Square-Kilometre Array The Next Generation Radio Telescope Dr Peter J Hall Australia Telescope...
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Transcript of Square-Kilometre Array The Next Generation Radio Telescope Dr Peter J Hall Australia Telescope...
Square-Kilometre Array
The Next Generation Radio Telescopehttp://www.atnf.csiro.au/SKA
Dr Peter J Hall
Australia Telescope National Facility
CSIRO SKA Program Leader
Presentation Outline
Radio astronomy and radio telescopes Motivation for building the SKA SKA concept and design goals
– key characteristics
Ideas for SKA realization– reflectors, arrays, lenses, signal processing
– interference mitigation
– site selection
Design and technology challenges Australian and international aspects of the SKA project
Radio Astronomy
Begun in 1930s by Karl Jansky - a Bell Labs communications engineer
Developed in 1940s by Grote Reber, a US radio engineer and radio amateur
Became respectable in late 1940s. Australia was an early player and has remained a world leader
Has provided insight into the most fundamental questions, e.g.
– 3 K big bang background radiation (communications engineers again)
– general relativity (binary pulsars) Gives access to physical conditions unattainable in labs Australia is good at astronomy, and RA in particular
– DISR impact studies
Radio Astronomy
RA derives information about the Universe from the study of natural radiation in the range ~ 10 MHz - 1000 GHz
Radio telescopes use the combination of an antenna and receiver to form a radiometer - a device for measuring the radiation temperature of a distant region of space viewed by the antenna beam
The received radiation may be continuum (broadband noise) or spectral line (“quasi-cw”) in character; variation on timescales of milliseconds to years may be involved
The measured temperature may or may not be the physical temperature of the region, depending on whether the emission is thermal or non-thermal
Radio Telescopes
Can be:– single continuous aperture (e.g. parabolic dish)
» focussing (wavefront delay) done optically
– synthesized aperture (e.g. array)» focussing done using time delay electronics
» can make huge effective aperture
» mathematically manipulate wave interference patterns between array elements to simulate continuous aperture
Sensitivity depends on total collecting area of aperture Angular resolution depends on linear extent of aperture (micro-
arcsecond attainable) Typically use very low-noise receivers (e.g. cryogenically cooled)
Computer
Dishes and Arrays
$$$ (computers)$$$
(Steel)
New paradigm: wavefront sensors and software replace steel
Physical Aperture
Synthesized Aperture
Major ATNF Radio Telescopes
64 m Parkes dish; 6 x 22 m AT Compact Array; both upgraded substantially to maintain international competitiveness
Radio Images Using the ATCA
SN1987a
NGC1808
PKS2356-61
Radio Telescopes of the Future HEMT receivers
– Wide-band, cheap, small and reliable– Need to build low-noise systems with many elements
Focal planes arrays– N beams => N-fold increase in telescope speed (and data rate!)– Greatly improve calibration schemes and imaging dynamic range – Synthesised beams and illumination patterns to overcome problems of feed
packing
Interference rejection– Adaptive nulling and RFI cancelling can work in single dishes and arrays
More computing capacity– Computing power doubles every 18 months (Moore’s Law)– Era of software-defined radio telescopes is upon us
Square Kilometer Array - Why?
Current large telescope technology dates from 1960/70’s
» VLA total area ~ 104 m2
Era of facilities upgrades approaching its end
Large increase in sensitivity is needed (100x), telescopes not receiver noise
limited ==> 1 km2 collecting area » epoch of first stars and galaxies» major advance in many other areas of astronomy (and hence physics)
New challenges: » cost ($US600 m cf ~ $US50 m for ATCA)» frequency coverage» man-made interference» completion by ~2010
Technology shift will be required
Radio Telescope Sensitivity
GMRT
Reber
Dwingeloo
Jodrell BankParkes
Arecibo
BonnWSRT
VLAAT
-3
-2
-1
0
1
2
3
4
5
1940 1950 1960 1970 1980 1990 2000
Date
Lo
g R
elat
ive
Sen
sitiv
ity
SKA
Core Issue
HST VLA
Solution
HST SKA
“Dark Ages”- before the stars ? Square-Kilometre Array
COBE satelliteNASA
“Primordial soup” - matter and energy
radio
Early galaxies- stars light up
Hubble Space TelescopeNASA / ESA
light
Astronomy Beyond the Light
SKA: Selected “Other” Astronomy
Active Galactic Nuclei
– does every ‘normal’ galaxy contain a black hole? Magnetic fields
– Faraday rotation studies of Milky Way, intergalactic medium and nearby galaxies Radio emission from hot and cool stars
– including imaging surfaces and atmospheres of giant stars Radio after-glows of gamma-ray bursts
– merger of a neutron star pair? Pulsars
– first demonstrated existence of extra-solar planets and gravitational waves; explicit demonstrations of general relativity
– future use in timing standards; interplanetary navigation; cosmological background of gravity waves
Deep space network tracking; SETI
SKA: The Concept One square km radio telescope (SKA) in 2010
– 2005 technology choice– 2007 construction– 2012 operations
Frequency range 0.3 - 12 GHz (minimum) Sensitivity 100 x VLA
– need ~ 68 dB K-1 at 1.4 GHz Multibeam essential at lower frequencies Need innovative design to reduce cost International funding unlikely to exceed $US600m
– 106 sq metre => ~$500 / sq metre» cf VLA $10,000 / sq metre
» GMRT $1,000 / sq metre
SKA Top-Level Specifications
Parameter Design GoalSensitivity Effective Area/System Temperature =
2 x 104 m2K-1
(about 68 dB K-1 at 1.4 GHz)Frequency range f = 0.2 to GHzNumber of simultaneous beams ~ 100Field of view 1 degree square at 1.4 GHzAngular resolution 0.1 arcsecond at 1.4 GHzInstantaneous bandwidth 0.5 + (f/5) GHzNumber of spectral channels 104
Number of simultaneous bands 2Polarization purity dB couplingSynthesized image dynamic range 106 at 1.4 GHz
Sky Key CharacteristicsOperating Frequency
SKA Key CharacteristicsField of View
HST FOV
1kT 20cm
1kT 6cm
mmA FOV
20 M
pc
at z
= 0
.3
SKA Key CharacteristicsConfiguration
200 km
20 km
Array Station
SKA Key CharacteristicsMultibeaming
4
8
12
16Synthesized beams
Station antenna patterns
Element antenna pattern
NFRA 1998
SKA - Multiple Station Concept
1000km(Courtesy NFRA)
Large Reflector SKA
Need revolution in construction technique before conventional large steerable dishes could be used
Chinese have suggested multiple Arecibo (‘holes in ground’) approach
SKA - Large Adaptive Reflector
Tile Array SKA
Luneburg Lens SKA
Luneburg Lens Focussing
Plane waves incident from left 1 m diameter lens, 2 GHz
radiation Classical Luneburg - focus on
surface
(Image courtesy Dr Andrew Parfitt, CTIP)
Luneburg Lens - The Loss Issue
0
20
40
60
80
100
120
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6
Noise Temperature Increase vs Lens Loss at Tphysical
= 290 KN
ois
e T
em
pe
ratu
re (
K)
Insertion Loss (dB)
Luneburg Lens - Alternative SKA Implementation
SETI Institute - 1hT
SKA Signal Processing - Reality Check
Can we expect to be able to process the signals from an array as vast as the SKA?
Look at the growth in computation power per unit (area, dollar…)– familiar as Moore’s Law
Moore’s Law - Astronomical Correlators
Correlator Performance vs Time
VLA?VLBA
ATNobeyama
VLAWRST
Fleurs
Mills Cross
6
7
8
9
10
11
12
13
14
15
16
17
18
1950 1960 1970 1980 1990 2000 2010 2020
Ope
ratio
ns p
er s
econ
d (e
xpon
ent)
Year
(Roughly doubles every two years)
SKA Signal Processing - Rough Guide
To correlate 106 antennas, over a 500 MHz bandwidth, with 104 frequency channels needs ~ 1012 Giga ops/sec
In 2010 astronomical correlators will be capable of ~107 Giga ops/sec– must aggregate SKA antennas prior to correlation– can only correlate ~4000 ‘elements’– with 100 stations, each station can have ~40 clusters of antennas– with 400 Luneburg Lens station, combine 10 lenses per cluster
If we wait until 2020, can reduce aggregation by ~3 – but only if Moore’s Law holds!
SKA - Interference Mitigation
Why?– SKA needs to observe outside (small) designated astronomy bands to
meet its scientific objectives
– SKA sensitivity is unprecedented (~100 times VLA)» each beam ~ 10Jy in 1 sec OR ~ -265 dBW/m2/Hz (128 MHz continuum
bandwidth)
– terrestial transmissions will be a problem for all but a few sites on Earth
– satellite transmissions are now globally pervasive (intentional constellation coverage for many LEOs)
How?– No single IM solution; need a hierarchy of techniques starting with
telescope site and environment, and ending with astronomy data processing
Terrestrial Interference
FORTÉ satellite: 131 MHz
Global InterferenceFrom The Sky - An Example
IRIDIUM satellite:measured 1998
ITU frequency allocation to Radio Astronomy
Signal levels of brightest*celestial radio sources
These peaks also change frequencyas the satellite moves across the sky
* Signals from early Universe are 100 billion times weaker
MHz
ITU permittedaverage levelS
ign
al
stre
ngt
h
SKA Interference Mitigation Essentials
Effective Robust Versatile: different observing modes, different
techniques (or different emphases in hierarchy)– e.g. snapshot versus synthesis imaging modes; pulsar modes
Low toxicity– removing the interference must not ruin the astronomy data, nor
turn easy-to-identify spurious signals into hard-to-identify artifacts
– bear in mind the imaging dynamic range needed in the SKA is >106 so uncorrected fiddling with imaging beams may be disastrous
SKA Interference Mitigation Hierarchy
Location of instrument (esp. central cluster), and legislated or regulated radio quiet zone
Array configuration (use power of correlation processing for as much critical science as possible)
Choice of concentrators and feeds Design of (cheap) high-intercept MMIC low-noise amplifiers Placement of RF/IF filters for high-level, fixed frequency RFI (e.g.
photonic fibre filters) “High” resolution quantizers and first-level digital filters DSP adaptive techniques (exploiting SKA buffer?) New image and time-domain processing techniques
Practical Interference Mitigation
AT Compact Array data Russian GLONASS satellite +
two frequency markers + astronomy signal in passband
Off-line digital adaptive filtering by Steve Ellingson, Electrosciences Lab OSU
On-line (real-time) realizations possible
Much synergy with military and commercial users
SKA Site Selection
Australia - Terrestial Transmitters
WA Site Search Area
Australian SKA Configuration?
SKA Critical Design Challenges
Wide bandwidth– antenna element type; use of true time delay phasing
Sensitivity– how to maintain effective area of antennas with frequency variation
Cost– need highly-integrated, easily manufactured systems
Interference mitigation– telescope site, adaptive RF, photonic and digital techniques
Calibration– 106 dynamic range; good polarization purity; both in presence of adaptive beaming!
Upgrade path– expensive infrastructure must last well; need to follow Moore’s Law (or equiv.)
Operations – robust; maintainable; advanced power generation and management
SKA Critical Technologies
Antennas & feeds– wideband, multi-beaming, easily manufactured, cheap– specific CSIRO challenge to make a cheap Luneburg Lens
RF front-ends– low-noise, ambient temperature, very highly integrated
Signal transmission and distribution– wideband analog or digital station links– need cost breakthrough in opto-electronic modulators– probably incorporate photonic signal processing in analog stages
Digital signal processing– for correlators, interference mitigation
Software– the SKA will be largely a “software radio” telescope
SKA - Current Australian Innovation
Antennas and arrays (e.g. Luneburg Lens, feed arrays) Highly-integrated (GaAs or InP MMIC) receivers Radio-frequency interference mitigation
– Adaptive (“smart”) antennas
– Robust receivers
– Software radio Photonics
– Fibre communications (GHz analog and digital)
– SKA connectivity and signal delay (wavelength division multiplexing)
– Active and passive fibre signal processing (e.g. bandstop filters)
– Ultra-wideband A-D Converters (15 GHz) Advanced synthesis imaging techniques
SKA - Benefits to Australia
CIE report for DISR (**DISR disclaimer)– distinguishes between participating and participating and hosting– examines quantified and unquantified benefits and costs
Quantified costs and benefits (QC&B)– R&D expenditure; operating expenditure; human capital; construction
expenditure; tourism benefits
Unquantified costs and benefits (UC&B)– development contracts; new IP; scientific knowledge; construction contracts;
HR & technology spinoffs; national prestige; community awareness of science and engineering
Bottom line for break-even– Participating: UC&B > $62 m (quantified cost ~ $72 m)
– Participating and hosting UC&B > $44 m (quantified cost ~ $81 m)
CSIRO Technology:Communications Antennas
Astronomy
Communications
Benefit / cost ~ 2(real estimate)
Achieving the Vision - International Collaboration
To build facilities which no single nation can afford Broaden knowledge base and provide cross fertilisation Joint URSI - IAU working group Endorsed by the OECD Megascience forum International MOU for technology study program
– Netherlands Australia
– China India
– Canada U.S.
– UK
Funding Distribution
Australia$50M
Asia$50M
Europe$250M
Nth. America$250M
Total cost $US600M
Australian Funding Profile
New funds
CSIRO
0
2
4
6
8
10
12
14
Date
$M/y
r
Strategic research
Prototype Construction Operations
Close existing facility
Summary
SKA is a scientific necessity if we are to understand critical phases in the evolution of the universe
It will have wide general application in all areas of astronomy
The scale of the telescope requires new design concepts and enabling technologies
Australia, and CSIRO, are well-placed to continue a leading role in the project
There are many opportunities for commercial involvement - astronomers are demanding (but harmless) customers
Updates at http://www.atnf.csiro.au/SKA