the first integration test of the atlas end-cap muon level 1 trigger system

14
14/November/2002 C F NSS2002 in Norfolk, Virginia, US A 1 The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System Introduction Overview of ATLAS End-cap Muon Level1 Trigger TGC electronics (Level1 Trigger + TGC Readout) Slice Test Setup Test Results Summary Chikara Fukunaga Tokyo Metropolitan University On behalf of the ATLAS TGC electronics group

Upload: aretha-olsen

Post on 03-Jan-2016

27 views

Category:

Documents


0 download

DESCRIPTION

The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System. Introduction Overview of ATLAS End-cap Muon Level1 Trigger TGC electronics (Level1 Trigger + TGC Readout) Slice Test Setup Test Results Summary. Chikara Fukunaga Tokyo Metropolitan University - PowerPoint PPT Presentation

TRANSCRIPT

Page 1: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

1

The First Integration Test of the ATLASEnd-cap Muon Level 1 Trigger System

IntroductionOverview of ATLAS End-cap Muon Level1 TriggerTGC electronics (Level1 Trigger + TGC Readout)Slice Test SetupTest ResultsSummary

Chikara FukunagaTokyo Metropolitan University

On behalf of the ATLAS TGC electronics group

Page 2: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

2

Introduction

3 main ASICs out of total 7 have been made with full specifications. Stand-alone tests of ASICs have been finished.An overall integrated test has been required with all these ASICs in one test bed →Slice test (SLT) system.C++ based trigger simulation program has been needed and developed, and it could give the test patterns and answers to the SLT system.Integration test started in Sept.,’01, all the components have been installed in Aug.,’02.

Page 3: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

3

Overview of ATLAS End-cap Muon Level1 Trigger

M1M2 M3

Thin Gap Chamber (TGC)

1.05 η 2.70, z = ±14m

r (wire)- (strip) readout

Total 150 K channels for Trigger

Total 7 layers (M1,M2 and M3)

Low-pT Trigger, pT ≥ 6 GeV

M1(3) triplet: 2 out of 1, 1out of 2

M2(2) vs. M3(2) doublets: 3 out of 4

Hi-pT Trigger, pT ≥ 20 GeV

M1 vs. doublets (M2&M3)

Sector Logic (SL)

R- coincidence, Highest pT tracks

To Muon Central Trigger Proc. I/F

Page 4: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

4

TGC electronics (Level1 Trigger + TGC Readout)

M3

M2

M1

On detector part Off detector part

Page 5: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

5

Slice Test (SLT) Setup

Page 6: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

6

SLT Components I– PS Board & ASICs

SLB ASIC

0.35m

250K gates

Low-pT Trigger

Readout buffer

PP ASIC

0.6 → 0.35m

50K gates

Analog+digital

LVDSrx

Fine delay

Bunch Crossing ID

Trigger (Hi-pT)

Readout (SSW)

Page 7: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

7

SLT Components II - Hi-pT board & ASIC

LVDS inFrom PS board

G-link outTo SL

Hi-pT ASIC

0.35mm

80Kgates

Hi-pT trigger

Hitachi BGA

Page 8: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

8

SLT Components III – Readout System

LVDS inFrom PS board (SLB)

G-link outTo ROD

Star Switch (SSW)

Read Out Driver (ROD)

G-link inFrom SSW

FIFOSDRAM

CPU

Page 9: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

9

SLT Components IV – Software systemIntegrated control software based on the ATLAS online SW framework

SLT requires initialization and module/ASIC configuration at beginning

Run control for run start/stop Run Control GUI & Status Window

Configuration DataBase Editor Window

Page 10: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

10

SLT Results I – Trigger Part Logic

Verification of Trigger Logic (Simulation vs. HW)The same trigger hit patterns used for the simulation were inputted to PPG (pulse Pattern generators), and compared outputs of the SLT system with one of the simulation:

Generated Trigger Hit patterns, and comparison with the simulation

1 track (~20000) → No error found.

2 tracks (~20000) → No error found.

≥ 3 tracks (~15000) → No error found.

Page 11: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

11

SLT Results II - Trigger Latency

StageSLT

MeasurementRequired

upper limit

TGC, ASD 160 175

PP ASIC 43 50

SLB ASIC 49 75

LVDS Tx,Rx 83 75

Cable 15m 75 75

Hi-pT ASIC 55 75

G-link Tx,Rx 105 75

Cable (90m) 450 450

SL 160 175

Cable (5m) 25 25

Total 1205 1250

Latency Measurement =Actual Measurement(PS board, HiPT and SL) ANDCable length Estimation

1205ns (SLT) < 1250ns (RUL)

Page 12: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

12

SLT Results III – Readout test

Since SSW has been delivered in this summer, full test of PS-board→SSW→ROD has not been done.

PS-board→PT4(SSW alternative)→ROD has been checked in 2001 with long run tests.

400 clock counts (40MHz) can be used for SLB or SSW readout if Level 1 rate is 100KHz. SLB uses 218 counts. If TGC occupancy is 4%, SSW needs 160 counts. SSW will not be bottle neck. (TGC Occupancy ~ 1%)

Page 13: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

13

SLT Results - ROD

ROD (Read Out Buffer) has several problems.4 bytes access to internal bus takes 0.2s.SSW No hits = 4bytesSSW Hits = 40bytes If all 13 SSWs have no hits,

14s, if all hits, 30s.One ROD with 13 SSWs

can be done with 30~70KHz (< 100KHz).We need design modification.

ROD Structure

Page 14: The First Integration Test of the ATLAS End-cap Muon Level 1 Trigger System

14/November/2002 CF

NS

S20

02 in

Nor

folk

, Vir

gini

a, U

SA

14

Summary

Block Test Status

Trigger PartIntegration@40MHz Done, pattern check OK

Latency OK 1205s<1250s

Readout Part

Integration Not yet, stand-alone

Readout Rate SSW OK 100KHz

Readout Rate ROD 30~70KHz

SoftwareOnline DAQ OK, will be used for beam

Trigger Logic Simulation Need improvements

Control System HSC-CCI OK for config. ASIC