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Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS CAN and LMB in ATLASCAN and LMB in ATLAS
Controls in ATLAS CAN Local Monitor Box
Concept Measurements and Results Future
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Hierarchical levels of DCSHierarchical levels of DCS
Supervisor Leveloperator console shift operator, sub-system expertserver data base, DAQ, External system
Subsystem control levelLocal Ctrl Station Gas, HV, endcap
SCADASCADA--------------------------------------------------------------------------------Device Control FE I/OFE I/O
stand-alone system alignment, gas analyserFieldbus node chamber, power supplyPLC cooling, gas mixer
Sensors, actuators
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Requirements I/O systemRequirements I/O system
Radiation (1011 neutrons/cm2 over 10 years outside of calorimeter) analogue effects (e.g. loss of gain) Single Event Upset (e.g. program corruption)
Magnetic field (1.5T in Muon, 0.1T electronics) Access restriction I/O points distributed over whole detector volume
( up to 100m distances) Standardized connections to SCADA
HW: CAN, LAN SW: CANopen, OPC, TCP/IP
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
CAN FieldbusCAN Fieldbus
Reasons for selecting CAN: robust excellent error detection and recovery open cheap good industry support (chips, products) CERN recommendations
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Applications of CANApplications of CAN
Classes of applications: Subdetector specific developments
TileCal (Clermont-Ferrand, Barcelona) Muon (NIKHEF)
Industrial instrumentation with CAN interface electronics crates power supplies (HT, LT)
General purpose modular system LMB industrial modules
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Local Monitor Box (LMB)Local Monitor Box (LMB)
Reasons for development of LMB: radiation tolerance operation in magnetic field electrical characteristics (isolation, grounding) high channel density packaging lowest possible power high production volume (price) common SCADA SW, only configuring needed
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
LMB Design FeaturesLMB Design Features Radiation Tolerance
selected COTS over-design performance, allow for degradation operate components at lower values than specified install at protected and accessible places replace after n years
Operation in magnetic field no coils, chokes, transformers, DC/DC remote power
Limited access remote diagnostics remote loading of programs and reset
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Concept of LMBConcept of LMB
Modular system made out of building blocks CAN node I/O unit (e.g. ADC, bit I/O) signal conditioning (e.g. range, excitation current) add-on features (e.g. interlocks)
Different packaging (e.g. stand-alone, plug-on board, embedded on existing PCB)
Prototyping in ATLAS (in collaboration with sub-detectors), production in industry
Standard industrial interface (CAN/CANopen)
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
LMB block diagramLMB block diagram
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Block diagram CAN nodeBlock diagram CAN node
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
LMB Front-end PT100 boardLMB Front-end PT100 board
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
LMB housingLMB housing
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
LMB modulesLMB modules
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Implementation of LMBImplementation of LMB
Prototype series produced (40 + 100 modules) and given to all ATLAS sub-detectors ( + others)
Existing building blocks: CAN controller module front end I/O board
multiplexed ADC 16+7 bit, 16-64 channels digital I/O ( in preparation)
signal adaptation board PT100 (4-wire connection) PTx, NTC (2-wire connection) (LAr, BNL) voltage, current adapters
interlock circuit (Pixel, Wuppertal)
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Radiation tests in TCC2Radiation tests in TCC2
Objectives:•long-term stability of operation in a radiation environment•behavior of components e.g. opto-couplers, EEPROM
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Radiation test opto-couplersRadiation test opto-couplers
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Radiation measurement resultsRadiation measurement results
Opto-couplers critical choose different type increase circuit gain
Multiplexer problem at 50Gy Current increase of micro-controller at 200 GY 3 memory corruptions in SRAM (SEU)
==> more tests needed at well-known conditions (particle type, energy spectrum)
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Pixel Cooling PrototypePixel Cooling Prototype
Hardware set-up: 400 temperature sensors 64 other ADC channels (flow, pressure, etc) Feedback loops (ADC, DAC) use LMB for ADC, industrial CAN modules for
other functions
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Pixel cooling measurementPixel cooling measurement
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Pixel cooling measurementPixel cooling measurement
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
LAr Precision Temperature LAr Precision Temperature MeasurementMeasurement
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
LAr Precision Temperature LAr Precision Temperature measurementmeasurement
PRT and PT5 10/7 1998
90.04
90.05
90.06
90.07
90.08
90.09
90.10
90.11
14:33 14:43 14:53 15:03 15:13 15:23
Time (h)
Tem
pera
ture
(K) PRT
PT5
PRT- PT5Mean = -3.1 mKStdev = 0.9 mK
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
LAr Precision Temperature LAr Precision Temperature measurementmeasurement
0
100
200
300
400
500
600
-10 -8 -6 -4 -2 0 2 4 6 8 10 12 14 (mK)
Freq
uenc
y
Date: 21 July 1998Time: 15:00 to 24:00hSample period: 30sSensors: PTR and PT5MEAN = 1.0 mKStdev = 1.2 mK
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Performance and features of LMBPerformance and features of LMB
Resolution 16 bit usable (0.8mK) absolute accuracy 4*10-5 (3mK) long term stability 50ppm over one month radiation tolerance looks achievable
weak components eliminated more tests to be done
works in magnetic field (0.9T) in-field programmable CAN standard (device profile?) low cost (2US$ per ADC channel)
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
Future LMB developmentsFuture LMB developments
Additional I/O module types: Digital I/O DAC Bus converters (e.g. JTAG, I2C) Dedicated functions with custom programs in
micro-controller
Workshop on PLCs and Fieldbusses, November 26th 1999, H.J.Burckhart
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ATLASDCS
SummarySummary
CAN fieldbus is ATLAS’ standard to connect SCADA system to I/O system
LMB concept very suited for distributed DCS Modularity Necessary performance has been achieved Projected price is “very reasonable” LMB adopted as baseline by ATLAS’ subdetectors
(also being tested by non-ATLAS groups, more users welcome)