The University of Hawaii (UH) QUick Infrared Camera (QUIRC) utilizes a 10241024 pixel
HgCdTe Astronomical Wide Area Infrared Imaging(HAWAII) array produced by Rockwell Science
Center. This array is sensitive to radiation from 1 to 2.5
scale, givingthe pixel scales listed in Table 1 for the various telescopes and configurations.
Table 1. QUIRC pixel scales
TelescopeOpticsarcsec/pixelFOV (arcsec)
UH 88-inchf/100.1886193x193
f/310.0608462x62
CFHTf/80.150154x154
0.61-mf/150.43440x440
QUIST 0.25mf/101.51550x1550
The QUIRC system is comprised of four functional components: (1) the detector, optics, and dewar;
(2)The detectorreadoutelectronics;(3)A DSP controller;and (4) the instrument controlSparcstation
and fiber optic communications interface. The first three components are physically integrated and
mounted on the telescope, while the fourth is typically located in the observing room and/or the
computer room.
m. The reimaging optics provide a 1:1
1
The QUIRC electronics are controlled from a Sparcstation by issuing commands and receiving data
via fiber optic cables. The control program on the Sparcstation is called “qcdcom”. The qcdcom
program is based on the ccdcom program by M. Metzger and was modified for use with QUIRC.
The qcdcom program controls taking exposures and writing data in FITS format to disk, operates t he
moving parts of the instrument such as the shutter, filter wheel, and pupil mask, communicates with
the t elescope and guider to obtain information and perform mosaics, and provides a script capability
for automatically performing simple observing tasks. qcdcom is a command line interface only and
does not directly provide image display, but can be used with any popular display program that can
read FITS files (e.g. saoimage, Vista, IDL). A link has also been provided to the viewfits program to
automaticallydisplay images (see below).
2Near-Infrared Observing Techniques
Imaging in the near-infrared (1–2.5m) generally requires more effort than at optical wavelengths,
because the background is so much higher. There are two general data reduction techniques in
common use—both of these require frequent observation of sky fields.
The first data reduction philosophy is one in which the sky fields are used for subtraction,and the sky
subtractedimage is divided by normalizeddome flats to remove the variationsin quantum efficiency.
The advantage of this technique is that the dome lights have similar color temperature to the typical
sources being studied.
The second data reduction technique is one in which the sky exposures are also used as flats, so the
image is sky subtracted, then divided by a normalized sky flat. This technique often will work better
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QUIRC User Guide
in cases where the background has been changing rapidly. It may also give better results if the dome
flat was not evenlyilluminated(it is difficultto achieve even illuminationat the 0.6m telescope). The
dark should be subtracted from the sky before division. The disadvantages of this technique are that
the sky flat shows the response of the detector to the OH airglow + thermal emission. In particular,
fringing may be present in certain configurations (e.g. 2.2m f/10 1:1), and fringing is something
which should be subtracted, not divided.
Thenumberofbadpixels usuallydictatesaspecialtechnique forobservinginwhichseveralexposures
are made of the field being studied, with each exposure shifted slightly from the others (dithering).
When the images are combined,the bad pixels in one image can be “filled in" with good pixels from
a shifted image. This technique also improves flat-fielding relative to a single long exposure at the
same position.
It is recommended that at the start and end of each night dome flats and darks be taken. The darks
should ideally be exposures of the same length as the object exposures. Even if the darks are not
directly used in the reduction, they will serve to show which pixels have high dark counts so that
these pixels can be included in a bad pixel mask. Dome flats are generally taken as a lights on/lights
off pair. Using this strategy results in a differenceimage (ON – OFF) which represents the detector’s
flat-field response to a source with color temperature of a few 1000 K, which is roughly the same
temperatureas some of the sources being studied.
The shutter is a leaf type shutter, meaning than the center part of the aperture is open slightly
longer than the outside. Recent tests showed significant center - to-edge illumination differences for
integrationtimeslessthan1 second. Therefore,short exposures should be avoided, particularlywhen
exposing dome flats—it is far better to dim the lights with the domelight dimmer switch and use an
exposure of a few seconds than to use the dome lights at full intensity and an exposure which is less
than a second (this can introduce spurious radially varying structure into the flat-field). There is an
uncertainty in the timing of the shutter of the order of 10 millisec. Therefore, short standard star
exposuresshouldalso be avoided—onthe2.2m,theEliasstandardsm ay need to be slightlydefocused
to allow reasonable exposure times in the broad filters.
At the 2.2m telescope there is a slight rotation in the nominal cassegrain rotator position (270). The
rotation was measured in February 1996 to be 0.883 degrees CCW (e.g., N is rotated 0.883 deg E of
vertical when displayed in the normal way). One could attempt to adjust slightly for this by changing
the rotator position, or adjust for it later during data reduction. If the precise rotation and scale is
importantto the observations, one must measure t his carefully during the run since the exact rotation
value is likely to change slightly between runs when the instrument is taken off the telescope and
remounted.
2.1Detector Linearity, Saturation, Read Noise, Dark Current
Hard saturation of thedetector occurs at 50,000 ADU’s. The total gain of the system results in a scale
factor of 1.85 electrons/ADU. Recent tests (2/96) showed the device to be linear to better than 1% for
values up to about 44,000 ADUs. However, the gain and illumination is variable across the array so
care must be taken so that parts of the array are not saturating when the averageADU value is getting
close to the non-linear region. The average value should be kept below 40,000 ADUs to ensure that
one is not saturating areas of the array. The average detector dark current is
the read noise is
15 electrons rms.
0.8 electrons/sec, and
October 30, 1997
2.2Dewar Temperature
The dewarnowhas a temperaturesensor and heater. For normaloperation,the temperature controller
should be used to set the detector temperature to 80.0K. If the controller is not used, drifts can occur
as the telescope is moved, resulting in dark current instabilities in the array. The new array is not
thought to be more sensitive to these effects than the previous detector, but some of the anomalies
previouslyseen by observers with the original QUIRC detector may have been due to this effect.
2.3Camera Sensitivity
3
The following sensitivity estimates are based on observations of 2 standard stars at the UH 2.2m
2
telescope on 2/6/96. The Point SRC (source) and Mag/arcsec
integrationtime, 5
. The point source detection values below assume a PSF of 0.5 arcsec FWHM.
The nominal orientation for QUIRC at the 88-inch telescope is for the black electronics box on the
dewar (the utility box) to point North (toward the control room). Then the resulting FITS data files
written by the program have N up and E to the left (i.e. the (0,0) pixel is in the SE corner).
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QUIRC User Guide
3.1Workstation setup
The program is run from a workstation in the control room, currently io (or halley on the 88”).
There is one configurationfilethatqcdcom reads upon startuptodeterminethetelescope,secondary,
and otherinformation. There are four presetconfiguration files currently used, located in the directory
These files are for the 0.6m, the 88” at
proper file, a symboliclink should be made in that directory called tel
appropriate configuration. For example, to set up for the 88” at
10, the 88” atf=31, and CFHT atf=8. To install the
config that points to the
f=
10,
This step only needs to be done once when t he telescope or secondary changes, and should already
be set up properly for the current configuration. Be careful not to delete the configuration files
themselves.
One xterm should be devoted to the camera program. The qcdcom program does not provide an
integrated image display capability. A separate program should be used to display the data. One
option is to use the viewfits program (vf). This is a display program developed by Tony Denault at
the IRTF that displays images and has statistical and graphical analysis features. A link has been
provided from qcdcom to this program that displays images automatically. The program can be run
by typing the following in any window:
%vf&
To display images automatically, one must set the data directory to be the same as where qcdcom i s
storing the FITS files. Thisis done by clicking on the “File" button and entering the proper path. One
must also issue the command set vfout in qcdcom to enable the link so that data are displayed
automatically. See the section on vf below for m ore information.
The saoimage program can also be used to display the QUIRC images. The observer should open a
saoimage window on the camera workstation. The command line usually must be edited to read in
the fits file. This can be done by pressing the “n" key (for the “new" command)while in the saoimage
window. For example,
-imtool -fits /scr/aug11/q940811.004
would read in file number 4. When in chop mode, qcdcom writes each chop position to a separate
file, and t he chop difference to a file ending in “chop" instead of the file number.
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