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The ASKAP/EMU Source Finding Data Challenge

Published online by Cambridge University Press:  19 October 2015

A. M. Hopkins*
Affiliation:
Australian Astronomical Observatory, PO Box 915, North Ryde, NSW 1670, Australia
M. T. Whiting
Affiliation:
CSIRO Astronomy & Space Science, PO Box 76, Epping, NSW 1710, Australia
N. Seymour
Affiliation:
International Centre for Radio Astronomy Research, Curtin University, GPO Box U1987, Perth WA 6845, Australia
K. E. Chow
Affiliation:
CSIRO Astronomy & Space Science, PO Box 76, Epping, NSW 1710, Australia
R. P. Norris
Affiliation:
CSIRO Astronomy & Space Science, PO Box 76, Epping, NSW 1710, Australia
L. Bonavera
Affiliation:
Instituto de Física de Cantabria (CSIC-UC), Santander, 39005 Spain
R. Breton
Affiliation:
Jodrell Bank Centre for Astrophysics, The University of Manchester, Manchester, M13 9PL, UK
D. Carbone
Affiliation:
Anton Pannekoek Institute for Astronomy, University of Amsterdam, Postbus 94249, 1090 GE Amsterdam, the Netherlands
C. Ferrari
Affiliation:
Laboratoire Lagrange, Université Côte d’Azur, Observatoire de la Côte d’Azur, CNRS, Blvd de l’Observatoire, CS 34229, 06304 Nice cedex 4, France
T. M. O. Franzen
Affiliation:
International Centre for Radio Astronomy Research, Curtin University, GPO Box U1987, Perth WA 6845, Australia
H. Garsden
Affiliation:
Laboratoire AIM (UMR 7158), CEA/DSM-CNRS-Université Paris Diderot, IRFU, SEDI-SAP, Service dAstrophysique, Centre de Saclay, F-91191 Gif-Sur-Yvette cedex, France
J. González-Nuevo
Affiliation:
Instituto de Física de Cantabria (CSIC-UC), Santander, 39005 Spain Departamento de Física, Universidad de Oviedo, C. Calvo Sotelo s/n, 33007 Oviedo, Spain
C. A. Hales
Affiliation:
National Radio Astronomical Observatory, P.O. Box O, 1003 Lopezville Road, Socorro, NM 87801-0387, USA Jansky Fellow, National Radio Astronomical Observatory, P.O. Box O, 1003 Lopezville Road, Socorro, NM 87801-0387, USA
P. J. Hancock
Affiliation:
International Centre for Radio Astronomy Research, Curtin University, GPO Box U1987, Perth WA 6845, Australia Sydney Institute for Astronomy, School of Physics A29, The University of Sydney, NSW 2006, Australia ARC Centre of Excellence for All-Sky Astrophysics (CAASTRO), The University of Sydney, NSW 2006, Australia
G. Heald
Affiliation:
ASTRON, the Netherlands Institute for Radio Astronomy, Postbus 2, 7990 AA, Dwingeloo, the Netherlands University of Groningen, Kapteyn Astronomical Institute, Landleven 12, 9747 AD Groningen, the Netherlands
D. Herranz
Affiliation:
Instituto de Física de Cantabria (CSIC-UC), Santander, 39005 Spain
M. Huynh
Affiliation:
International Centre for Radio Astronomy Research, M468, University of Western Australia, Crawley, WA 6009, Australia
R. J. Jurek
Affiliation:
CSIRO Astronomy & Space Science, PO Box 76, Epping, NSW 1710, Australia
M. López-Caniego
Affiliation:
Instituto de Física de Cantabria (CSIC-UC), Santander, 39005 Spain European Space Agency, ESAC, Planck Science Office, Camino bajo del Castillo, s/n, Urbanización Villafranca del Castillo, Villanueva de la Cañada, Madrid, Spain
M. Massardi
Affiliation:
INAF-Istituto di Radioastronomia, via Gobetti 101, 40129 Bologna, Italy
N. Mohan
Affiliation:
National Centre for Radio Astrophysics, Tata Institute of Fundamental Research, Post Bag 3, Ganeshkhind, Pune 411 007, India
S. Molinari
Affiliation:
IAPS - INAF, via del Fosso del Cavaliere 100, I-00173 Roma, Italy
E. Orrù
Affiliation:
ASTRON, the Netherlands Institute for Radio Astronomy, Postbus 2, 7990 AA, Dwingeloo, the Netherlands
R. Paladino
Affiliation:
INAF-Istituto di Radioastronomia, via Gobetti 101, 40129 Bologna, Italy Department of Physics and Astronomy, University of Bologna, V.le Berti Pichat 6/2, 40127 Bologna, Italy
M. Pestalozzi
Affiliation:
IAPS - INAF, via del Fosso del Cavaliere 100, I-00173 Roma, Italy
R. Pizzo
Affiliation:
ASTRON, the Netherlands Institute for Radio Astronomy, Postbus 2, 7990 AA, Dwingeloo, the Netherlands
D. Rafferty
Affiliation:
Hamburger Sternwarte, Universität Hamburg, Gojenbergsweg 112, D-21029 Hamburg, Germany
H. J. A. Röttgering
Affiliation:
Leiden Observatory, Leiden University, P.O. Box 9513, 2300 RA, the Netherlands
L. Rudnick
Affiliation:
Minnesota Institute for Astrophysics, University of Minnesota, 116 Church St. SE, Minneapolis, MN 55455
E. Schisano
Affiliation:
IAPS - INAF, via del Fosso del Cavaliere 100, I-00173 Roma, Italy
A. Shulevski
Affiliation:
ASTRON, the Netherlands Institute for Radio Astronomy, Postbus 2, 7990 AA, Dwingeloo, the Netherlands University of Groningen, Kapteyn Astronomical Institute, Landleven 12, 9747 AD Groningen, the Netherlands
J. Swinbank
Affiliation:
Anton Pannekoek Institute for Astronomy, University of Amsterdam, Postbus 94249, 1090 GE Amsterdam, the Netherlands Department of Astrophysical Sciences, Princeton University, Princeton, NJ 08544, USA
R. Taylor
Affiliation:
Department of Astronomy, University of Cape Town, Private Bag X3, Rondebosch, 7701, South Africa Department of Physics, University of the Western Cape, Robert Sobukwe Road, Bellville, 7535, South Africa
A. J. van der Horst
Affiliation:
Anton Pannekoek Institute for Astronomy, University of Amsterdam, Postbus 94249, 1090 GE Amsterdam, the Netherlands Department of Physics, The George Washington University, 725 21st Street NW, Washington, DC 20052, USA
*
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Abstract

The Evolutionary Map of the Universe (EMU) is a proposed radio continuum surveyof the Southern Hemisphere up to declination + 30°, with the AustralianSquare Kilometre Array Pathfinder (ASKAP). EMU will use an automated sourceidentification and measurement approach that is demonstrably optimal, tomaximise the reliability and robustness of the resulting radio sourcecatalogues. As a step toward this goal we conducted a “DataChallenge” to test a variety of source finders on simulated images. Theaim is to quantify the accuracy and limitations of existing automated sourcefinding and measurement approaches. The Challenge initiators also tested thecurrent ASKAPsoft source-finding tool to establish how it could benefit fromincorporating successful features of the other tools. As expected, most findersshow completeness around 100% at ≈ 10σ dropping to about 10% by≈ 5σ. Reliability is typically close to 100% at ≈10σ, with performance to lower sensitivities varying between finders. Allfinders show the expected trade-off, where a high completeness at lowsignal-to-noise gives a corresponding reduction in reliability, and vice versa.We conclude with a series of recommendations for improving the performance ofthe ASKAPsoft source-finding tool.

Information

Type
Research Article
Copyright
Copyright © Astronomical Society of Australia 2015 
Figure 0

Table 1. List of source-finding tools tested.

Figure 1

Figure 1. A subsection of the first Data Challenge image (left), and the input source distribution to this image (right). This image includes sources distributed randomly with a flux density distribution that is uniform in the logarithm of flux density. This distribution gives rise to a much higher surface density of bright sources, and proportionally more bright sources compared to faint sources, than in the real sky.

Figure 2

Figure 2. A subsection of the second Data Challenge image (left), and the input source distribution to this image (right). This image includes sources distributed with intrinsic clustering, and with a flux density distribution drawn from the observed source counts (e.g., Hopkins et al. 2003), in an effort to mimic the characteristics of the real sky.

Figure 3

Figure 3. A subsection of the third Data Challenge image (left), and the input source distribution to this image (right). This image includes sources as for the second Data Challenge image, but with 20% of the sources now assigned a non-negligible physical extent. The extended sources are modelled as two-dimensional elliptical Gaussians.

Figure 4

Figure 4. The distribution of input source flux densities for the three Challenges.

Figure 5

Figure 5. The completeness and reliability fractions (left and right respectively) as a function of input source flux density (completeness) or measured source flux density (reliability) for each of the tested source finders for Challenge 1. The grey lines show the distribution for all finders in each panel, to aid comparison for any given finder.

Figure 6

Figure 6. The completeness and reliability fractions (left and right respectively) as a function of input source flux density (completeness) or measured source flux density (reliability) for each of the tested finders for Challenge 2. The grey lines show the distribution for all finders in each panel, to aid comparison for any given finder.

Figure 7

Figure 7. The completeness and reliability fractions (left and right respectively) as a function of input source flux density (completeness) or measured source flux density (reliability) for each of the tested finders for Challenge 3. The grey lines show the distribution for all finders in each panel, to aid comparison for any given finder. Note that PySE (FDR) was only submitted for Challenges 1 and 2, and does not appear here.

Figure 8

Figure 8. The product of the completeness and reliability as a function of input source flux density for each of the tested source finders for Challenges 1–3 (left to right). The grey lines show the distribution for all finders in each panel, to aid comparison for any given finder. Note that PySE (FDR) was only submitted for Challenges 1 and 2.

Figure 9

Figure 9. Examples illustrating potential sources of both incompleteness and poor reliability for four of the tested source finders for Challenge 1. Top left: Apex; Top right: blobcat; Bottom left: Selavy (smooth); Bottom right: Selavy (atrous). Orange crosses identify the location of input artificial sources. Circles are the sources identified by the various finders, with green indicating a match between a measured source and an input source, and purple indicating no match. Isolated orange crosses indicate incompleteness, and purple circles show poor reliability.

Figure 10

Table 2. Results from image-based analysis, for Challenge 1. We consider residual images made in two ways, subtracting either the image or the smoothed model from the implied image, and measure the rms derived from the MADFM (in mJy/beam), and the sum of the squares of the residuals (in (Jy/beam)2). We show for comparison, in the line labelled ‘input’, the same statistics derived from subtracting the smoothed model from the challenge image. In each column the three submitted entries with the lowest values are highlighted in bold, as is the best performance of Selavy for reference.

Figure 11

Table 3. Results from image-based analysis, for Challenge 2. Columns as for Table 2.

Figure 12

Table 4. Results from image-based analysis, for Challenge 3. Columns as for Table 2.

Figure 13

Table 5. Positional accuracy statistics in arcsec. For a 5σ detection limit, the minimum rms error expected is μ ≈ 0.3arcsec. For 10σ, similar to the threshold for APEX, it is μ ≈ 0.15arcsec.

Figure 14

Figure 10. The ratio of the measured to the input flux density, as a function of the input flux density, for Challenge 2. The solid and dashed lines are the expected 1σ and 3σ errors from the rms noise in the image. The dot-dashed line indicates the expected flux ratio from a nominal 5σ threshold, obtained by setting Smeas = 5σ for all values of Sinput.