IR All-Sky Camera
Sloan Digital Sky Survey Telescope Technical Note
19910801
Walter
A. Siegmund and Charles
Hull
It has long been apparent that an all-sky picture of clouds over
an observatory site and available in near real-time would be a great
benefit to personnel using a telescope. The acquisition of such a
device was rated very high by the Apache Point Observatory Science
Advisory Committee a couple years ago, indeed higher than some
astronomical instruments. For remote observing, such a cloud imager
is almost essential. Our experience is, on nights with partial cloud
cover, that most of the requests of the night assistant by the remote
observer are for information on cloud distribution. Such interaction
is a poor substitute for a cloud picture sent to the remote observer
and is a poor use of the night assistant. Finally, protection of the
telescope from precipitation can be better assured with continuously
updated cloud images. This is important for both on-site and remote
observers since a rain cloud can develop quickly in a direction away
from the direction the telescope is pointed.
We have every reason to believe that clouds can be detected very
simply and easily in the 10-12 micron wavelength window. The same
factors which make low water vapor of crucial importance for IR
astronomy, make this band useful for cloud imaging. We have anecdotal
evidence from J.T. Williams of MMTO and David Westfall, formerly of
CFHT and now of New Mexico Institute of Mining, that video-rate 10
micron cameras are very effective at imaging clouds. Fred
Forbes and his colleagues of NOAO report that a water vapor
monitor using an uncooled pyroelectric detector is very sensitive to
clouds.
The video-rate IR cameras used by Williams and Westfall, are
cryogenically cooled and not designed for continuous operation.
Instead, we consider a single channel uncooled pyroelectric detector
scanned using a mirror on an gimbal driven by stepper motors. This
scanning scheme will generate scan lines much like lines of constant
longitude on a globe. The equator, in this pattern, will be the great
circle running east to west across the sky and through the zenith. We
suggest this pattern since it can be displayed directly without
remapping or written to a FITS format file, albeit with a little
distortion. The scanner covers the sky down to two air masses except
for a small portion in the direction of the motor driving the outer
gimbal. The off-axis parabolic mirror, that images the sky on the
detector, is mounted 15° above the gimbal axis. This enhances
sky coverage in the direction of the motor driving the outer gimbal,
but will cause further distortion of the image if the scanning of
successive lines is not modified slightly.
The optical components of the system are listed below. An off-axis
gold coated parabolic mirror images the sky onto the detector. A 10
micron filter above the detector determines the bandpass of the
system (the detector sensitivity is not wavelength dependent). The
focal length of the mirror is 25 mm. The detector is 0.5 mm in
diameter. Thus, the field of view is 0.020 radians. To critically
sample, we should sample every 0.010 radians. This gives about 200
samples across the 2 radians we wish to scan. Sampling at 200 Hz, a
scan line will take 1 second and a frame will take 200 seconds or 3.3
minutes. Rather than scan in a TV raster pattern, we will scan
successive lines in opposite directions to eliminate the deadtime
during retrace.
For the detector, the noise equivalent power, i.e., the power
incident on the detector needed to provide a signal to noise ratio of
one, is
where A is the detector area and D* is the sensitivity parameter
specified by device manufacturers.
We plan to sample at 200 Hz, so to avoid aliasing we need a
low-pass filter with a cut-off at 100 Hz. Over this bandwidth,
,
the noise power is
Our goal (suggested by Fred Gillett) is to detect 1% of an IR
opaque cloud at 0°C. The flux from a black body is
Evaluating this expression for 0°C and 10 microns gives
6.38E-12 W/m^2 Hz and 1% of this is 6.38E-14 W/m^2 Hz.
The power incident on the detector from such a cloud which fills
the field of view is
where T is the throughput of the optical system, d is the diameter
of the beam,
is the solid angle viewed by the detector, and
is the bandpass of the IR filter. The solid angle viewed by the
detector is
where f is the focal ratio of the parabolic mirror.
Combining the above expressions we find that the signal to noise
ratio is
Evaluating this expression for 3.8E12 Hz passband of the IR
filter, the 0.77 throughput of the optical system (neglecting the
detector window), and evaluating the rest of the parameters from the
values given below, we find a SNR of 4.1.
Component Manufacturer Comments
Detector EDO Corp. 300-2 Ø0.5 mm, D*=4E8 cm-Hz^1/2/W
Filter OCLI W10672-9 Ø25 mm x 1 mm, 82% transmission, 10-11.4 µm
Mirror Janos A8037-116 F.L. = 25 mm, Ø25 mm, 97% reflectance
Mirror Edmund R32,088 38x54x9.5 mm elliptical, 97% reflectance
The 10 micron window has significant opacity, about 14% with 1 cm
precipitable water. Since we plan to scan to about 2 air masses, the
edge of the picture will be about twice as bright as the center. We
may wish to subtract a function which compensates for this effect to
make it easier to see clouds.
We do not intend to chop the beam against a reference. Instead, we
will be looking for features in the cloud cover. This camera will not
be sensitive to uniform cloud cover. However, this is a cloud pattern
that the proposed Digital Sky Survey monitor telescope with its low
spatial coverage, is sensitive to, and thus compliments the
capability of the IR scanner.
The brightest astrophysical sources (outside the solar system) are
about 1E21 W/m^2 Hz. This is far below the sensitivity of this
system. This is one great advantage of imaging clouds at this
wavelength, i.e., the interpretation of cloud images is not confused
by background sources.
Reference
1. Forbes, F., Morse, D.A., Poczulp, G.A.,
Site Survey Instrumentation for the National New Technology
Telescope (NNTT), Optical Engineering, 27, no. 10, p. 845.