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Orthogonal Transfer CCD Arrays OTAs: Pros and Cons for LSST

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Production started mid-January; 10 week fabrication time first wafers in mid-March. Wafer level testing in late March (STA) and April (ITL) ... – PowerPoint PPT presentation

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Title: Orthogonal Transfer CCD Arrays OTAs: Pros and Cons for LSST


1
Orthogonal Transfer CCD ArraysOTAs Pros and
Cons for LSST
  • A collaborative effort between
  • MIT Lincoln Laboratory (Burke)
  • Semiconductor Technology Associates (Bredthauer)
  • Univ of Hawaii / PanSTARRS (Tonry, Luppino)
  • WIYN Observatory (Jacoby)
  • Univ of Arizona / Imaging Technology Laboratory
    (Lesser)

2
MotivationImproved Image Quality Over 1
  • Based on Tip/Tilt Performance at WIYN (Claver)
  • Tip/tilt improves seeing by 15 in FWHM
    (typically about 0.14)
  • RIZ medians become 0.52, 0.43, 0.35
  • Atmosphere decorrelates at 2 arcmin degrades
    0.32 images by 10

3
OPTIC The OTAs Ancestor
  • Example 300s R-band image
  • 3 of 4 guide regions selected
  • Read at 10-50 Hz
  • Tip/tilt correct remaining pixels
  • CCD Format
  • 2 2Kx4K OT CCDs
  • 4 high-speed read zones
  • 4 science zones

4
OPTIC A Time Domain Application
  • Quick readout of selected regions
  • Enables the 10-50 Hz time domain for CCDs
  • Example planet transits
  • 0.3s samples binned to 60s
  • Relative accuracy 6E-4
  • Approaches HST (1E-4)

Planet Transit
5
Orthogonal Transfer Array (OTA)
OTCCD pixel structure
OTA 8x8 array of OTCCDs
Basic OTCCD cell
6
Summary of OTA Properties
  • 64 independent 500 x 500 CCDs
  • Individual addressing of CCDs
  • 2 arcmin field of view at LSST
  • Bad columns confined to cells
  • Point defects are tolerated
  • Cells with bright stars ? guide stars, or read
    fast, up to 30 Hz, to avoid blooming, or for time
    studies
  • 8 video channels 2s readout
  • Intercell gaps (0.1-0.3 mm 1-3) dithering
    required
  • Inter-OTA spacings 2 mm (20)

5cm
12 um pixels 0.23 at LSST
7
Pinout Configuration
99 pins include some redundancy (69
required) Symmetry allows single package for
front or backside devices
Right side
Left side
8
STA CCD Array ConfigurationLincoln is similar
  • 8x8 Array of elements
  • 480x494 Subcells allow for increased busing area
  • 3840 x 3952 pixels per OTA
  • 336 micron x 132 micron streets
  • Data sheet available

49.48 mm
9
Dalsa Fabrication Status
  • Foundry run divided into 3 silicon groups to
    guard against flaws
  • 8 wafers of 40 ?-cm material (thin to 15 ?m)
  • 8 wafers of 150 ?-cm material
  • 8 wafers of 500 ?-cm material (thin to 30 ?m)
  • Production started mid-January 10 week
    fabrication time ? first wafers in mid-March
  • Wafer level testing in late March (STA) and April
    (ITL)
  • Package (ITL) 1 thick OTA in April for lab and
    on-sky testing at WIYN.
  • Package 1 thin OTA in July for lab and on-sky
    testing at WIYN
  • Revisions to masks, second foundry run to start
    in the Fall 2004

10
Packaging Status
  • Designed by G. Luppino and M. Lesser
  • Components being fabricated by Kyocera for
    delivery in April

11
Expected Device Properties
  • Pixel rates gt 1 Mpix/s
  • Read noise 6-8 e- (degraded by long video lines
    on chip)
  • Pixel size is 12 ?m MITLL testing 10 ?m
  • Thinning depends on resistivity (thus, so does
    QE, MTF vs ?)
  • Blooming is different than usual CCD with channel
    stops puddling of charge instead of trails is
    cosmetically cleaner

12
Advantages For LSST
  • Improved device yield
  • Resilient to shorts (lose a cell, not an entire
    detector)
  • Bad columns delimited by cell size
  • Tip/tilt image enhancement (smaller pixels are
    better)
  • Control of blooming from bright stars
  • OT pixels lead to puddling of charge (N
    affected pixels) rather than trailing (gt1K pixels
    in a column)
  • Fast readout of cells with bright stars avoids
    saturation
  • Extreme saturation is delimited by cell size
  • Improved observing efficiency
  • Can start exposures while telescope settles
  • Can observe in windy conditions
  • Science array provides guider signal
  • Development underway by other groups available
    with licensing agreement
  • Reduces demands on telescope structure and control

13
Disadvantages For LSST
  • Detectors dont exist yet
  • Fill factor is 90 due to circuitry between
    cells (though future developments can greatly
    reduce this loss)
  • With OT shifting, each cell has unique
    astrometric solution (dominated by simple XY
    offset)
  • With OT shifting, each cell has a unique PSF that
    may vary slightly across a cell
  • Due to the 64 amplifiers per OTA, heat load is
    about 0.7 watt per 50 mm of silicon
  • More complex electronics
  • NOAO MONSOON
  • IFA IOTA
  • Pixel traps may be present

14
Other Considerations for LSST
  • Consider OTA geometry but without OT pixels
    control bright stars
  • Consider OTA but with smaller pixels (10 ?m
    0.20)
  • Consider OTA but with type 2 pixels
    half-pixel tip/tilt control
  • Replace logic on the detector with bump-bonded
    ASIC having front-end electronics
  • improves fill factor
  • Improve readout speed by 8X (to 0.25 sec)
  • Reduces read noise by eliminating long video
    lines

15
More Considerations for LSSTAlternative
Observing Modes
  • Use OT to track moving objects instead of
    telescope motions
  • Use OTA geometry to obtain high speed time series
    data on many stars at once

16
Simulated Image Improvement
  • Adopt real centroid sequence from a WIYN
    observation
  • Native seeing 0.65
  • 300 sec exposure
  • Data from OPTIC
  • Pixels are 0.14

17
Simulated Image Improvement
  • Assume Gaussian PSFs of 0.33, 0.55, 0.77
  • Apply shift sequence
  • Trail from guider telescope shake atmosphere

No tip/tilt Correction
With tip/tilt Correction
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