Introduction Construction, Integration and commissioning on the surface Installation and...

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Introduction Construction, Integration and commissioning on the surface Installation and commissioning after installation in the cavern Selected performance results from test-beams Some results from cosmics data analysis The ATLAS Liquid Argon Calorimeter: Construction, Integration, Commissioning Ph. Schwemling on behalf of the ATLAS LAr Group

Transcript of Introduction Construction, Integration and commissioning on the surface Installation and...

• Introduction• Construction, Integration

and commissioning on the surface

• Installation and commissioning after installation in the cavern

• Selected performanceresults from test-beams• Some results from

cosmics data analysis

The ATLAS Liquid Argon Calorimeter:

Construction, Integration, Commissioning Ph. Schwemling on behalf of the

ATLAS LAr Group

The ATLAS Detector

The ATLAS Liquid Argon Calorimeters

endcap A endcap Cbarrelendcap A endcap Cbarrel• LAr Calorimeters:– EM Barrel : (||<1.475) [Pb-LAr]– EM End-caps : 1.4<||<3.2 [Pb-LAr]– Hadronic End-cap: 1.5<||<3.2 [Cu-LAr]– Forward Calorimeter: 3.2<||<4.9 [Cu,W-LAr]

• ~190K readout channels

46 m13 m

4.5 m

The ATLAS Electromagnetic (EM) Calorimeter

• 2 wheels (16 modules) in the barrel and 1 wheel (8 modules) per endcap

• Accordion shape in EM barrel and end cap calorimeters (>22X0)

• Main advantages– LAr as act. material inherently linear– Inherently radiation hard– Hermetic coverage (no cracks)– Longitudinal segmentation– High granularity (Cu etching)– Fast readout possible

tdrift =450 ns

E

The ATLAS Forward and Hadronic Calorimeters

FCAL1 Anode Structure

FCAL End View

LAr gap FCAl 1/2/3: 250/375/500 µm

• Forward Calorimeter (FCal)– 3 wheels per endcap (10)

• Cu matrix for the first wheel (2.6, 28X0)• W matrix for the other two wheels (2x

3.7)• Hadronic Endcap Calorimeter (HEC)

– 2 wheels per endcap (10), 32 modules each

• Cu absorbers (25mm/50mm thick)• Each gap consists of 4 sub gaps of

1.85mm

HEC module

Physics requirements

• Discovery potential of Higgs determines most of the performance requirements for the EM calorimetry

• Largest possible acceptance• Large dynamic range : 20 MeV…2TeV ( 3 gains,

12bits)• Energy resolution (e±γ): E/E ~ 10%/√E 0.7%

precise mechanics & electronics calibration (<0.25%)…

• Linearity : 0.1 % (W-mass precision measurement) presampler (correct for dead material), layer

weighting, electronics calibration• Particle id: e±-jets , γ/π0 (>3 for 50 GeV pt)

fine granularity• Position and angular measurements: 50 mrad/√E

Fine strips, lateral/longitudinal segmentation • Hadronic – Et miss (for SUSY)

– Almost full 4π acceptance (η<4.9)• Jet resolution

E/E ~ 50%/√E 3% η<3, E/E ~ 100%/√E 10% 3<η<5

• Speed of response (signal peaking time ~40ns) to suppress pile-up

• Non-compensating calorimeter granularity and longitudinal segmentation very important to apply software weighting techniques

Jets

Jets,Missing Et

Electrons Photons

Construction

HV and electrical testsafter module assemblyRepair of abnormalchannels

Mechanical measurementsduring production/assembly:•Stability at 1% level•Resulting constant term 0.5%

Integration• Delivery of 3 cryostats and preparations of cryostats

at CERN starts in 2002• Module production in institutes and delivery to CERN

from 2001 – 2004• Wheel assembly in clean rooms from 2002 – 2004• Wheel insertion into cryostats from 2003 – 2004• Cold tests on the surface in 2004 – 2005

Barrel wheel inside cryostatModule construction in the labs

EM EndCap A wheel after its insertion, cabling finished, July 2004

Cold Commissioning on the Surface

• All three cryostats were commissioned at LAr temperatures (88K) filled with LAr on the surface (cold commissioning)

• The goal of the cold commissioning was to :– Check the connectivity and integrity of the connections and all

the detector channels and calibration lines at LAr temperatures– Test the integrity of all HV channels at nominal voltage at LAr

temperatures– Measure electronics parameters needed for signal reconstruction– Measure the noise and coherent noise (with ATLAS electronics

boards)• The barrel commissioning lasted 10 weeks in summer 2004• The end cap C commissioning lasted 8 weeks in winter 2005• The end cap A commissioning lasted 6 weeks in summer 2005• Number of channels to be tested on all three subdetectors:

– 190304 read out channels– 14592 calibration lines– 4248 HV channels

Cold Commissioning – Tests

• Applying High Voltage– Slow ramp up (measure current draw)– Stability test during several weeks

• HV continuity tests (EM and FCal only):– AC signal applied on the HV line– Via the detector capacity a signal is induced

on the signal cables– Checks connectivity of the HV and signal lines

To FE elec.

Calib. signalRcal

• Pulsing all lines with the calibration board, and reading pulses back with the front end boards

• Reflectometry measurements

• LC, Rcal measurements (EM)

– Measure these parameters at cold

– Used in the calibration run analysis

• Tests of the final Front-End-Crate electronics

– Noise measurements

Few (<1‰)abnormalchannels

0.1-0.2 % amplitudestability over onemonth

Cold Commissioning Test Summary

Signal &

Calibration

Bad channels (#|%)

Bad calibration lines (#|acc.

%)

Dead channels

(#|%)

EMEC C 40 | 0.13 1 | 0.04 6 | 0.02

HEC C 3 | 0.11 3 | 0.37 3 | 0.11

FCal C 10 | 0.70 0 | 0.00 0 | 0.00

EMEC A 20 | 0.06 4 | 0.16 8 | 0.03

HEC A 0 | 0.00 1/3 | 0.8 3 | 0.11

FCal A 9 | 0.63 0 | 0.00 0 | 0.00

EM Barrel

49 | 0.04 1 | 0.01 31 | 0.03

HV

Correction needed

(HV#|acceptan

ce%)

Dead (HV#|

acceptance%)

EMEC C 25 | 5.00 0 | 0.00

HEC C 12 | 7.50 0 | 0.00

FCal C 8 | 1.80 0 | 0.00

EMEC A 35 | 8.75 1 | 0.25

HEC A 13 | 8.10 0 | 0.00

FCal A 11 | 4.19 0 | 0.00

EM Barrel 8.5 | 1.90 0 | 0.00

Situation in April 2006

> 99.7% of the detector

channels work!

» 99.9% of detector channels

work!

•Since then, some of the HV problems repaired by « burning » shorts•ECC had to be emptied. When refilling, changes may appear•Final list of problematic channels being prepared now.

Commissioning After Installation

• As soon as the front end boards are installed in the cavern and connected to the ATLAS read out system regular calibration runs are recorded

– Injection of a calibration pulse (via the Rcal) on the detector module inside the cryostat, and reading it back with the whole read-out chain

– Allows to check the integrity of all connections, the status of the detector cells and the functioning of the read out chain and the calibration system

Calibration pulse shapes for some FEB (one plot per front end board, each 128 channel)

Am

plitu

de (

AD

C

cou

nts

)

Time (ns)

AD

C

Linearity of one calibration channel

DAC counts

(AD

C-l

inear

fit)

/600

DAC counts

Ramp run pulsing 3 barrel modules

Gaining practical experience : cryogenics

Small temperature variationsunderstood by cryo team.

• Comparison of 3 runs (1 per month)• Observe excellent stability of the maximum

amplitude (calibration runs) and the baseline – Maximum amplitude stable to 0.14% – Pedestal variations below 0.05 ADC counts (<0.1MeV)

Gaining practical experience :Read-out stability

•Located at CERN, H8 (barrel) and H6 (end-cap)beam-lines.Electron beams from 10 to 300 GeV•4 Barrel modules (out of 32 total),3 End-Cap modules (out of 16 total)tested between 2000 and 2002.

•Topics studied•Position resolution, γ/π0 separation•Response to muons•Time resolution•Uniformity, linearity, energy resolution

Production testbeam

Calorimeter response to muons

Middle Strips

Time resolution of theLArg calorimeter

E beam

Linearity for electrons

Erec=λ(off+w0E0+E1+E2+w3E3)

•4 parameters, dependant•Simple method

χ2=Σ(Eirec-Eitrue)2i

2

Resolution for electrons

End-cap combined testbeam 2004

Understand high (2.5-4.9) region

Cosmic ray data

Cosmics commissioning goals

• Exercise Front-End electronics and readout chain

• Look for dead/bad cells• Check/adjust detector

timing at ns level• Check cell response

uniformity at 1-2% level

Commissioning with cosmics

1 2

3 4

A

B

)41(

4 SD

4 SD8 trigger cables, more if LAr technicians

Typically 15 k events overone week2% events projectiveS/B about 10 in middle sampling

Individual cellsignal

Projective muonsenergy deposit(middle sampling)

Predicted physic pulses vs data

Typical pulses with GeV energy deposit (same as for 5 samples)

Fair qualitative agreement in the peak and in the undershoot for every layer

25 samples

E = 3.8 GeVFront, η ~ 0.23

FT7; Slot3; Ch72Run 24606

Back, η ~ - 0.03

FT1; Slot9; Ch64Run 24606

E = 17.0 GeVMiddle, η ~ - 0.04

FT1; Slot11; Ch5Run 24606

E = 6.3 GeV

Predicted physics pulses vs data

Correlating LAr Time and Tile Time

FEB: Side A (1), FT 23, Slot 12

• Tile time is the time at the y = 0 crossing. A time-of-flight to the LAr cell correction is made.

• Slope consistent with 1 to ~5% with intercept values ~ 2ns. After fixing slope, intercept decreased to just under ~ 1ns.

Correlating LAr time and Tile time

• Spread of data about linear fit in previous slide represents combined LAr-Tile resolution. Width of TLAr - TTile distribution quantifies the resolution.

•Resolution goes as the inverse of the energy - separate into bins of LAr cell energy.

• Fit to quadrature sum of E-1 term and constant term. Res agrees with test beam, Const substantially larger (TB, 0.65 ns). to be understood

Timing resolution with cosmics

•Plot MPV of muon Landau distribution as a function of . •Shape of various clustering methods agree well with MC and the expected cell depth at the ~2% level in 0.1 bins. The results use ~ 10k clusters.

• A naïve statistical extrapolation suggests ~160k clusters necessary to probe depth in cell bins at 1% level.

* All normalized to 0.3 < < 0.4 bin

Muon response dependance over

Conclusions

All LAr calorimeters successfully integrated in their cryostats and in ATLAS, after extensive test and quality control during construction.

Excellent condition of the calorimeter (more than 99.9% of channels work), stability very good.

Cosmic muons are routinely recorded together with the hadronic Tile calorimeter, muon detector and ID system. Data used to improve understanding of the detector and prepare real data taking

The ATLAS calorimeter system will be ready in spring 2008 for the first physics data, expected in the second half of 2008 !

Spares

Calorimeters