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Spectrograph Detector

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Research School of Astronomy & Astrophysics. Critical Design Review. 19-20 ... Linearize and least-square fit to obtain photon rate. Noise Improvement = (n/12) ... – PowerPoint PPT presentation

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Title: Spectrograph Detector


1
Spectrograph Detector Hardware
2
Developments Since CoDR
  • Collaborating with IfA on NIFS detector subsystem
  • Rockwell PACE technology HAWAII-2 HgCdTe ordered
  • Designed detector mount and cryostat wiring
  • Bypassing detector internal output amplifier and
    using external output amplifier to eliminate
    amplifier glow
  • Purchased components for detector temperature
    control and demonstrated mK stability
  • Determined final configuration and ordered SDSU-2
    detector controller
  • Using Quad Channel Coadder Video Board instead of
    two Dual Channel Video Boards for IfA
    compatibility
  • Using detector reference to improve bias
    stability
  • Plan to implement digital filtering to overcome
    mux. glow

3
IfA/RSAA Collaboration
  • Collaborate on the design and characterization
  • IfA world leaders
  • Similar low dark current and noise to IfA AEOS
  • NIFS design adapted from AEOS
  • April 2002 - Science detector delivered to IfA
    for characterization
  • End July 2002 - delivered to RSAA for integration

4
Spectrograph Detector
5
Spectrograph Detector
  • PACE Technology HAWAII-2 HgCdTe ordered
  • Measure QE at 65K
  • Lower dark current (0.01e/s/pix) at 65K than 77K
  • Mount temperature sensors on Eng. and Science
    Detector
  • Need information on sensor wiring
  • No mention of AR coating
  • Still developmental
  • Reduces mux glow, fringing and ghosting off front
    of detector
  • Possible upgrade should we pursue this option

6
Detector Housing
  • Stray light shield
  • Electrically isolated to reduce noise pickup
  • Temperature controlled 60K 1K

7
Detector Mounting Board
  • Two-layer, Teflon flexi-rigid board
  • Space constraint and reduce solder joints and
    connectors
  • Cooling block 65K 1mK
  • Inner 223 non-signal pins soldered to cooling
    copper block cool detector
  • Cooling block large enough such that 2mW over 10s
    raises temperature lt 1mK

8
Detector Mounting Board Layout
  • Four mil tracks with minimum four mil spacing
  • Technology being trialed on our DBS CCD system

9
External Output Amplifier
  • Eliminate amplifier glow
  • Use J270 JFET source follower
  • For acceptable drift, J270s mounted in detector
    cooling block to stabilize temperature ( 1K)
  • Microphonic noise pickup from cyrocoolers
    possible in high impedance path from output pin
    to gate of J270 - Use rigid wiring
  • Reference improve bias stability
  • using similar circuit
  • thermally couple and match reference and signal
    J270s

Reference
10
Flex Circuits
  • Two Teflon flex circuits
  • Clocks
  • Outputs and biases
  • Grounds
  • Cold strapped by
  • Clamp to CWS at radiation shield
  • Clamp to CWS at Skirt
  • Micro D connectors to Detector Housing
  • Four mil tracks with minimum four mil spacing

11
Detector Temperature Control
Temperature Test Cryostat
DC IOC Controller
Lake Shore Temperature Controller
12
Detector Temperature Control
  • Achieve low drift ? mK stability
  • Purchased
    Lake Shore Model 340
  • Cernox CX-1080-LR sensor
  • Vishay RTO TO-220 packaged resistor
  • Demonstrated mK stability in a test Cryostat over
    days
  • Response to disturbances
  • cold strap
  • detector dissipation

13
Detector Wiring Discussion
  • Is our thermal design sufficient to obtain mK
    stability of detector?
  • Demonstrated components can achieve mK stability
  • Controlling the temperature of detector assembly
    environment
  • Wiring is sufficiently cold clamped and of high
    thermal impedance
  • Cooling block is in as close thermal contact as
    we can achieved
  • Have we done enough to eliminate microphonics as
    a problem?
  • Using rigid wiring in sensitive areas
  • Added additional vibrational isolation to
    Cryocooler mount

14
Spectrograph Detector Controller
15
Design Overview
16
Bias Stability
  • High level of bias stability is essential
  • John Barton measured HAWAII-1 signal drift
    1.5e/mK
  • gt control detector temperature to mK level
  • Rockwell has provided a reference output on the
    HAWAII-2 for drift compensation

17
Reference Circuit
  • Enabled on 1025th horizontal clock
  • Signal and reference processing circuits are made
    as similar as possible
  • Same amplifier circuit with matched FETs J270s in
    close thermal contact
  • Feed into same video channel by utilizing IfA
    Video Switch Board.
  • Take 32 samples, average and subtract as with CCD
    overscan

Signal
18
SDSU-2 Controller Stability
  • Limited by
  • video ADC ADS-937 ? 10 µV/K
  • bias/clock/video offset DAC DAC8420 ? 20 µV/K
  • Spec. is drift lt read noise 5e ? 15-30
    µV at det. gain 3.0-6.0 µV/e
  • Achieved by controller stability lt 2C over
    longest exposure
  • Relax further if reference pixel works
  • Plan to water-cooled the controller ? stability ?
    water temperature
  • Looked at WFI on 40inch for example of
    water-cooled controller
  • lt 2C over two days
  • OK if Gemini water chiller lt 2K/hr

19
Sampling Techniques
  • Implement three types
  • Double Correlated Sample
  • Fowler Sampling
  • Linear Fitting
  • Complicated by multiplexer glow

20
Multiplexer Glow
  • Mux. glows every time it is clocked
  • Affects multiple sampling - more reads, then read
    noise ? but glow ?
  • As number of reads increases, total system noise
    initially decreases, bottoms and then increases
  • Extent with HAWAII-2 unknown
  • Reduced by
  • AR coating array to stop light piping effect
    through substrate
  • Skewing the clocks
  • Overcome by digital filtering each pixel
  • Multiple ADC samples per pixel access.
  • Noise improvement ?(n)

Noise
HAWAII-1
Finger et al 2000
Digital Filtering
Total noise
Read noise
Glow
Number of Reads
21
Detector Controller Discussion
  • Will water cooling the detector controller obtain
    good thermal stability?
  • Need data from Gemini.
  • variation of water temperature with dome
    temperature at cassegrain
  • variation of NIRI jacket temperature with dome
    temperature
  • likely dome temperature variation during longest
    exposure
  • Have we done enough to achieve good bias
    stability?
  • Designed the detector temperature control system
    to achieve mK stability
  • Temperature stabilize the detector controller to
    less than 2K over longest exposure
  • Use reference circuit to compensate for drift
  • Will multiplexer glow be a problem?
  • Affects how well linear fitting will reduce noise
  • HAWAII-2 mux. designed to have less glow. Extent
    unknown
  • Overcome by implementing digital filter in all
    three sampling techniques

22
Detector Characterization
23
Characterize
  • Determine operating point
  • good QE, sufficient well depth (50ke), and
    linearity and minimizes read noise, dark current,
    and cosmetic problems
  • Bias stability
  • Check adequacy of mK detector stability
  • Measure detector controller stability
  • Determine best way to use reference
  • Multiplexer glow
  • Determine best mix of digital filtering and
    sampling method to obtain best noise performance
    for different observing situations
  • Persistence
  • Linearity
  • Fringing stability and how to flat field

24
END
25
CdZnTe MBE Technology 5µm Array
  • Possible loan of 5µm MBE Array from NGST project
  • MBE has advantages over PACE
  • lower dark current (0.01 ? 0.001 e/s/pixel)
  • eliminates persistence. (0.3-0.5 1st read, none
    thereafter)
  • higher uniform QE (60 ? 85) (CdZnTe better
    refractive index match)
  • NIFS designed to accommodate 5µm MBE Array
  • Packaging different ? redesigned of detector
    mounting

26
(No Transcript)
27
Detector Discussion
  • Information required on sensor wiring of
    temperature sensors on Eng. and Science Array
  • What is the progress of AR coating and will it be
    considered as an option?

28
Spectrograph Detector Wiring
29
Thermal Shunts
  • Notes

30
Changes Since CoDR
  • Change of SDSU-2 Video Processor Board
  • CoDR proposed two Dual Channel IR Video Board
    (Dual Channel)
  • Instead one Quad Channel Coadder Video Board
    (Coadder)
  • Reason - compatibility with IfA
  • Added IfA Video Switch Board
  • Switches between signal and reference and enables
    the same video channel to sample both reference
    and signal.
  • SDSU-2 power supply mounted and air-cooled inside
    the DC thermal enclosure instead of mounted and
    water-cooled on the Cryostat

31
Choice of Video Processor Boards
  • Dual Channel IR Video Processor Board
  • two analog signal video processing chains
  • six bias generators
  • Quad Channel Coadder Video Processor Board
    (Coadder)
  • four analog signal video processing chains
  • no bias generators
  • image-processing capability, but not useful
  • clock board provides biases

32
Comparison of Video Processor Boards
  • Identical video processing channels
  • Coadder has image processing capability, but not
    enough memory to be useful
  • Modest readout rate gt all image processing done
    in external processor
  • Coadder complex gt DSP code more complicated than
    necessary
  • IfA are developing AEOS, a spectrograph with
    HAWAII-2 , using the Coadder and will use the
    Coadder to characterize the NIFS detector
  • More compatibility with IfA gt less changes to
    IfA DSP code
  • Dual channel board has six low noise bias
    generators. The coadder will require the biases
    to be provided by the noisier clock board
  • Summary

more complicated potentially noisier
Versus
IfA compatibility
33
Bias Stability
  • High level of bias stability is essential because
  • Long integration times 3600secs
  • The way the readout is performed (multiple reads
    over full exposure time)
  • Accurately subtract fixed pattern dark current
  • Low read noise 5e, bias stability specified as
    read noise
  • John Barton measured HAWAII-1 signal drift
    1.5e/mK
  • gt control temperature to mK level
  • Rockwell has provided a reference output on the
    HAWAII-2 for drift compensation

34
Detector Circuit
35
Component Drift
  • Dominated by ADS-937 and DAC8420
  • Drift lt read noise 5e ? 15-10 µV at detector
    gain of 3.0-6.0 µV/e

 
36
Sampling Techniques
  • Implement three types
  • Double Correlated Sample
  • Signal End read - Start read
  • Bright object and background limited
  • Fowler Sampling
  • Average( n/2 End reads) Average(n/2 Start
    reads)
  • Noise improvement ?(n/2)
  • Medium length exposures
  • Linear Fitting
  • Reads at equal periods throughout exposure
  • Linearize and least-square fit to obtain photon
    rate
  • Noise Improvement ?(n/12)
  • Long exposure length

37
DSP code
  • Three Motorola 56000 DSPs
  • VME interface board
  • Timing board
  • Coadder video board
  • Two code
  • VME interface board DSP code
  • Use GMOS code as starting point
  • Add interrupts to sequence data transfer
  • Timing/coadder video board DSP code
  • Preliminary command interface document written
  • Copy IfA code after Video Switch Board tested
  • modify where necessary to suit and to add
    features such as
  • Linear fitting
  • Digital filtering

38
Grounding and Shielding
39
Grounding and Shielding
  • Adhered to good grounding and shielding practices
  • Grounding system designed
  • Minimized earth loops
  • star point
  • make sure cryostat earthed to telescope only. no
    earth through components controller, cryocooler
    lines, cables etc
  • Separate noisy grounds from low level signal
    grounds
  • All cabling use shields
  • Keep noisy circuitry and cables away from low
    level signals.
  • Only earth shields at one end, preferably at
    source
  • Orient cryocooler so that its radiated large
    magnetic field has least affect on the detector
    controller.
  • Electrically isolate shields from each other
    especially noisy shields from low level shields
  • eg. clocks from biases from output signal

40
Detector Ground
  • Star point ground no ground loops
  • Used isolated internal shield around detector
  • Cryostat grounded once to telescope
  • All cables are shielded and shields connected at
    one end only
  • Noisy signals/cables are separated from low level
    ones
  • Orient cryocooler so that its radiated large
    magnetic field has least affect on the detector
    controller

41
Component Controller Ground
42
Detector Test Facilities
43
Test Facilities
  • Test Software
  • CICADA RSAA Instrument Control and Data
    Acquisition software
  • support SDSU-2 for CCDs
  • modify to support IR detectors
  • Test Cryostat
  • IfA
  • Do initial characterization and optimization
    using KSPEC, cross-dispersed spectrograph
  • RSAA
  • Modify existing 8 IR labs cryostat (CWS at 55K)
  • No optics, but neutral density filter for looking
    out
  • Manually operated cold shutter for darks
  • IR LEDs inside cryostat for flat fields -
    controlled from outside cryostat
  • Accommodate final Detector Housing and assembly
    and wiring
  • Data Analysis Software
  • IRAF

44
Test Cryostat Measurement
  • What measurements do we want to do
  • read noise, dark current - completely blank off
    with cold stop
  • photon conversion gain, full well capacity and
    linearity - illuminate evenly with stable source
    intensity (e.g.IR LEDs inside cryostat)
  • quantum efficiency - illuminate with repeatable
    stable source of known intensity (e.g. black
    body) - absolute vs relative
  • cross-talk and persistence - test image generator
    such as hot spot and lines
  • fringing???? - should we wait until in final
    cryostat

45
Test Cryostat
  • IfA
  • Initial detector characterization at IfA
  • KSPEC, cross-dispersed spectrograph
  • RSAA
  • Modify existing Irlabs 8 double can cryostat
    (CWS at 55K)
  • Place neutral density filter over detector so
    that detector does not saturate when it looks out
  • Manually operated cold shutter directly over the
    detector for doing darks
  • IR LEDs inside cryostat for flat fields -
    controlled outside cryostat
  • Accommodate final Detector Housing, assembly, and
    wiring
  • Test image generator
  • Hot spot to one quadrant for measuring cross-talk
    and persistence
  • Lines for testing spatial characteristics

46
Operating Point
  • Vary temperature and detector voltage, measure
    and plot
  • Read noise (e)
  • Photon conversion gain (e/ADU)
  • Dark current (e/s/pixel)
  • Full well capacity (e)
  • Cosmetics
  • Quantum efficiency
  • Select suitable operating point with
  • good QE
  • sufficient well depth, (50ke) and linearity
  • minimizes read noise, dark current, and cosmetic
    problems

47
Detector Characterization Discussion
  • Can we learn to live with persistence?
  • Will fringing be stable and be able to be flat
    fielded?
  • Will we achieve low enough read noise, dark
    current at a sufficient well depth and quantum
    efficiency to do good science?

48
Persistence
  • Decay of residual images in 10 seconds darks
  • Point source of 5 million photons/sec
  • After 60 sec, residual 6000e
  • After many hours, still much greater than dark
    current signal.

G. Finger ESO
49
HAWAII-1 Fringing
  • Constructive and destructive interference effects
    in sapphire substrate - stable with time
  • peak-to-valley variation 10
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