J. Pety and N. Rodríguez-Fernández: Revisiting the theory of interferometric wide-field synthesisTab<strong>le</strong> 4. Minimum sizes of the dirty beam images to get an imagefidelity or a dynamic range greater than a given value.Minimum fidelityaθ alias /θ fwhmor dynamic range ( f b = 0) b ( f b = 0.0625) ( f b = 0.1)10 2 2.2 2.2 2.210 3 3.5 3.7 6.610 4 8.4 13.4 13.710 5 19.8 >20.0 >20.0Notes. (a) The image sizes are expressed in units of the primary beamfull width at half maxium. (b) The computation is done for 3 differentratios of the secondary-to-primary diameters (i.e. f b , the antenna blockagefactors). The values are derived from the modeling of the antennapower patterns shown in Fig. 3.<strong>tel</strong>-<strong>00726959</strong>, version 1 - 31 Aug 2012fidelity of interferometric imaging at (sub)-millimeter wave<strong>le</strong>ngthswill be limited to a few hundred. In this case, V ∼(α p ,α s ) aliasing can be to<strong>le</strong>rated when the amplitude of B is <strong>le</strong>ssthan a fraction of the inverse of the maximum instrumentalfidelity;2. the maximum instrumental fidelity is much greater than theimage fidelity, as can be the case at centimeter wave<strong>le</strong>ngths.In this case, V ∼(α p , α s ) aliasing can only be to<strong>le</strong>rated whenthe amplitude of B is <strong>le</strong>ss than a fraction of the inverse of thedynamic range of the image.The criterion derived in each case gives a typical image size(θ alias ), which can be converted into the desired u p sampling rate.To be more quantitative, Fig. 3 models the normalized antennapower patterns of an antenna illuminated by a Gaussian beamof 12.5 dB edge taper and with a given blockage factor (ratio ofthe secondary-to-primary diameters). The top panel presents anideal case without secondary miror, whi<strong>le</strong> the midd<strong>le</strong> and bottompanels present simp<strong>le</strong> models of the ALMA and PdBI antennas.The largest angular sizes at which the power patterns are<strong>le</strong>ss than a given value, P 0 , is a first-order estimate of θ alias /2toget a fidelity or dynamic range higher than 1/P 0 .Tab<strong>le</strong>4 givesthe values of θ alias /θ fwhm as a function of the searched fidelityor dynamic range. This condition is sufficient but not necessary.Indeed, the aliasing properties also depend on the brightness distributionof the source.4.2.3. The u sampling rate of I dirty (u)We have no garantee that the sky outside the targeted field ofview is devoid of signal, so the only way to ensure a given dynamicrange inside the targeted field of view is to choose theimage size large enough so that the aliasing of potential outsidesources is negligib<strong>le</strong>. This means that the dirty image size mustbe equal to the field-of-view size plus the to<strong>le</strong>rab<strong>le</strong> aliasing sizeθ image = θ field + θ alias . (55)The conjugate uv distance and associated uv sampling then ared image =d fieldand ∂u = d image· (56)1 + d fieldn sampd alias4.2.4. The u ′ and u ′′ sampling rates of D(u ′ ,u ′′ )Fig.The u ′′ axis must thus be samp<strong>le</strong>d at the same rate as the seconddimension of the definition space of S , i.e., as u s .Moreover,u ′ has in this equation a behavior (u ′ = u p + u ′′s ) similar to3. Simp<strong>le</strong> models of the antenna power patterns as a function ofthe sky ang<strong>le</strong> in units of half the primary beam FWHM (θ fwhm ). Inthe 3 cases shown, the illumination is Gaussian with an edge taperof 12.5 dB but 3 different ratios of the secondary-to-primary diameters(i.e. f b , the antenna blockage factors) are considered (see e.g.Goldsmith 1998, Chap. 6). The midd<strong>le</strong> and bottom panels respectivelymodel ALMA and PdBI antennas. The red lines define the minimumangular sizes for which the antenna power pattern is <strong>le</strong>ss than a givenfraction.u (=u p + u s ). It must thus have the same sampling behavior as u.This sampling rate (∂u ′ = d image /n samp ) is quite high. Some deconvolutionmethods (see below) allow us to relax this samplingrate.4.3. Absence of gridding “correction”Imaging of sing<strong>le</strong>-field observations goes through the followingsteps: 1) convolution by a gridding kernel; 2) regular resampling;3) fast Fourier transform; and 4) gridding “correction”. The socal<strong>le</strong>dgridding “correction” is a division of the dirty beam anddirty image by the Fourier transform of the gridding kernel usedin the initial convolution. This step is mandatory when imagingsing<strong>le</strong>-field observations to keep the image-plane measurementequation as a simp<strong>le</strong> convolution equation (see e.g. Sramek &Schwab 1989). When imaging wide-field observations, as proposedhere, the Fourier transform along the α s dimension, followedby the shift-and-average operation, freeze the convolutionkernel into the dirty beam of the wide-field measurement equation.This is why the gridding “correction” step is irre<strong>le</strong>vant here.Page 9 of 21
A&A 517, A12 (2010)<strong>tel</strong>-<strong>00726959</strong>, version 1 - 31 Aug 20125. Dirty beams, weighting, and deconvolutionIn radioastronomy, the dirty beam is the response of the interferometerto a point source. In the wide-field synthesis framework,the response of the interferometer to a point source, D, aprioridepends on the source position on the sky. D(α ′ , α ′′ ) can thus beinterpreted as a set of dirty beams, with each dirty beam referredto by its fixed α ′′ sky coordinate. These simp<strong>le</strong> facts raise severalquestions. What are the properties of the convolution kernel? Isit possib<strong>le</strong> to modify these properties? How do we deconvolvethe dirty image?5.1. A set of wide-field dirty beamsWith the wide-field synthesis framework proposed here,Appendix A.6 shows thatD ( α ′ ,α ′′) =∫∫B ( α ′′ −α ′ ) ( ) ( )−α s Ω α ′ −α p ,α ′′ −α s Δ αp ,α s dαp dα s , (57)α p α swhereΔ ( ) α pα p ,α s ⊃ S ( )uu p ,α s , (58)pandΩ ( α ′ ,α ′′) (α′ ,α ′′ )⊃ W ( u ′ , u ′′) . (59)(u ′ ,u ′′ )Δ(α p , α s ) is the sing<strong>le</strong>-field dirty beam, associated with the uvsampling at the sky coordinate α s .AndΩ(α ′ , α ′′ ) will be cal<strong>le</strong>dthe image plane weighting function, whi<strong>le</strong> W(u ′ , u ′′ )istheuvplane weighting function. The set of wide-field dirty beams D isthen the doub<strong>le</strong> convolution of the image plane weighting functionand the sing<strong>le</strong>-field dirty beams, apodized by the primarybeam at the current sky position α s .Whi<strong>le</strong> the shape of the sing<strong>le</strong>-field dirty beam is directlygiven by the Fourier transform of the sampling function, theshape of the wide-field dirty beam depends, directly or throughFourier transforms, on the sampling function (S ), the primarybeam shape (B), and the weighting function (W). Moreover,the wide-field dirty beam shape a priori varies slowly with thesky position, since it is basically constant over the primarybeamwidth as stated in Sect. 4.2. It neverthe<strong>le</strong>ss varies, implying,for instance, a “slow” variation of the synthesized resolutionoverthewho<strong>le</strong>fieldofview.Whi<strong>le</strong> the sing<strong>le</strong>-field and wide-field dirty beam expressionsseem very different, they share the same property of expressingthe way the interferometer is used to synthesize a <strong>tel</strong>escope oflarger diameter in the image plane. In other words, the samplingfunction for sing<strong>le</strong>-field imaging and D for wide-field imagingexpress the sensitivity of the interferometer to a given spatialfrequency. These uv space functions are cal<strong>le</strong>d the transfer functionsof the interferometer (Thompson et al. 1986, Chap. 5).Modifying the transfer function has a direct impact on the measuredquantity. Once the interferometer is designed and the observationsare done, the only way to change this transfer functionis data weighting.An ideal set of wide-field dirty beams, D(α ′ , α ′′ ), would havethe following properties. All the wide-field dirty beams shouldbe identical (i.e., independent of the α ′′ sky coordinate) andequal to a narrow Gaussian (its FWHM giving the image resolution).This would give the product of a wide Gaussian of u ′ bya Dirac function of u ′′ , as the ideal wide-field transfer function,D(u ′ ,u ′′ ).Page 10 of 215.2. Dirty beam shapes and weightingWhen imaging sing<strong>le</strong>-field observations, giving a multiplicativeweight to each visibility samp<strong>le</strong> is an easy way to modify theshape of the dirty beam and thus the properties of the dirtyand deconvolved images. Natural weighting (which maximizessignal-to-noise ratio), robust weighting (which maximizes resolution),and tapering (which enhances brightness sensitivity atthe cost of a lower resolution) are the most popular weightingtechniques (see e.g. Sramek & Schwab 1989).In the case of wide-field synthesis, a multiplicative weightcan also be attributed to each visibility samp<strong>le</strong> before anyprocessing. However, the weighting is also at the heart of thewide-field synthesis because it is an essential part of the shiftand-averageoperation. No constraint has been set on the weightingfunction up to this point, which indicates that the weightingfunction (W) gives us a degree of freedom in the imaging process.We look in turn at both kinds of weighting. In both cases, anobvious issue is the definition of the optimum weighting functions.As in the case of sing<strong>le</strong>-field imaging, there is no sing<strong>le</strong>answer to this question. It depends on the conditions of the observationand on the imaging goals.5.2.1. Weighting the measured visibilitiesNatural weighting consists of slightly changing the definitionof the sampling function. It is now set to a normalized naturalweight where there is a measure and 0 elsewhere. The naturalweight is usually defined as the inverse of the thermal noisevariance, computed from the radiometric equation, i.e., from thesystem temperature, the frequency resolution, and the integrationtime. Using this weighting scheme before computing thefirst Fourier transform along the α s sky dimension makes sensebecause the observing conditions (and thus the noise) vary fromvisibility to visibility.We propose to generalize this weighting scheme to otherobserving conditions than just the system noise. Indeed, criticallimitations of interferometric wide-field imaging are pointingerrors, tracking errors, atmospheric phase noise (in the(sub)-millimeter domain), etc. Whi<strong>le</strong> techniques exist for copingwith these prob<strong>le</strong>ms (e.g., water vapor radiometer, directiondependentgains: Bhatnagar et al. 2008), they are not perfect.The usual way to deal with the remaining prob<strong>le</strong>ms is to flag thesource data based on a priori know<strong>le</strong>dge of the prob<strong>le</strong>ms, e.g.,pointing measurement, tracking errors, rms phase noise on calibrators,etc. However, flagging involves the definition of thresholds,whi<strong>le</strong> reality is never black and white. It can thus be askedwhether some weighting scheme could be devised to minimizethe effect of pointing errors, tracking errors or phase noise onthe resulting image. We propose to modulate natural weightingbased on the a priori know<strong>le</strong>dge of the observing conditions.5.2.2. Weighting the synthesized visibilitiesRobust weighting or tapering the measured visibilities do notmake sense in wide-field synthesis because the dirty image ismade from the synthesized visibilities after the first Fouriertransform along the α s sky dimension. A weighting function Wthen appears naturally as part of the shift-and-average operator.Its optimum value depends on the properties of the measuredsampling function. Here are a few examp<strong>le</strong>s.Infinite, continuous sampling. This is the ideal case studied inSect. 3.1. Knowing that the Ekers & Rots Eq. (15) links the
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2.7 ANIMATION ET DIFFUSION DE LA CU
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2.8 PARCOURS 131992-1993 ÉCOLE NOR
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Chapitre 3Copyright: IRAM/PdBIIntro
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