Supplementary Material
to:
An Introduction to Radio Astronomy
4th edition Cambridge University Press 2019
Last updated 04/12/2021
Chapter 8: Single-aperture Radio Telescopes
A corrugated horn feed:
The commonest feed design used in
radio astronomy systems (section 8.1) employs surface corrugations between λ/4 and λ/2 in depth. The modified surface avoids a discontinuity
at the edges of the horn aperture. The flexibility allowed by such an arrangement allows broad band
reception coupled with good control of the beam pattern and polarization purity.
A corrugated
horn feed for K-band (centre frequency 22 GHz) mounted in a test fixture and
with a circular polariser on the output.
The horn has an internal diameter of 65mm at the open end. (courtesy E. Blackhurst)
Phased Array Feeds (PAFs): ASKAP and APERTIF
PAFs are revolutionising the field-of-view available to dishes. The ASKAP PAF (left) is a close-packed planar array of 94 dual-polarization dipoles – see https://www.csiro.au/en/Research/Astronomy/ASKAP-and-the-Square-Kilometre-Array/PAFs which covers the range 700-1800 MHz with an instantaneous bandwidth of 300 MHz available. The APERTIF feed (right), developed at ASTRON in the Netherlands uses a box-like structure of close-packed Vivaldi tapered slot dipoles (see www.apertif.nl ).
Both feed systems are designed for L-band operation and can produce up to 30 close-packed beams on the sky hence greatly extending the field-of-view (FoV) of the telescope. Careful adjustments of the complex weights applied to the elements forming each beam (see main text Fig 8.27) can also improve the aperture efficiency over that of a “standard” feed and hence increase the telescope’s effective area Aeff. The great advantage of PAFs is the increase in the survey speed which, for a given bandwidth, is proportional to FoV x [Aeff/Tsys]2 (see the new section at the end of Supp. Mat Chapter 11). However, both these L-band PAFs are uncooled for reasons of cost and complexity and the achieved Tsys values are typically a factor two higher than for a cryogenically-cooled single feed receiver, this partly offsets the FoV and Aeff improvements. Several groups around the world are, therefore, now developing cryogenically cooled PAFs.
Measured antenna power patterns
Fig 8.15 shows a highly idealised power pattern of an antenna in polar
coordinates. Below we show three actual
plots of antenna power patterns taken from student experimental work at the
Jodrell Bank Observatory.
Low-cost “cantenna” feed
A low-cost “cantenna” (an open circular waveguide) for
feeding a small (3.1m) parabolic dish at 21cm wavelength was constructed out of
a food can (top left) with a type-N
connector and λ/4 probe (drawing bottom left). The beam pattern plotted in
Cartesian coordinates is shown at the top right and in polar
coordinates at the bottom right. The data were taken at 5o intervals
and normalised to 0 dB on axis, the FWHM is ~65o and the peak backlobe is -15 dB (credit
Abeer Almutairi). Many websites provide detailed
information on the design and construction of cantennas.
Commercial Yagi
This commercial 16-element Yagi antenna was
designed for UHF broadcast TV reception in a band near 600 MHz; a planar phased
array of these antennas in the MUST facility is shown in Fig 8.12. Left) a schematic of the antenna
configuration (credit E. Vavilina); right) a power pattern, plotted in polar
coordinates, taken on a temporary outdoor range. The data were taken at 5o
intervals and normalised to 0 dB on axis, the FWHM is ~30o and the
peak backlobe is -19 dB.
Experimental Corrugated Horn
Left) An experimental low-cost corrugated horn antenna (aperture 0.55m)
built to assess a novel construction technique and its potential for future
radio astronomy projects at L-band. Right)
the measured (black) and calculated (blue) power patterns plotted in Cartesian
coordinates. The sidelobes are much lower than those of the Yagi antenna and
the agreement with theory is good; note however that accurate measurements
at the -40dB level in the field are subject to residual scattering despite the
use of a large ground screen (not shown). (credit
I.W.A.Browne & A.
Colclough).
Feed illumination,
surface profiles and power beam of a parabolic dish via holography
(Section 8.8 and Chapter 9)
The accurate surface profile of a dish can be determined in several
ways: by laser scanning, by photogrammetry or, as here, using radio holography.
In this technique a distant source, often a satellite transponder but a powerful
celestial radio source can also be used, is observed with an interferometer.
The dish under test (DUT) acts as one element and is raster scanned across the
target source while the beam of the other element remains fixed on the source.
By this means the complex voltage polar diagram of the DUT is obtained; the
complex field across the aperture of the DUT can then be obtained by Fourier
transformation. From the phase pattern the variations in surface profile in
wavelengths (and hence mm) can be obtained.
(Left) the phase and (right) the
amplitude components of the complex illumination pattern of the Torun 32-m dish
obtained during the late stages of a holographic programme using the
Eutelsat w2 satellite transponder at 12.1 GHz.
In both patterns the shadow of the secondary mirror support legs can be
seen; a test panel, which has been mis-set from the overall parabolic shape,
can also be seen in the lower right quadrant.
The amplitude pattern shows the effect of the feed taper; less power is
collected from the outer parts of the dish.
Left) the phase deviations have been translated into wavelengths and hence mm away from the desired parabolic profile. A calibration panel (height 3 mm) can be seen in the lower right hand quadrant. After the holographic resetting the overall surface rms was ~0.4mm rms corresponding to a reflectivity of ~78% at an observing frequency of 30 GHz (wavelength 10mm; Ruze formula). Prior to resetting (see profile patterns below) the surface rms was 0.8 mm rms corresponding to a reflectivity of 36% at 30 GHz. (right) the corresponding beam pattern, the larger sidelobes in p.a. ±45o are due to blocking/scattering of radiation by the secondary mirror support legs.
1-D
cuts through the above beam pattern expressed in dB relative to the peak. The
top panel shows a vertical cut (in elevation) over two angle ranges (±4o
and ±1o).
The bottom panel shows a cut at 45o over a ±4o range; the higher level of the
sidelobes in this direction can clearly be seen.
Left) The surface
profile at an early stage in the holographic measurement programme when the
setting accuracy was 0.8 mm rms; right)
the surface profile after a first stage of resetting. Note that in this stage different test panels
were set up compared to that used in the final resetting stage shown above.
IMAGE CREDIT: A Kus
and G. Pazderski (TcFA
Torun)
For recent detailed descriptions of the use of holography to characterise radio antenna beams see
· “Primary beam effects of radio astronomy antennas: I.
Modelling the Karl G. Jansky Very Large Array (VLA) L-band beam using
holography” by K. Iheanetu et al. (2019) https://arxiv.org/pdf/1903.02486.pdf
· “Primary beam effects of
radio astronomy antennas: I. Modelling the MeerKAT
L-band beam ” by K. Iheanetu et al. (2019) https://arxiv.org/pdf/1904.07155.pdf
Voltage
and power beams – a pictorial recapitulation (Sections 8.3 and 8.9)
N.B. antenna size is denoted by D in the
main text not d as in the diagram below
Left) There is a “Fourier pair”
relationship between the spatial pattern of the electric field
illumination across the aperture (the aperture distribution) and the angular
pattern of the complex electric field in the far-field (the “voltage
beam”): this is a basic result from
Fraunhofer diffraction theory. Here,
for simplicity, the illumination pattern is drawn as 1-D cut through a
uniformly-illuminated square antenna and the voltage beam is therefore a sinc function. Note that at
a given frequency the voltage beam oscillates from negative to positive at the
radio frequency i.e. typically at GHz rates. The power beam, being the voltage
beam squared, does not oscillate.
Right) The Wiener-Kinchin
theorem states that the power spectrum of a function is the Fourier
transform of its autocorrelation function (ACF). In this case the power spectrum is the
angular spectrum of the power beam and the ACF is that of the antenna aperture
distribution. The power beam is therefore a sinc2 function. Note that although the ACF is has
twice the extent of the uniform distribution its tapered shape gives a power
beam which does not have double
the formal resolution of the voltage beam in particular the 1st zero
in sinc2 and sinc is at 1/u. The FWHM of
the intensity main beam (left) is, however,
narrower than that of the voltage beam (right) as shown in the main text Fig
8.20 and reproduced here.
Beam smoothing and angular frequency cut-off
The “true”
sky distribution (intensity or power) can be viewed as either
·
a fine grid of point sources to be
convolved with the (spatial) antenna power beam
or
·
a spectrum of angular frequency
components with units of cycles radian-1 (compare with Hz i.e. cycles s-1) to be weighted by the
angular frequency “transfer function” of the antenna for intensity.
In the first case convolution
with the antenna power beam smooths out fine details in the spatial temperature distribution
of the sky on angular scales smaller than ~λ/D i.e. smaller than 1/u (Figs 8.31
and 8.32). In the second case we consider the sky temperature distribution
(intensity or power) as made up of Fourier components of different angular frequencies (number of cycles rad-1 across sky) e.g. 500
cycles rad-1 in the figure below
The antenna can be regarded as
having a virtual “intensity aperture” (i.e. its angular frequency transfer
function; the ACF of the aperture distribution) extending from -u to +u. For
the specific case of a uniformly illuminated square aperture the ACF has a
triangular shape but all distributions will fall away from the central peak.
This transfer function implies an increasingly low weighting to the higher
spatial frequency Fourier components in the sky brightness distribution; it
acts as a low-pass filter cutting out angular frequencies greater than u: hence
the smoothed sky distribution is “band-limited” i.e. “cut-off” beyond u cycles/radian
In summary
State-of-the-art radio telescopes:
The historical development of the design and construction of reflector antennas used for radio astronomy is extensively covered in the book by J,M. Baars and H.J. Kärcher ” Radio Telescope Reflectors” pub. Springer 2017. This is available on the web at https://link.springer.com/content/pdf/10.1007%2F978-3-319-65148-4.pdf
Fixed Reflectors.
The telescopes
with the largest collecting area are the fixed reflectors FAST and
Arecibo. Their beams are swung over
large angles by moving the feed. This
requires compensation
for aberration. In FAST this is achieved by deforming the
flexible surface; the Arecibo surface is spherical, and compensation is
achieved in a secondary feed and reflector system.
Five Hundred
Metre Aperture Radio Telescope (FAST). Situated
in Guizhou province in south-west China FAST is now the largest single dish in
the world. The surface is active and can be pulled by over 2000 steel cables
into a parabolic profile with a diameter of 300m. As the source moves across
the sky the parabolic area and the suspended feed move under computer control
to track it http://fast.bao.ac.cn/en/
Arecibo
Telescope. Situated in Puerto Rico and
commissioned in the 1960s it was for over 50 years the world’s largest single
aperture telescope with an effective diameter of ~200m. The reflecting surface
has a fixed spherical profile and to correct for aberrations the focus area has
secondary and tertiary mirrors
Dishes with adjustable
surfaces.
Green Bank Telescope (GBT). Currently
the world’s largest fully steerable dish with a diameter exceeding 100m. The offset design was chosen to minimise
scattering off the telescope structure and hence to reduce sidelobes (https://greenbankobservatory.org/telescopes/gbt. The surface panels are adjustable by over 2000
actuators under computer control. An overall surface accuracy of 240 μm rms. has been achieved which allows useful
observations down to 3mm (110 GHz) wavelength to be made when the atmospheric
opacity is low (for more details see Frayer et
al (2018) https://arxiv.org/pdf/1811.00105.pdf ).
Sardinia Radio Telescope (SRT). The 64-m Sardinia Radio Telescope has an
active surface controlled by over 1000 actuators; the specification of 150 μmr.m.s. enables operation to 3 mm wavelength with
good efficiency. Designed for flexible operation for a variety of uses,
including space communications, the SRT’s innovative optics permit a wide range
of receivers to be operated at several focal stations (http://www.srt.inaf.it).
Tian Ma Telescope The 65-m
Tian Ma telescope in Shanghai China was commissioned in part to support China’s
Lunar Exploration project. It has Cassegrain optics and active surface control
giving an overall accuracy of 300 μmr.m.s.
allowing good performance up to 50 GHz (http://english.shao.cas.cn/fs/201410/t20141008_12893.html
Dishes at millimetre wavelengths
IRAM 30-m telescope at Pico Veleta (iram-institute.org) The Franco-German Institut
de Radio AstronomieMillimetrique (IRAM) operates a
30-metre radio telescope, designed for millimeter-wave
observations, on the Pico Veleta (altitude 285m) near Granada Spain. Its
overall r.m.s. surface accuracy is 70 μm and is intended primarily for spectroscopic studies
of the interstellar medium. To over- come the atmospheric emission from water
vapor, it has a nodding secondary that allows comparison of the observing field
with a reference field nearby (http://www.iram-institute.org/EN/30-meter-telescope.php)
Atacama Pathfinder Experiment Telescope (APEX) The 12-m diameter APEX (Atacama Pathfinder
Experiment)telescope is operated by a consortium of the Max Planck Institutf¨urRadioastronomie (MPIfR)
at 50%, the Onsala Space Observatory (OSO) at 23%,
and the European Southern Observatory (ESO) at 27%. It is situated on the Llano
Chajnantor close to the ALMA array at an altitude of
5105m. The antenna is a modified ALMA prototype dish with an r.m.s. surface accuracy of 17 μm
enabling it to operate at frequencies above 1000 GHz (http://www.apex-telescope.org).
James Clerk
Maxwell Telescope (JCMT) The 15-m
James Clerk Maxwell Telescope (JCMT)was
originally conceived and operated by a UK, Dutch and Canadian
consortium. It is now operated by the East Asian Observatory. The telescope is
situated near the summit of Mauna Kea in Hawaii at an altitude of 4,092 m; it
has a surface accuracy of 24 μmr.m.s. enabling
it to operate at sub-mm wavelengths (http://www.eaobservatory.org/jcmt/)
Large
Millimetre Telescope The 50-m
diameter Large Millimetre Telescope Alfonso
Serrano is a Mexico/USA project situated on the summit of Volcan Sierra Negra
at an altitude of 4600m. The primary surface was completed in December 2017.
The LMT is now the world’s largest single dish designed for operation at short
mm wavelengths. See http://www.lmtgtm.org/ and http://www.lmtgtm.org/13-december-2017-the-50m-diameter-primary-surface-completed/
Nobeyama 45m near Minamimaki, Nagano, Japan: the observatory is at an altitude of
1350m and the telescope was completed in 1982. It remains amongst the largest
dishes aimed at mm-wave observations from 22-115 GHz and has made many contributions to
radio astronomy. https://www.nao.ac.jp/en/research/telescope/45m.html
Mapping large areas of sky
The corrected Haslam 408 MHz all-sky map
The classic 408 MHz all-sky
map of Haslam et al (1982) (see
Section 8.9) has been reanalyzed to remove residual errors. A full description
of the processes involved is given in the paper: Remazeilles, M., Dickinson, C., Banday, A. J., Bigot-Sazy, M.-A.,
Ghosh, T., "An improved source-subtracted and destriped
408 MHz all-sky map", MNRAS 451, 4311 (2015).
Versions of the new maps can be downloaded
from
http://www.jb.man.ac.uk/research/cosmos/haslam_map/
and
https://lambda.gsfc.nasa.gov/product/foreground/f_images.cfm
Sections of the 408 MHz all sky
maps before (HAS03 an earlier version of the maps) and after correction (HAS14)
taken from Remazeilles et al (2015). The stripes arose from total power
(“baseline”) offsets principally due to receiver gain variations (“1/f noise”).
Discrete artefacts arose
principally from imperfect subtraction of extragalactic sources. The source
visible in HAS82 was imperfectly subtracted in HAS03 but well subtracted in
HAS14.
References
to other large area maps
Several
other large area continuum surveys have been made with single dishes (see Remazeilles et al (2015) for references) while the HI4PI survey (Supplementary Material Chapter 3: Spectral Lines) is
an all-sky spectral line survey. For references to other large area sky maps see Chapter
14.
Twin-beam Radiometry (Sections
4.4 and Section
8.6)
OCRA-p on the Torun 32-m dish
The 30 GHz OCRA-p radiometer, described in detail
by Lowe (2006), and pictured in Supplementary Material Chapter 6, has twin feed
horns and independent receivers and was mounted at the secondary focus of the
Torun 32-m telescope (left hand panel);
the front of the receiver housing can be seen just below the mouth of the square
L-band horn. For large antennas (D > 15m) and at frequencies above ~10 GHz (λ < 0.03 m) the near-far field transition is more
distant than ~15km (often much more) hence the path through the atmosphere is
all within the near field. The right
hand panel shows the two near-field beams (path 1 and path 2) projected
on the sky with variations in the clear
atmospheric opacity indicated via the gray scale. The beams largely overlap so rapidly
differencing the receiver outputs (effected by a correlation-type receiver, see
Supplementary Material Chapter 6) greatly reduces the atmospheric effects as
well as receiver gain changes and
changes in the ground spillover. Since twin beam radiometers
differentiate the radio astronomical sky (the beams separate in the far field –
see below) they are insensitive to slow angular variations in sky brightness. Reference: S. Lowe 2006 PhD. Thesis
University of Manchester
Two beams above the atmosphere
(in the far field)
The
overlapping “quasi-cylindrical “ near field patterns
separate into the classical Fraunhofer beams with ≈1.2 λ/D - these
beams do NOT overlap. Their separation φ= x/f where x is the separation of the feed centres and f is the focal length of the dish. Consider two cases:
a) Astronomical (not atmosphere) emission in both beams is very similar
· Constant background: thus [TA1 -TA2] = 0 hence
no astronomical signal results.
· Taking the difference between the beams has “differentiated” the sky
brightness temperature distribution - hence this method is insensitive to slowly varying TB variations
b) Astronomical background emission is different in
each beam
· Compact
source in one and not the other
· System
ideally suited for surveys or monitoring observations of compact sources
Phased
array beam patterns – pictorial descriptions
Reception
pattern of a simple phased array (adding beamformer)
Phased
arrays provide “direct” imaging i.e. an instantaneous beam is formed
just as in a single dish. The classic book “Radio Astronomy” by J.D. Kraus
(section 6.4) provides a neat introduction to array theory although it is also
covered in many other places. In our main text sections 8.2 and Fig8.11
we discuss the simplest case where all the array elements are connected to the
same final receiver. In this case the relative weighting of the baselines is
triangular (see also below). In the following
set of diagrams we break down the formation of the
beam into a series of steps
---N.B. antenna size is
denoted by D in the main text not d as in the diagrams below--
The width of
the primary beam and the height of the sidelobes can be altered with additional
weightings/tapers. Appendix 6 of Kraus’s “Radio Astronomy” lists some standard
tapers and the resulting
beam patters which result.
Animations of phased arrays
There are many animations illustrating the basics of phased arrays available on the Web e.g. https://www.youtube.com/watch?v=vtPPAnvJS6c and https://www.youtube.com/watch?v=qvdfsgueJc8. The reader will be able to find others.
A illustration of the
scientific advantages of a phased array can be seen by clicking mbrace.mp4
(credit
M. Kramer). This animation schematically
showcases the ability of the central block (implicitly containing many reception
elements) to form multiple beams simultaneously – the number being limited only
by the cost of the digital beamforming hardware. Many observers or groups of
observers can therefore be running independent observations at the same
time. At 00:00:06 the beam pointing to
the right of vertical shows several higher resolution beams within it; this is
the result of adding together data from the other blocks of elements around the
central block. The upper panel in “Step
4” above shows one such “array” beam; additional array beams can be formed with
more electronics. Also shown is the
ability of a phased array to respond quickly to changes in the sky (appearance
of transient sources).
Calibration of Single
Dish Observations
The many practical issues of mapping calibration of single dish
observations was not explicitly covered in Chapter 8
although some of the basic principles were covered and basic calibration principles
were covered in Chapter 6. There are
many sources of up to date advice and wisdom but a good place to start is the
introductory paper:
“Single dish calibration techniques at
radio wavelengths”: K O’Neil (2002) NAIC/NRAO School on Single-Dish Astronomy
Techniques and Applications ASP Conference Series Vol 278 eds. Stanimirovic
S., Altschuler D.R., Goldsmith P.F. and Salter C.J.
also available at https://arxiv.org/abs/astro-ph/0203001
Other more detailed sources include:
The talks at
NRAO Summer schools
https://science.nrao.edu/facilities/gbt/single-dish-school-lectures/sds-2015
https://science.nrao.edu/science/meetings/2015/summer-schools/single-dish-program
The European Single Dish School in the
Era of Arrays https://www.mpifr-bonn.mpg.de/ESSEA2010
Broad band calibration for single dish
telescopes: https://events.mpifr-bonn.mpg.de/indico/event/48/session/5/contribution/18/material/slides/0.pdf
Pointing
single dishes
In section
8.9.4 we briefly discussed the pointing requirements of single
dishes. The paper “Green Bank Telescope: Overview and
analysis of metrology systems and pointing performance” by White et
al. https://arxiv.org/pdf/2111.12636.pdf describes in great detail
the challenges overcome in pointing the world’s largest fully steerable single
dish.