the atlas pixel system architecture
DESCRIPTION
The ATLAS Pixel System Architecture. ATLAS Pixel Module: 1 Sensor 16 Frontend chips 1 Module Control Chip (MCC). Module. Stave / Disk. Control Room. How does it look like?. Connections between FE-Chips, MCC, passive components and cable through a thin kapton PCB - PowerPoint PPT PresentationTRANSCRIPT
The ATLAS Pixel System Architecture
• ATLAS Pixel Module:– 1 Sensor
– 16 Frontend chips
– 1 Module Control Chip (MCC)
Module Control RoomStave / Disk
How does it look like?
• Connections between FE-Chips, MCC, passive components and cable through a thin kapton PCB
• Active area = 16.4 60.8 mm2
• 16 Chips with ~ 50000 pixels of 50 400 m2 total
• Larger pixels between chips
The ATLAS-Pixelsensors
• n-in-n silicon
• 250 m thick
• Normal pixels:– 50 × 400 m2
• In interchip-regions:– Long pixels (600m)
– “Ganged” pixels
The ATLAS Pixelchips
• Chip Size: 7.4 mm × 11 mm
• 18 × 160 = 2880 Pixels
• Pixel Size: 50 m × 400 m
• Deep submicron, radiation hard
(tested up to 60 Mrad)
• 40 MHz operating frequency
• Zero suppression in every pixel
• Data is buffered until trigger arrives
• Serial control and readout, LVDS IO
• Analogue part: – ~ 40 W power dissipation / pixel– ~ 200 e noise– Amplitude measured via pulse width
(time over threshold)
The ATLAS Pixelcell
• One pixel cell: in case of a charge above threshold address and Time over Threshold are read out Zero suppression in pixel
Constant current feedback- Leakage tolerance > 100 nA- Linear decay
Analogue information- Measure hit width
Individual Adjustment of- Threshold- Feedback- Adjust ranges
ATLAS Pixelchip-history / production
• FE-I1:– Up to now 90 modules produced (90 % good modules)– Problems:
• Problems with threshold dispersion / tuning• Inefficiencies (timewalk) in interchip-regions (longer / ganged pixels)• SEU-hardness not satisfactory (numbers?)
• FE-I2:– Produced, modules built (numbers?), tested, irradiated– Problems of FE-I1 solved– Problems:
• Race condition in digital part (global register) FE-I2.1, FE-I3
• FE-I3:– Production version, production expected to start end of this year
• Module production:– Done by IZM (PbSn) and AMS (In)– ATLAS cut: Less than 150 bad pixels (0.3%) per module, less than 50 per
chip
The Module Control Chip (MCC)
• Interface between module and readout system – More or less equivalent to the pilot in our system
• Receives commands from the readout system– Slow commands (config etc.)
– Fast commands (during data taking, mainly for synchronisation issues)
– Trigger command
• Distributes commands and triggers to chips – Length of trigger can be configured from 25 – 400 ns
– Minimum distance between two triggers 125 ns
• Combines 16 individual events from the FE-chips
ATLAS Pixel Module - Block Diagram
1
15
ATLAS Pixel Module - Connections
• Command/Data Interface: 3/4 LVDS lines– DCI: Data & Command In
– DTO/DTO2: Data Out, Data Out2 optional to increase bandwidth
– CK: 40 MHz clock
• Additional connections:– 1 High voltage
– 2 Low voltages with sense-lines(?)• VDDD 2.0V for chips and MCC (0.8 – 1.5 A)• VDDA 1.7V (1.2 A)
– CK Return for synchronisation
• Backplane: Isolated
ATLAS Pixel Module - Dimensions
• Thicknesses:
Active area: 16.4 mm
Module width:22.4 mm
Module length length of active area= 60.8 mm
MCC: 180 mSensor: 250 mFE-Chips: 180 m
(+ Kapton + passive components)
Possible Arrangements
• 1-Plane setup
• Dead areas:– Beam hole 2.2 × 0.6 cm
– 2 bands of > 6 mm
• Power per plane: ~16 W
61.2 mm
• 2-Plane setup
• Dead areas:– 1 band of 12 mm
• Power per plane: ~ 8 W~ 78 mm- overlap
Design issues
• “Pigtail”– Flex cable connected to the kapton layer– Should (maybe) be designed by us, i.e. module should be delivered without– Form? (2D: routing of the lines, 3D: protection of the wire bonds)– Impedance issues, critical?– Connection: Wire bonds, soldering?
• Ceramic / PCB– One piece or hybrid / ceramic?– Backplanes can / should be isolated
Behind/close to module no circuitry is needed, only heat conductivity
– Lines impedance matched
• Readout lines– Three LVDS lines (2 two module, 1 from module)– Maybe one return clock for synchronisation– Maximum length?
• Power supply– Two power lines (per module ?)– Sense lines? (Note: digital current varies especially when module is noisy)
• Readout– Protocol – difficult to implement in CFD readout-system?
ATLAS - Systemtests
• First tests of mini-systems done:– 3 modules on a stave
– 6 modules on a partial disk
• Barrel setup (pigtail) looks close to something we could use …