Beam%20Test%20Result%20of%20the%20ATLAS%20End-cap%20Muon%20Level-1%20Trigger - PowerPoint PPT Presentation

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Beam%20Test%20Result%20of%20the%20ATLAS%20End-cap%20Muon%20Level-1%20Trigger

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Beam Test Result of the ATLAS End-cap Muon Level-1 Trigger Chikara Fukunaga Tokyo Metropolitan University On behalf of ATLAS TGC electronics group – PowerPoint PPT presentation

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Title: Beam%20Test%20Result%20of%20the%20ATLAS%20End-cap%20Muon%20Level-1%20Trigger


1
Beam Test Result of the ATLAS End-cap Muon
Level-1 Trigger
  • Chikara Fukunaga
  • Tokyo Metropolitan University
  • On behalf of ATLAS TGC electronics group

2
Beam Test at CERN SPS H8
  • Most of the main (prototype or final) electronics
    components of ATLAS End-cap Muon Level 1 system
    have been constructed.
  • Slice test system worked (LECC2002), and results
    looked OK
  • Muon beam of about 100 GeV with 25ns bunched mode
    was available (May and September 2003)
  • Confirmation of functionality of the system with
    chambers and muon
  • Integration with other ATLAS components

3
ATLAS End-cap Muon Level 1 Trigger
  • Thin Gap Chambers (TGC) with wire (r) and strip
    (f) readout
  • Level 1 Trigger and 2nd coordinate for MDT muon
    measurement
  • Triplet M1Doublet M2 and M3
  • Pivot M3

4
Level 1 Signal Generation Scheme
  • Dr and Df from the straight line of IP and M3 for
    each planes
  • Low-pT with M1 alone or M2 and M3
  • High-pT with M1 (triplet) and doublets
  • R-f coincidence in Sector Logic (SL)

5
TGC electronics
Bunch Xing ID Delay adjustment (Synchronization) F
ront-end Gate Width
6
TGC setup at H8 in 2003
7
TGC electronics at H8
Hi-pT and Star Switch (SSW) On detector part 2
TGC Triplet and PS boards (On detector Part 1)
8
TGC electronics in the H8 hut
ROD, Test ROD SL, Control etc.
9
Electronics components used
  • Chamber (Triplet 32(Strip) x 24(wire), Doublet
    both 32 chan.)
  • ASD board (16ch.) x 2 PS pack
  • PS board 8 PP ASICs final design, 2 SLB ASICs
    prototype, 1 DCS x2
  • Hi-pT crate
  • High pT module (4 Hi-pT ASIC final design) x1
  • Star Switch (SSW) module x2 (FPGA based)
  • HSC
  • ROD crate(s)
  • Sector Logic for r-f coincidence (FPGA based)
  • RODs (ROD and Test-ROD alternatively) (FPGA
    based)
  • TTCvi
  • CCI
  • Cable
  • Individually shielded TP Category-5 cable from PS
    board to Hi-pT crate 10m (ATLAS15m) for LVDS
  • Optical fiber from Hi-pT crate to Sector
    Logic/ROD in the hut 150m (ATLAS90m) for G-link.

10
Test results
  • Chamber efficiency measurements
  • For finding the best synchronization condition,
    namely delay constant value set in PP ASIC
  • For this purpose we have a variable delay (PLL)
    circuit in PP ASIC in which the delay is
    adjustable in 25ns/32 precision (every 16
    channels)
  • Trigger efficiency
  • Low-pT, Hi-pT and r-f coincidence in SL
  • Validity of readout data
  • Combined run with MUCTPI for trigger and readout

11
TGC Chamber efficiencies
  • PP ASIC parameters
  • BCID
  • Delay constant (x-axis)
  • Gate Width (25,30,35ns)
  • SLB ASIC
  • Right, Center and Left bunch data readout

Triplet 1st Wire
Strip
12
TGC Trigger efficiency
  • Gate Width 30ns
  • Bunch Xing association 100
  • 99.7 trigger efficiency
  • 3 dead space from chamber supports
  • 1 spurious beam trigger
  • Efficiency of full trigger chain
    (Low-pT-Hi-pT-Rf)

13
Beam Profile Readout check
  • Readout (SSW and ROD firmware ROD/ROS software)
    system worked fine. Minor bug has been identified
    in SSW FPGA firmware, it was cured quickly.
  • Beam Profile under the (best) condition of 30ns
    Gate and 15ns Triplet delay.

14
Readout/Trigger Validity check with other
sub-detector(s)
  • TGC and MUCTPI process trigger data correctly
  • Both readout trigger data correctly

15
Conclusion
  • We have checked functionality of the TGC Level 1
    muon end-cap system with muon beam of 25ns
    bunched mode at SPS-H8
  • Confirmation of validity of design logic of main
    three ASICs (PP, SLB and Hi-pT) has been done.
  • System functionality with other sub-detectors and
    common environment (TTC, DCS) has been also
    confirmed.
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