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VMMASICfortheATLASASIC for the ATLAS …€¦ · VMMASICfortheATLASASIC for the ATLAS...

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VMM ASIC for the ATLAS VMM ASIC for the ATLAS Muon Phase 1 Upgrade Muon Phase 1 Upgrade Gianluigi De Geronimo a,b , Wenxiang Ding b , Aseem Gupta b , George Iakovidis a , Sorin Martoiu c , Venetios Polychronakos a , Emerson Vernon a a Brookhaven National Laboratory, NY, USA b Stony Brook University, NY, USA c IFIN‐HH Bucharest, Romania June 2016 ‐ FEE ‐ Krakow
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Page 1: VMMASICfortheATLASASIC for the ATLAS …€¦ · VMMASICfortheATLASASIC for the ATLAS MuonPhase1UpgradeMuon Phase 1 Upgrade Gianluigi De Geronimoa,b, Wenxiang Dingb, Aseem Guptab,

VMM ASIC for the ATLASVMM ASIC for the ATLAS Muon Phase 1 UpgradeMuon Phase 1 Upgrade

Gianluigi De Geronimoa,b, Wenxiang Dingb, Aseem Guptab, George g g g p gIakovidisa, Sorin Martoiuc, Venetios Polychronakosa, Emerson Vernona

a Brookhaven National Laboratory, NY, USAb Stony Brook University, NY, USA

c IFIN‐HH Bucharest, Romania

June 2016 ‐ FEE ‐ Krakow

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Outline

• New Small Wheel

• NSW Front‐End Electronics

• The VMM ASICThe VMM ASIC– Analog Front‐End

Digital Back End (Level 0 Processor)– Digital Back‐End (Level‐0 Processor)

• Conclusions

2

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ATLAS Muon Spectrometer at LHCmuon barrel stations

ATLAS Detectormuon barrel stations

muon inner stations"small wheels"

muon middle station

3muon outer stations

"endcap"

muon middle station"big wheels"

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New Small Wheel• Current small wheel only provide rough tracking and no trigger capability• Current small wheel only provide rough tracking and no trigger capability

Trigger only relies on big wheel   →   false tracks, significant physics loss

N ll h l (NSW) i i d i i ki hi h• New small wheel (NSW): triggering and precision tracking at high rate

big wheel

small wheelnew small wheel

4

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NSW Detector TechnologiesTwo kinds of high‐rate capable large‐area gas detectorsg p g g

4                           44        4

sTGCsmall‐strip Thin Gap Chamber

MicroMegasMicro‐Mesh Gaseous structure

• Primary trigger detector (pads/strips) • Primary precision trackerPrimary trigger detector (pads/strips)• Combines pads, strips, wires (~3mm pitch)• Angular resolution < 1 mrad (strips)• Redundant position resolution (strips, wires)4 4 t id l f l l

Primary precision tracker• Strips (~0.5mm pitch)• Position resolution < 100 µm• Redundant triggering4 4 i id l

5

• 4 + 4 outside layers for long lever arm• 400,000 electronics channels

• 4 + 4 inside layers• 2.1 million electronics channels

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sTGC Detector• Trigger

• pad signal selects strip region• selected strips sent for trigger

• Tracker• combines strips and wirescombines strips and wires

sTGC Signalwires sandwiched between 2 cathode planesbetween 2 cathode planes

Ion tail currentFE Electronics Requirements

• 1 MHz/channel• Fast processing P=25ns • Recovery < 200 ns (< 1µs at 50pC)

6

• Positive or negative charge• DC or AC coupling• Charge 50pC, linear to 2pC

• Capacitance up to 2nF• Resolution < 1fC at 200pF• Signal tail suppression

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MicroMegas Detector

ionization/drift

amplification

MicroMegas Signal

FE Electronics Requirements

7

• Accurate charge & time measurements• Group trigger• Good collection P=100‐200n

• Charge up to 250fC, negative• Capacitance 50‐300 pF• Resolution < 0.5 fC at 200pF

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NSW Front‐End Electronics ArchitectureFour ASICs

ART

Four ASICs(1 mixed‐signal, 3 digital)

TDS

VMMTDS

8

ROC

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VMM3 Architecture and Functionality

logic

orSETT, SETB

ARTCKART

TDS (ToT TtP PtT PtP 6bADC)64 channels

D1/flagCA shaper

logic

6‐b ADC

10 b ADCpeak

TDS (ToT, TtP, PtT, PtP, 6bADC)CK6B

IN/ ag

D2PDOTDO

12‐b BC

10‐b ADC

8‐b ADCtime4X FIFO

mux

MO

L0

addr.

Gray countlogic

CKTK/L0pulser

trim

bias registersCKTP

tempDAC ENA/softresetprompt

registers CKDT

TKI/BCR/OCRgCKTP prompt

SCK, CSSDI, SDO

TKI/BCR/OCR

SLVS 1.2V CMOSANALOG LVDS bi‐dir

CKBC

9

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VMM3 Layout

s

µm Mixed‐signal cessor

Mixed‐signal: ~ 5.2 M transistors tran

sistors

8384

g

L0 procg

: ~ 5.2 M

 tL0

~ 15308 µmµ

10L0 processor digitally implemented

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Analog Front‐End(simulations)

11

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Response to ‐Current vs Cdet

Qdet 2pCGain 0 5mV/fCGain 0.5mV/fC

plitu

deam

p

2pF, 20pF, 200pF, 2nF

Att ti t 2 F 25 t i d ithi 8%

time

• Attenuation at 2nF, 25ns contained within 8%• Peaking time increase at 2nF contained within 6ns

12

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sTGC Signal Simulation ‐ Detail

6pC

arge

rent

charge

cha

curr

g~ 50% in 200ns

current~ 25% in 25ns

Simulation of 6pC signal to 1µs

Ab t 25% d 50% f h ll t d i 25 d 200 ti l

time

• About 25% and 50% of charge collected in 25ns and 200ns respectively

13

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Response to sTGC‐Currents

delta Qdet 2pC & 6pCC 200 Fe Cdet 200pFGain 0.5mV/fC

amplitu

d

sTGC

tail

• The response to the sTGC current exhibits an increase in peaking time

time

• The response to the sTGC current exhibits an increase in peaking time of about 13ns and a tail extending to some µs – discrimination an issue• No saturation with 6pC sTGC signals up to 6pC (expected average)14

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BLH Modified for Tail SuppressionBLH Circuit

low‐frequency filterBLH Circuit

non‐linear stage

signal                    ref

programmable tail suppressor

• The BLH is programmable: along with the unipolar response mild• The BLH is programmable: along with the unipolar response, mild and strong tail suppressions are available

15

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Tail Suppressor with sTGC‐Currents

Qdet 6pCCd t 200pFe Cdet 200pFGain 0.5mV/fC

amplitu

d

strong mildnone

strong

• Impact of the tail suppressor on sTGC‐currents, with a return below

time

Impact of the tail suppressor on sTGC currents, with a return below threshold within 200ns and full baseline return in less than ~ 600ns

16

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High Rate Events ‐ DC Coupled Sensor

analog output, Qdet=6pC, 1MHz charge amplifier output

ude

ude dc baseline

amplitu

amplitu

negative chargepositive charge

dc baseline

• A stable baseline can be observed at the analog output

timetime

A stable baseline can be observed at the analog output• For dc‐coupled sensor, a baseline shift occurs at the output of the charge amplifier, with polarity equal to the signal17

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High Rate Events ‐ AC Coupled Sensor

analog output, Qdet=6pC, 1MHz charge amplifier output

dc baselineude

ude

positive chargeamplitu

amplitu

negative charge

t ~ RDETCAC

dc baseline

• For ac‐coupled sensor, after the initial baseline shift of the same

timetime

For ac coupled sensor, after the initial baseline shift of the same polarity, a second shift of opposite polarity occurs due to the zero net charge (zero‐area ...) with potential for long‐term saturation18

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Additional Front‐End Circuits

• Dynamic discharge circuit (DDC): combines both polarity resets to contain baseline shifts for high‐ratepolarity resets to contain baseline shifts for high rate operation with AC coupled sensors.

F t i it (FRC) id f t di h• Fast recovery circuit (FRC): provides fast discharge for very high charge events to guarantee recovery within ~1µswithin  1µs.

b k l d‐ see backup slides ‐

19

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ENC at Maximum Gain

Unipolar ResponseGain 16mV/fCEN

C

positive chargenegative charge

25ns

10k200ns

~10e‐/pF~10e /pF1k

1nF100pF capacitance

20

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Digital Back‐End(L l 0 P )(Level‐0 Processor)

Sorin Martoiu, IFIN‐HH Bucharest

21

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Level‐0 Processor

BC window

BC counterBC clock

L0 trigger

LAT. FIFO (64)

LAT. FIFO (64)

LAT. FIFO (64)

L0 CH FIFO (16)

L0 SEL

L0 SEL

L0 CH FIFO (16)

L0 CH FIFO (16) UILD

L0 SEL

LAT. FIFO (64)

LAT. FIFO (64)

L0 SEL

L0 SEL

L0 CH FIFO (16)

L0 CH FIFO (16)

EV BU

BCID FIFO (32)

Latency FIFO takes data from the mixed‐signal front‐end• FIFO designed to accommodate 4 MHz data in a 10 µs latency window• 20‐bit data: threshold, amplitude (ADC), timing (ADC)20 bit data: threshold, amplitude (ADC), timing (ADC)

22

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Level‐0 Processor

BC window

BC counterBC clock

L0 trigger

LAT. FIFO (64)

LAT. FIFO (64)

LAT FIFO (64)

L0 CH FIFO (16)

L0 SEL

L0 SEL

L0 CH FIFO (16)

L0 CH FIFO (16) UILD

L0 SEL

LAT. FIFO (64)

LAT. FIFO (64)

L0 SEL

L0 SEL

L0 CH FIFO (16)

L0 CH FIFO (16)

EV BU

BCID FIFO (32)

At L0 trigger builds BC trigger window and selects data for the L0 CH FIFO• flushes old data• fills non valid data as needed (for simultaneous overflow)• fills non‐valid data as needed (for simultaneous overflow)• builds BCID FIFO

23

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Level‐0 Processor

BC window

BC counterBC clock

L0 trigger

LAT. FIFO (64)

LAT. FIFO (64)

LAT FIFO (64)

L0 CH FIFO (16)

L0 SEL

L0 SEL

L0 CH FIFO (16)

L0 CH FIFO (16) UILD

L0 SEL

LAT. FIFO (64)

LAT. FIFO (64)

L0 SEL

L0 SEL

L0 CH FIFO (16)

L0 CH FIFO (16)

EV BU

BCID FIFO (32)

B ild tBuilds event• BCID followed by valid data with address• header• event built in < 1µs• event built in < 1µs

Sends data through two data links (DDR, 640MB/s)`24

Page 25: VMMASICfortheATLASASIC for the ATLAS …€¦ · VMMASICfortheATLASASIC for the ATLAS MuonPhase1UpgradeMuon Phase 1 Upgrade Gianluigi De Geronimoa,b, Wenxiang Dingb, Aseem Guptab,

Conclusions and Future Work• VMM: front end ASIC for NSW in ATLAS Muon P1 upgrade• VMM: front‐end ASIC for NSW in ATLAS Muon P1 upgrade

• programmable options and functions for all pads, strips and wires insTGC and MicroMegas detectors (2.6 million channels total)

• combines mixed‐signal and digital design implementations•moves in the direction of System‐on‐Chip (SoC)• 64 channels, 160kMOSFETs/channel64 channels, 160k MOSFETs/channel• interfaces to 3 digital ASICs (TDS, ART, ROC)• sub‐fC and sub‐ns resolution at 200 pF, 25 ns

l i l i i i i l i l ADC d d h•multiple trigger primitives, multiple ADCs and data paths• VMM3 is being fabricated, aims at pre‐production

CERN and the ATLAS CollaborationNachman Lupu (Technion Haifa Israel) ‐ Lorne Levinson & team (Weizmann Inst Israel)

Acknowledgment

25

Nachman Lupu (Technion Haifa, Israel)  ‐ Lorne Levinson & team (Weizmann Inst., Israel)Ken Johns & team (Univ. Arizona, USA)   ‐ Jay Chapman & team (Michigan Univ., USA)Paolo Giromini & team (Harvard, USA)  ‐ John Hobbs, Chris Bee (Stony Brook, USA)Jon Kotcher, Alessio D’Andragora, Lin Yao, (BNL, USA)

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Backup SlidesBackup Slides

26

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Path Towards VMM

VMM1 (2012)50 mm²

VMM2 (2014)115 mm²

VMM3 (2016, in fabrication)130 mm²

500k MOSFETs(8k/ch.)•mixed‐signal

h d

> 5M MOSFETs (>80k/ch.)• planned deep re‐design of VMM1•much higher functionality and 

l it th VMM1

> 10M MOSFETs (>160k/ch.)• deeply revised front‐end for sTGC• L0 processorSEU l• 2‐phase readout

• no ADCscomplexity than VMM1• continuous fully‐digital readout• ADCs

• SEU‐tolerant• SLVS interface• additional functions• aims at pre‐productionsTGC specifications finalized

27

• aims at pre‐productionsTGC specifications finalized 

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Analog Front‐EndBLHBLH

bias

test

CA1 CA2 CA3 SH1 SH2 SH3

~ 4mm

• Programmable polarity and injection capacitor• Three‐stage charge amplification with programmable gain• Three‐stage shaping amplifier (DDF) with programmable peaking timeg p g p ( ) p g p g• Programmable baseline stabilizer (BLH)

28

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sTGC Signals Specifications"make sure that the signal tails in the cathode readout are properlyincorporated into the simulation"[G. Mikenberg]

"for charges larger than 6 pC thefor charges larger than 6 pC the dead time increases and estimated to reach ~1 usec for 50 pC"[V. Polychronakos]

Design guidelines• accurate tail model• 6pC average

Design guidelines• accurate tail model• 6pC average• 60pCmax• 1MHz• 2nF

• 60pCmax• 1MHz• 2nF• analog recovery as fast as possible• analog recovery as fast as possible

29See also “sTGC analog requirements”: https://edms.cern.ch/document/1536160/1

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sTGC Signal Simulation

charge ~ 95% in 12µs6pC

arge

rentg

~ 60% in 1.3µs

µ

cha

curr

Simulation of 6pC signal to 20µscurrent

• About 60% and 95% of charge collected in 1 3µs and 12µs respectively

time

• About 60% and 95% of charge collected in 1.3µs and 12µs respectively

30

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Dynamic Discharge Circuit (DDC)negativeReset negativeReset

reset dynamic d h

bias

test

resetdischarge

• The dynamic discharge circuit (DDC) option combines the negative 

positive

y g ( ) p g(used in negative charge mode) and positive (used in positive charge mode)  reset in a single stabilizing circuit. The pole‐zero cancellation is fully preserved This circuit introduces a small increase in parallel noisefully preserved. This circuit introduces a small increase in parallel noise (~200 e‐ at 200ns). 

31

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AC Coupling with DDC

analog output, Qdet=6pC, 1MHz charge amplifier output

dc baselineude

ude

positive charge

dc baseline

amplitu

amplitu

negative charge

dc baseline

• For ac‐coupled sensors the charge amplifier output shift is contained

timetime

For ac coupled sensors the charge amplifier output shift is contained by the DDC.

32

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Response to Very High Charge

analog output charge amplifierlit

ude

litud

e

Qdet 10pC to 60pC 60pC

poutputam

p

amp

Cdet 200pFGain 0.5mV/fC

60pC10pC

10pC

timetime

• Saturation of the charge amplifier extends to 2µs at 20pC and 6µs

p timetime

Saturation of the charge amplifier extends to 2µs at 20pC and 6µs at 60pC• Similar behavior is obtained for positive charges

33

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Fast Recovery from High Charge

Front‐End AmplifierFRC

A       B

Th f t i it (FRC) t ti t t t lifi• The fast recovery circuit (FRC) senses saturation state on two amplifier nodes (A, B) and enables a current source connected to the input node34

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Response to Very High Charge with FRC

charge amplifieritu

de

itude analog output

Qd 10pC to 60pC60pC

poutput

ampl

ampl

Qdet 10pC to 60pCCdet 200pFGain 0.5mV/fC

60pC10pC10pC

•With the fast recovery circuit enabled, the saturation of the

10pC timetime

With the fast recovery circuit enabled, the saturation of the charge amplifier is reduced to 1.2µs at 20pC and 2µs at 60pC• Similar behavior is obtained for positive charges

35

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Input Node Stability at Saturation

analog output charge amplifieritu

de

itude

Qd 10pC to 60pC

pinput

ampl

ampl

Qdet 10pC to 60pCCdet 200pFGain 0.5mV/fC

60pC 40mV

60pC10pC

• At 60pC the input voltage of the charge amplifier exhibits a short

10pC timetime

At 60pC the input voltage of the charge amplifier exhibits a short pulse of ~40mV. The virtual ground is recovered within 2µs• Similar behavior is obtained for positive charges

36

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ENC at Minimum Gain

Unipolar ResponseGain 0.5 mV/fC

positive chargenegative charge

25nsENC

200ns

1nF100pF capacitance

37

Page 38: VMMASICfortheATLASASIC for the ATLAS …€¦ · VMMASICfortheATLASASIC for the ATLAS MuonPhase1UpgradeMuon Phase 1 Upgrade Gianluigi De Geronimoa,b, Wenxiang Dingb, Aseem Guptab,

ENC at Minimum Gain ‐ sfm/sbip

Tail‐Cancellation & Dynamic‐Discharge Response EnabledGain 0.5mV/fC

positive chargenegative charge

25ns

ENC

200ns

1nF100pF capacitance

38


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