residuals (in %) for the 8 filter wheel

positions.

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Chapter 4. Linearity studies using one LASER intensity and different wheel positions29

Entries 9552

Mean 0.05922

RMS 0.1555

qui squared probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

Nu

mb

er o

f en

trie

s

0

1000

2000

3000

4000

5000

6000

Entries 9552

Mean 0.05922

RMS 0.1555

(a)

Entries 9552

Mean -0.0004076

RMS 0.005154

offset-0.05 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 0.05

nu

mb

er o

f en

trie

s0

100

200

300

400

500

600

700

800

900Entries 9552

Mean -0.0004076

RMS 0.005154

(b)

Entries 9552Mean 0.6244

RMS 0.1857

slope0 0.5 1 1.5 2 2.5

nu

mb

er o

f ev

ents

0

50

100

150

200

250

300

Entries 9552Mean 0.6244

RMS 0.1857

(c)

Entries 9551

Mean 0.02396

RMS 0.7211

Normalized residual of point corresponding to filter 1 (in %)-10 -5 0 5 10

nu

mb

er o

f en

trie

s

0

200

400

600

800

1000

1200

1400

1600

1800

Entries 9551

Mean 0.02396

RMS 0.7211

(d)

Entries 9552

Mean -0.04984

RMS 0.5175

Normalized residual of point corresponding to filter 2 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

100

200

300

400

500

Entries 9552

Mean -0.04984

RMS 0.5175

(e)

Entries 9552Mean 0.1333

RMS 0.8848

Normalized residual of point corresponding to filter 3 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

100

200

300

400

500

Entries 9552Mean 0.1333

RMS 0.8848

(f)

Entries 9551

Mean 0.01728

RMS 0.7116

Normalized residual of point corresponding to filter 4 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

300

350

Entries 9551

Mean 0.01728

RMS 0.7116

(g)

Entries 9552

Mean -0.01698

RMS 0.3489

Normalized residual of point corresponding to filter 5 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

100

200

300

400

500

600

700

800

Entries 9552

Mean -0.01698

RMS 0.3489

(h)

Entries 9552

Mean -0.01771

RMS 0.2954

Normalized residual of point corresponding to filter 6 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

200

400

600

800

1000

Entries 9552

Mean -0.01771

RMS 0.2954

(i)

Entries 9551Mean -0.0103

RMS 1.195

Normalized residual of point corresponding to filter 7 (in %)-20 -15 -10 -5 0 5 10 15 20

nu

mb

er o

f en

trie

s

0

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400

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800

1000

1200

Entries 9551Mean -0.0103

RMS 1.195

(j)

Entries 9552

Mean -0.08198

RMS 0.6339

Normalized residual of point corresponding to filter 8 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

300

350

400

Entries 9552

Mean -0.08198

RMS 0.6339

(k)

Figure 4.9: 20k run histograms (run 129570) a) the χ2 probability, b) the offsetparameter, c) the slope and d-k) the normalized residuals (in %) for the 8 filter wheel

positions.

Page 39: Linearity Studies of the TileCal detector PMTs of ATLAS ... · PDF fileLinearity Studies of the TileCal detector PMTs of ATLAS/LHC experiment, with the Laser monitoring system by ...

Chapter 4. Linearity studies using one LASER intensity and different wheel positions30

Entries 9477

Mean 0.01773

RMS 0.08379

qui squared probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

nu

mb

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trie

s

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1000

2000

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5000

6000

7000

8000

Entries 9477

Mean 0.01773

RMS 0.08379

(a)

Entries 9477

Mean -0.0003221

RMS 0.005049

offset-0.05 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 0.05

nu

mb

er o

f en

trie

s0

100

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500

600

700

800

900

Entries 9477

Mean -0.0003221

RMS 0.005049

(b)

Entries 9477Mean 0.6305

RMS 0.1784

slope0 0.5 1 1.5 2 2.5

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

300

Entries 9477Mean 0.6305

RMS 0.1784

(c)

Entries 9476

Mean -0.02317

RMS 1.069

Normalized residual of point corresponding to filter 1 (in %)-20 -15 -10 -5 0 5 10 15 20

nu

mb

er o

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trie

s

0

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1200

1400

1600

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Entries 9476

Mean -0.02317

RMS 1.069

(d)

Entries 9476

Mean -0.03562

RMS 0.5292

Normalized residual of point corresponding to filter 2 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

100

200

300

400

500

Entries 9476

Mean -0.03562

RMS 0.5292

(e)

Entries 9475Mean 0.2088

RMS 1.222

Normalized residual of point corresponding to filter 3 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

150

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300

350

Entries 9475Mean 0.2088

RMS 1.222

(f)

Entries 9476

Mean -0.001479

RMS 0.61

Normalized residual of point corresponding to filter 4 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

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300

350

400

Entries 9476

Mean -0.001479

RMS 0.61

(g)

Entries 9477

Mean -0.02668

RMS 0.3038

Normalized residual of point corresponding to filter 5 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f ev

ents

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600

700

800

900

Entries 9477

Mean -0.02668

RMS 0.3038

(h)

Entries 9477

Mean -0.02201

RMS 0.3026

Normalized residual of point corresponding to filter 6 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

100

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300

400

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600

700

800

900

Entries 9477

Mean -0.02201

RMS 0.3026

(i)

Entries 9476

Mean -0.07963

RMS 1.207

Normalized residual of point corresponding to filter 7 (in %)-20 -15 -10 -5 0 5 10 15 20

nu

mb

er o

f en

trie

s

0

200

400

600

800

1000

1200

Entries 9476

Mean -0.07963

RMS 1.207

(j)

Entries 9476

Mean -0.04466

RMS 0.5808

Normalized residual of point corresponding to filter 8 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

300

350

400

Entries 9476

Mean -0.04466

RMS 0.5808

(k)

Figure 4.10: 15k run histograms (run 129574) a) the χ2 probability, b) the offsetparameter, c) the slope and d-k) the normalized residuals (in %) for the 8 filter wheel

positions.

Page 40: Linearity Studies of the TileCal detector PMTs of ATLAS ... · PDF fileLinearity Studies of the TileCal detector PMTs of ATLAS/LHC experiment, with the Laser monitoring system by ...

Chapter 4. Linearity studies using one LASER intensity and different wheel positions31

Entries 9647Mean 0.1026

RMS 0.2003

qui squared probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

nu

mb

er o

f en

trie

s

0

1000

2000

3000

4000

5000

Entries 9647Mean 0.1026

RMS 0.2003

(a)

Entries 9647

Mean 0.002154

RMS 0.007995

offset-0.05 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 0.05

nu

mb

er o

f en

trie

s0

100

200

300

400

500

600

Entries 9647

Mean 0.002154

RMS 0.007995

(b)

Entries 9647Mean 0.6381

RMS 0.2285

slope0 0.5 1 1.5 2 2.5

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

300

350Entries 9647Mean 0.6381

RMS 0.2285

(c)

Entries 9635Mean -0.1532

RMS 4.652

Normalized residual of point corresponding to filter 1 (in %)-20 -15 -10 -5 0 5 10 15 20

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

300

350

Entries 9635Mean -0.1532

RMS 4.652

(d)

Entries 9647Mean -0.3947

RMS 1.058

Normalized residual of point corresponding to filter 2 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

20

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240

Entries 9647Mean -0.3947

RMS 1.058

(e)

Entries 9647Mean -0.1491

RMS 0.6422

Normalized residual of point corresponding to filter 3 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

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150

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300

350

400

450

Entries 9647Mean -0.1491

RMS 0.6422

(f)

Entries 9647Mean 0.3302

RMS 1.238

Normalized residual of point corresponding to filter 4 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

300Entries 9647Mean 0.3302

RMS 1.238

(g)

Entries 9647Mean 0.1034

RMS 0.7396

Normalized residual of point corresponding to filter 5 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

50

100

150

200

250

300

350

400Entries 9647Mean 0.1034

RMS 0.7396

(h)

Entries 9646Mean 0.1075

RMS 0.7915

Normalized residual of point corresponding to filter 6 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

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trie

s

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400

Entries 9646Mean 0.1075

RMS 0.7915

(i)

Entries 9627Mean 0.5878

RMS 6.013

Normalized residual of point corresponding to filter 7 (in %)-20 -15 -10 -5 0 5 10 15 20

nu

mb

er o

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s

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Entries 9627Mean 0.5878

RMS 6.013

(j)

Entries 9645Mean -0.3903

RMS 1.789

Normalized residual of point corresponding to filter 8 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

f en

trie

s

0

20

40

60

80

100

120

Entries 9645Mean -0.3903

RMS 1.789

(k)

Figure 4.11: 15k run histograms (run 130425) a) the χ2 probability, b) the offsetparameter, c) the slope and d-k) the normalized residuals (in %) for the 8 filter wheel

positions.

Page 41: Linearity Studies of the TileCal detector PMTs of ATLAS ... · PDF fileLinearity Studies of the TileCal detector PMTs of ATLAS/LHC experiment, with the Laser monitoring system by ...

Chapter 4. Linearity studies using one LASER intensity and different wheel positions32

Entries 9533

Mean 0.07077

RMS 0.1727

qui squared probability0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

nu

mb

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Entries 9533

Mean 0.07077

RMS 0.1727

(a)

Entries 9533

Mean -0.0006397

RMS 0.00619

offset-0.05 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 0.05

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Entries 9533

Mean -0.0006397

RMS 0.00619

(b)

Entries 9533Mean 0.6331

RMS 0.2009

slope0 0.5 1 1.5 2 2.5

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mb

er o

f en

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s

0

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Entries 9533Mean 0.6331

RMS 0.2009

(c)

Entries 9531Mean 0.0149

RMS 1.309

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nu

mb

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Entries 9531Mean 0.0149

RMS 1.309

(d)

Entries 9533

Mean -0.05616

RMS 0.5423

Normalized residual of point corresponding to filter 2 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

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s

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Entries 9533

Mean -0.05616

RMS 0.5423

(e)

Entries 9533Mean 0.1338

RMS 0.9077

Normalized residual of point corresponding to filter 3 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

mb

er o

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Entries 9533Mean 0.1338

RMS 0.9077

(f)

Entries 9532

Mean 0.01299

RMS 0.6756

Normalized residual of point corresponding to filter 4 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

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Entries 9532

Mean 0.01299

RMS 0.6756

(g)

Entries 9533

Mean -0.01734

RMS 0.3654

Normalized residual of point corresponding to filter 5 (in %)-5 -4 -3 -2 -1 0 1 2 3 4 5

nu

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Entries 9533

Mean -0.01734

RMS 0.3654

(h)

Entries 9533

Mean -0.01918

RMS 0.3202

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nu

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Entries 9533

Mean -0.01918

RMS 0.3202

(i)

Entries 9532

Mean -0.01425

RMS 1.29

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Entries 9532

Mean -0.01425

RMS 1.29

(j)

Entries 9533

Mean -0.07875

RMS 0.6197

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nu

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Entries 9533

Mean -0.07875

RMS 0.6197

(k)

Figure 4.12: 20k run histograms (run 130430) a) the χ2 probability, b) the offsetparameter, c) the slope and d-k) the normalized residuals (in %) for the 8 filter wheel

positions.

Page 42: Linearity Studies of the TileCal detector PMTs of ATLAS ... · PDF fileLinearity Studies of the TileCal detector PMTs of ATLAS/LHC experiment, with the Laser monitoring system by ...

Chapter 5

Linearity studies using a single

filter wheel position and different

intensity runs

In chapter 4, results of linearity studies obtained with a moving filter wheel were dis-

cussed. The data show that the point by point fluctuations are larger than the statistical

errors, producing bad χ2 probability fits. The origin of the systematic errors can be stud-

ied using a simpler data taking configuration with a single filter position and different

laser intensities. The results obtained are discussed in this chapter. Data with the filter

wheel in position 5 (no light attenuation) and 8 intensities equal to 15k, 17k, 19k, 21k,

23k, 25k, 27k and 29k were used. Selecting only points with energy between 100 - 700 pC

were eliminated the energy intervals in the region of the nonlinearity of the electronics

(<100 pC) and the energies for which the PMTs start to saturate [10] . Additionally

was removed all the PMTs flagged as having an identified bad behavior.

In Section 1, the results obtained using the LASER box PMT’s (PMT1 and PMT2)

were discussed. These results do not suffer from the light crosstalk effect. The linearity

studies performed using the photodiode 4 are presented in section 2. Sections 3 and 4

are devoted to the results obtained using the PMTs of the TileCal to normalize.

The linearity results were obtained using the scatter plots PMT signal versus the signal

of the reference counter. A typical example obtained using the PMT1 of the LASER box

is shown in 5.1. The TileCal photomultiplier and reference signals were defined as the

average of the corresponding distributions. The error is given by the ratio between the

r.m.s. of the correspondent distributions and the square root of the number of histogram

entries. Contrary to chapter 4 where the original ntuples were used and the parameters

33

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 34

calculated from the distributions, in this case they were already given by the calibration

software.

As shown in 5.1 the data are fitted using the straight line function PMT = a.Sigref +

b. Where Sigref is the normalization signal.

PMT1 signal (in ADC)

400 600 800 1000 1200

PM

T_0

sig

nal (

in p

C)

200

300

400

Figure 5.1: Example of a fit

5.1 PMTs vs PMT1

The results are shown in Figure 5.2. One can immediately see that the residuals of the

points are biased: not centered at zero as they should. The same for the offset parameter.

This indicates that there are some systematic effects that are shifting the points in some

direction affecting the fits, resulting in bad chi-squares. This effect produces residuals

that go up to 2% maximum.

The results can be explained if the PMT1 signal is not linear. Also there could be some

kind of change in the Laser system itself in a way that 2 runs with the same intensity

produce different output signals. Those hypothesis will be discussed in the next sections.

5.1.1 Linearity of the PMTs in the LASER box

The same set of runs was taken, this time with the shutter closed, so that no light passed

to the PMTs of TileCal and to diodes 2 to 4, eliminating the crosstalk on diode 1. This

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 35

Chi-square Probability

0 0.2 0.4 0.6 0.8 1

Num

ber

of E

ntrie

s

0

2000

4000

6000

8000

(a)

Offset Parameter

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

Num

ber

of E

ntrie

s

0

200

400

(b)

Slope

0 0.5 1 1.5 2

Num

ber

of E

ntrie

s

0

200

400

(c)

Normalized Residual of the point 1 (in %)

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2

Num

ber

of E

ntrie

s

0

100

200

300

(d)

Normalized Residual of the point 2 (in %)

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2

Num

ber

of E

ntrie

s

0

500

1000

(e)

Normalized Residual of the point 3 (in %)

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2

Num

ber

of E

ntrie

s

0

200

400

600

800

(f)

Normalized Residual of the point 4 (in %)

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2

Num

ber

of E

ntrie

s

0

500

1000

1500

(g)

Normalized Residual of the point 5 (in %)

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2

Num

ber

of E

ntrie

s

0

500

1000

1500

(h)

Normalized Residual of the point 6 (in %)

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2N

umbe

r of

Ent

ries

0

500

1000

1500

(i)

Normalized Residual of the point 7 (in %)

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2

Num

ber

of E

ntrie

s

0

500

1000

(j)

Normalized Residual of the point 8 (in %)

-2 -1.5 -1 -0.5 0 0.5 1 1.5 2

Num

ber

of E

ntrie

s

0

500

1000

(k)

Figure 5.2: Histograms obtained in the study PMT vs PMT1. a) the chi-squaredprobability, b) the offset parameter, c) the slope, and d-k) The residuals (in %) of the

points 1 to 8 that correspond to the intensities 14k to 23k.

one was assumed to be linear and thus used as reference. The plots PMT1/2 vs Diode

1 were produced and again the normalized residuals were calculated (Figure 5.3).

The χ2/NDF is bad (11.4 for PMT1 and 22.2 for PMT2, and chi-square probabilities

very low 10−11, 10−22 respectively) but again, the statistical errors in each point are

very small due the large number of entries. Looking at the residuals they are smaller

than 0.5% so one can assume that the linearity of the PMTs of the Laser box is adequate.

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 36

Diode 1 Signal (in ADC)

200 400 600 800

Nor

mal

ized

Res

idua

ls (

in %

)

0

0.5

(a) PMT1 vs Diode 1

Diode 1 Signal (in ADC)

200 400 600 800

Nor

mal

ized

Res

idua

ls (

in %

)

-0.5

0

0.5

(b) PMT2 vs Diode 1

Figure 5.3: Linearity of the PMTs in the LASER box

5.1.2 Comparing runs with the same intensity

To try to understand the amplitude of the fluctuations, several runs were taken at 14k

and 26k. The ratios PMT/PMT1 were computed.

PMT Signal (in pC)

216 218 220 222 224 226

PM

T_0

/PM

T1

0.3135

0.314

0.3145

(a) 14k

PMT Signal (in pC)

215 220 225 230 235

PM

T_0

/PM

T1

0.3135

0.314

0.3145

0.315

(b) 26k

Figure 5.4: Fluctuations in the Signal for the same intensity

Figure 5.4 shows the values of the ratios in the case of 14k (a) and 26k (b) intensities.

There are some fluctuations in the signal not suppressed by the ratios at the low intensity

that go to 4% for some PMTs and much smaller at higher intensities (<0.5%).

The impact of the variation of the temperature in the laser head on the linearity deter-

mination was also studied. Figure 5.5 shows that for a set of runs taken consecutively

with intensities 14k, 26k, 14k, 26k and so on, the temperature of the laser head clearly

increases with time.

The dependence of the signals in one PMT of the Tilecal (PMT0) and in the PMT1 are

shown in Figures 5.6 and 5.7 for intensities equal to 14k and 26k respectively.

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 37

Time (in minutes)

5 10 15 20 25 30 35 40 45

Tem

pera

ture

of t

he L

aser

hea

d (in

C)

24.2

24.4

24.6

24.8

25

Figure 5.5: Temperature evolution in consecutive runs

Time (in minutes)

10 15 20 25 30 35 40 45

PM

T_0

of t

he T

ileca

l sig

nal (

in p

C)

220

225

Time (in minutes)

10 15 20 25 30 35 40 45

PM

T1

sign

al (

in p

C)

690

700

710

Figure 5.6: Signals for PMT1 and PMT0 versus time for intensity 14k.

Laser head temperature (in C)

24 24.5 25 25.5 26

PM

T_0

of t

he T

ileca

l sig

nal (

in p

C)

215

220

225

230

235

Laser head temperature (in C)

24 24.5 25 25.5 26

PM

T1

sign

al (

in p

C)

700

720

740

Figure 5.7: Signals for PMT1 and PMT0 versus the temperature for intensity 26k,one can see there is a correlation here

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 38

For 26k it is clearly seen some correlation between the signals and the temperature. The

ratios also seem correlated to the temperature (Figure 5.8). The effect is less apparent at

26k because, as shown in Figure 5.7, the change in PMT1 and PMT0 are more correlated.

Time (in minutes)

10 15 20 25 30 35 40 45

PM

T_0

/PM

T1

0.3135

0.314

0.3145

(a) 14k

Laser head temperature (in C)

24 24.5 25 25.5 26

PM

T_0

/PM

T1

0.3135

0.314

0.3145

0.315

(b) 26k

Figure 5.8: Correlation between the ratios and a) time for 14k and b) the temperaturefor 26k

5.1.3 Different intensities with temperature

Going back to the runs analyzed at the beginning, it was compared the points with

different temperatures in the Laser head.

PMT1 Signal (in ADC)

400 600 800 1000 1200

PM

T_0

Sig

nal (

in p

C)

200

300

400

Figure 5.9: Linearity plot for the 1st PMT of the Tilecal

Figure 5.9 shows the scatter plot PMT0 versus PMT1. The data shows a variation of

the slope or offset around 600 ADC that seems linked to the variation in temperature

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 39

(shown in Figure 5.10). Comparing the chi-squares of the linear fit, the overall fit has

χ2/NDF=384, the blue (<600 ADC) 16 and the red (>600 ADC) 18.

PMT1 Signal (in ADC)

400 600 800 1000 1200

Tem

pera

ture

of t

he L

aser

hea

d (in

C)

24.8

25

25.2

Figure 5.10: Change in temperature along the runs

As it is unrealistic to wait for stabilization of the LASER head temperature before

taking the data, because this will take a few hours, in order to try to eliminate any

kind of systematic error coming from the LASER box, one needs to use as reference a

signal coming from somewhere after the laser box. There are two possibilities: use the

diodes after the laser box or some PMT of the Tilecal itself. Using a PMT of TileCal

as reference there could be a bias to the linearity determination because the reference

device can have the same problems of the measured PMTs. They can cancel in the ratio.

5.2 Using diode 4 as reference

In order to eliminate possible effects due to temperature variation, one can use a reference

after the laser box as well. One candidate are the diodes, that are expected to be not

so good due to the cross-talk effect. Cutting above 1800 ADC channel, so that the

saturated signals can be removed, one gets the results plotted in Figure 5.11.

Looking at the plots there is an improvement in the chi-square probability as well as the

very shifted offset parameter due to the cross-talk effect. Again, there are some small

bias in the residuals. But there is an improvement of the normalized residuals to 0.5%.

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 40

Chi-square probability

0 0.2 0.4 0.6 0.8 1

Num

ber

of e

ntrie

s

0

1000

2000

3000

(a)

Offset Parameter

0 20 40 60 80 100

Num

ber

of e

ntrie

s

0

100

200

300

400

(b)

Slope

0 0.1 0.2 0.3 0.4 0.5 0.6

Num

ber

of e

ntrie

s

0

100

200

300

400

(c)

Normalized residuals for point 1 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

500

1000

1500

2000

(d)

Normalized residuals for point 2 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

800

(e)

Normalized residuals for point 3 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

500

1000

(f)

Normalized residuals for point 4 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

500

1000

1500

2000

(g)

Normalized residuals for point 5 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

(h)

Figure 5.11: Histograms obtained in the study PMT vs diode 4. a) the chi-squaredprobability, b) the offset parameter, c) the slope, and d-h) The residuals (in %) of the

points 1 to 5

5.3 Using the 1st PMT of the TileCal as reference

Using the 1st PMT of the TileCal one gets very similar results to the previous case

with the obvious exception of the offset that no longer is that much shifted (no more

cross-talk). Again, there are some small bias in the residuals. The results are shown in

Figure 5.12.

5.4 Using the 1st PMT of the same fiber

Now, comparing only PMTs of the same fiber, one should get an improvement because

they all get the same signal regardless of the effect that signal suffered being splitted in

the optical apparatus. The results shown in Figure 5.13 were obtained using as reference

of each PMT of TileCal the first PMT belonging to the same fiber. Indeed, when the

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 41

Chi-square probability

0 0.2 0.4 0.6 0.8 1

Num

ber

of e

ntrie

s

0

1000

2000

3000

4000

(a)

Offset Parameter

-5 0 5 10 15 20 25 30

Num

ber

of e

ntrie

s

0

200

400

(b)

Slope

0 1 2 3 4 5

Num

ber

of e

ntrie

s

0

100

200

300

400

(c)

Normalized residuals for point 2 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

(d)

Normalized residuals for point 3 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

(e)

Normalized residuals for point 4 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

500

1000

1500

(f)

Normalized residuals for point 5 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

(g)

Normalized residuals for point 6 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

(h)

Normalized residuals for point 7 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

800

(i)

Normalized residuals for point 8 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

(j)

Figure 5.12: Histograms obtained in the study PMT vs the 1st PMT of the TileCal.a) the chi-squared probability, b) the offset parameter, c) the slope, and d-k) The

residuals (in %) of the points 2 to 8

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1st PMT of a fiber is used as a reference to the following PMTs in the same fiber one

gets the histograms in Figure 5.13.

Chi-square probability

0 0.2 0.4 0.6 0.8 1

Num

ber

of e

ntrie

s

0

500

1000

(a)

Offset parameter

-10 -5 0 5 10

Num

ber

of e

ntrie

s

0

200

400

600

(b)

Slope

0 0.5 1 1.5 2 2.5 3 3.5 4

Num

ber

of e

ntrie

s

0

100

200

300

400

(c)

Normalized residual of point 1 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

100

200

300

(d)

Normalized residual of point 2 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

(e)

Normalized residual of point 3 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

(f)

Normalized residual of point 4 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

500

1000

(g)

Normalized residual of point 5 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

500

1000

(h)

Normalized residual of point 6 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

800

(i)

Normalized residual of point 7 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

200

400

600

(j)

Normalized residual of point 8 (in %)

-0.4 -0.2 0 0.2 0.4

Num

ber

of e

ntrie

s

0

50

100

150

(k)

Figure 5.13: Histograms obtained in the study PMT vs 1st PMT of the fiber. a) thechi-squared probability, b) the offset parameter, c) the slope, and d-k) The residuals

(in %) of the points 1 to 8.

As shown there is a huge improvement in the parameters. The offset is, for the first

time, centered around zero, as it should be, as well as the normalized residuals. So no

bias is observed using those references. One strange thing is the presence of fits with

low chi-square probability. Looking at the residuals, this could be due to the 1st point

that has larger values than the others. Removing that point from the fit leads to the

chi-square probability shown in Figure 5.14. In this case there is a tendency (also seen

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Chapter 5. Linearity studies using a single filter wheel position and different intensityruns 43

in the previous plot) of an high chi-square probability, not flat as expected. These is

probably due to the fact that the PMTs of the same fibers are strongly correlated. The

residuals now go to 0.2% at maximum.

Chi-square probability

0 0.2 0.4 0.6 0.8 1

Num

ber

of e

ntrie

s

0

200

400

600

800

Figure 5.14: Chi-square probability excluding the 1st point

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Chapter 6

Conclusions

It was proven difficult to quantify and describe well the various methods used in the

study. This is due to the very small errors of the parameters which give always bad χ2

probabilities. Despite that, several conclusion could be drawn.

Low intensities combined with large attenuation factors produce large residuals. As the

signal is low, any small deviations from the linearity fit contribute much more than

stronger intensity signals. There is also a non linearity effect in the electronics [10] that

contributes to the non linearity observed and is responsible for the increased residuals.

From chapter 5 it seems there are many sources of systematic errors in the system

starting from the LASER box. A change in the LASER head temperature seems to

have an impact on the signal splitting produced by the splitting mirror, resulting in bad

chi-squares fit probabilities and residuals that go up to 2%. Even using Diode 4 and a

TileCal PMT, there are still some (small) bias in the results indicating there are also

some systematics in the distribution of the light in the fibers. Regardless of this bias

there is an improvement in the residuals which go up to 0.5% maximum. Those bias are

finally suppressed when we look to PMTs of the same fiber. A summary of these results

is shown on Table 6.1.

Method p0 [pC] residuals [%] mean of χ2

prob distribution

PMTs vs PMT1 ∼-10 biased and <2% 0

PMTs vs diode 4 ∼30 biased and <0.5% 0.05

PMTs vs 1st PMT of TileCal ∼5 biased and <0.5% 0.16of TileCal

PMTs vs 1st PMT ∼0 not biased and <0.2% 0.75of the same fiber

Table 6.1: Summary of the results of the various methods

44

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