J. Pety and N. Rodríguez-Fernández: Revisiting the theory of interferometric wide-field synthesis<strong>tel</strong>-<strong>00726959</strong>, version 1 - 31 Aug 2012quantity we want to estimate, i.e., I, to many noisy 5 measurements,V(u p , u s ), via a product by B (assumed to be perfectlydefined), we can invoke a simp<strong>le</strong> <strong>le</strong>ast-squares argument (seee.g. Bevington & Robinson 2003) to demonstrate that the optimumweighting function isW ( u p , u − u p)=w ( u p , u − u p)B(up − u )∫u pw ( u p , u − u p)B2 ( u p − u ) du p, (60)with w(u p , u s ) the weight computed from the inverse of thenoise variance of V(u p , u s ). Using Eq. (20), it is then easyto demonstrate that D(u) = 1, and then I dirty (α) = I(α). Thedirty image is a direct estimate of the sky brightness; i.e.,deconvolution is superfluous.Comp<strong>le</strong>te sampling. The signal is Nyquist-samp<strong>le</strong>d, but it has afinite support in both the uv and sky planes, implying a finitesynthesized resolution and a finite field of view. In contrastto the previous case, this one may have practical applications,e.g., observations done with ALMA in its compactconfiguration. Indeed, the large number of independent baselinescoup<strong>le</strong>d to the design of the ALMA compact configurationensure a comp<strong>le</strong>te, almost Gaussian, sampling for eachsnapshot. In this case, the best choice may be to choose theweighting function so that all the dirty beams are identical tothe same Gaussian function. In this case, the deconvolutionwould also be superfluous.Incomp<strong>le</strong>te sampling. This is the more general case studied inSect. 3.2. The signal not only has a finite support but it alsois undersamp<strong>le</strong>d (at <strong>le</strong>ast in the uv plane). The deconvolutionis mandatory. The choice of the weighting function thus willdepend on imaging goals.If the user needs the best signal-to-noise ratio, some kindof natural weighting will be needed. It is tempting to useEq. (60) as a natural weighting scheme. However, the maincondition for derivation of this weighting function, i.e., theEkers & Rots Eq. (15), is not valid anymore, as the noisymeasured quantity (SV) is now linked to the quantity wewant to estimate (I) by a local average (see Eq. (31)). Thisis why it was more appropriate to try to get a Gaussian dirtybeam shape in the comp<strong>le</strong>te sampling case.If the signal-to-noise ratio is high enough, the user has twochoices. Either he/she wants to maximize angular resolutionpower and needs some kind of robust weighting, or he/shewants to get the more homogeneous dirty beam shape overthe who<strong>le</strong> field of view. This requirement cannot always befully met. The Ekers & Rots scheme enab<strong>le</strong>s us to recoverunmeasured spatial frequencies only in regions near to measuredones, because B has a finite support.5.3. DeconvolutionWriting the image-plane measurement equation in aconvolution-like way is very interesting because all thedeconvolution methods developed in the past 30 years areoptimized to treat deconvolution prob<strong>le</strong>ms (see e.g. Högbom1974; Clark 1980; Schwab 1984; Narayan & Nityananda 1986).For instance, it should be possib<strong>le</strong> to deconvolve Eq. (23) withjust slight modifications to the standard CLEAN algorithms.Indeed, Eq. (23) can be interpreted as the convolution of the5 The noise is assumed to have a Gaussian probability distributionfunction.sky brightness by a set of dirty beams, so that the only change,once a CLEAN component is found, would be the need to findthe right dirty beam in this set in order to remove the CLEANcomponent from the residual image.Following Clark (1980)andSchwab (1984), most algorithmstoday deconvolve in alternate minor and major cyc<strong>le</strong>s. During aminor cyc<strong>le</strong>, a solution of the deconvolution is sought with a simplified(hence approximate) dirty beam. During a major cyc<strong>le</strong>,the current solution is subtracted either from the original dirtyimage using the exact dirty beam or from the measured visibilities,implying a new gridding step. In both cases, the major cyc<strong>le</strong>sresult in greater accuracy. The iteration of minor and majorcyc<strong>le</strong>s enab<strong>le</strong>s one to find an accurate solution with better computingefficiency. In our case, the approximate dirty beams usedin the minor cyc<strong>le</strong> could be 1) dirty beams of a much smal<strong>le</strong>r sizethan the image; or 2) a reduced set of dirty beams (i.e., guessingthat the typical variation sizesca<strong>le</strong> of the dirty beams with thesky coordinate is much larger than the primary beamwidth); or3) both simultaneously. The model would be subtracted from theoriginal visibilities before re-imaging at each major cyc<strong>le</strong>. Thetrade-off is between the memory space needed to store a full setof accurate dirty beams and the time needed to image the data ateach major step. Some quantitative analysis is needed to knowhow far the dirty beams can be approximated in the minor cyc<strong>le</strong>.It is worth noting that the accuracy of the deconvolved imagewill be affected by edge effects. Indeed, the dirty brightnessat the edges of the observed field of view is attenuated by the primarybeam shape. When deconvolving these edges, the deconvolvedbrightness will be <strong>le</strong>ss precise, because the primary beamhas a low amplitude there. This only affects the edges, becauseinside the field of view, every sky position should be observed afraction of the time with a primary beam amplitude between 0.5and 1. This edge effect is neverthe<strong>le</strong>ss expected to be much <strong>le</strong>sstroub<strong>le</strong>some than the inhomogeneous noise <strong>le</strong>vel resulting fromstandard mosaicking imaging (see Sect. 7.1).6. Short spacings6.1. The missing flux prob<strong>le</strong>mRadio interferometers are bandpass instruments; i.e., they filterout not only the spacings longer than the largest baseline <strong>le</strong>ngthbut also the spacings shorter than the shortest baseline <strong>le</strong>ngth,which is typically comparab<strong>le</strong> to the diameter of the interferometerantennas. In particular, radio interferometers do not measurethe visibility at the center of the uv plane (the so-cal<strong>le</strong>d “zerospacing”), which is the total flux of the source in the measuredfield of view.The lack of short baselines or short spacings has strong effectsas soon as the size of the source is more than about 1/3 to1/2 of the interferometer primary beam. Indeed, when the sizeof the source is small compared to the primary beam of the interferometer,the deconvolution algorithms use, in one way oranother, the information of the flux at the lowest measured spatialfrequencies for extrapolating the total flux of the source. Theextreme case is a point source at the phase center for which theamplitude of all the visibilities is constant and equal to the totalflux of the source: extrapolation is then exact. However, thelarger the size of the source, the worse the extrapolation, whichthen underestimates the total source flux. This is the well-knownprob<strong>le</strong>m of the missing flux that observers sometimes note whencomparing a source flux measured by a mm interferometer withthe flux observed with a sing<strong>le</strong>-dish antenna.Page 11 of 21
A&A 517, A12 (2010)<strong>tel</strong>-<strong>00726959</strong>, version 1 - 31 Aug 2012Fig. 4. Length of the averaging linepaths displayed as black lines inpanel c.2) of Fig. 2, as a function of the spatial sca<strong>le</strong> in the final, widefielduv plane. In the case of a continuous sampling of u p between d minand d max , these quantities can be interpreted as the number of measuresthat contribute to the estimate of I(u).Wide-field synthesis does not recover the full short spacings.Let us assume that the visibility function is continuouslysamp<strong>le</strong>d from d min to d max , with d min ∼ 1.5 d prim . The <strong>le</strong>ngth ofthe averaging linepath 6 ), L(u), can be interpreted as the numberof measures that contribute to the estimation of I(u). Figure 4shows the variations of L(u) function when starting from a visibilityfunction continuously defined in the [d min , d max ]intervalalong the u p dimension. We can expect to recover I(u) onlyinside the [d min − d prim , d max + d prim ] interval. In particular, informationon short spacings lower than d min − d prim (e.g. thecrucial zero spacing) cannot be recovered when using a homegeneousinterferometer, and the short spacings in the interval[d min − d prim , d min ] are recovered with increasing accuracy fromd min − d prim to d min .Botheffects imply the need for comp<strong>le</strong>mentaryinstruments to accura<strong>tel</strong>y measure the missing shortspacings.6.2. Usual hardware and software solutionsTo derive the correct result for larger source sizes, it is necessaryto comp<strong>le</strong>ment the interferometer data with additionaldata, which contain the missing short-spacing information. TheIRAM-30 m sing<strong>le</strong>-dish <strong>tel</strong>escope is used to comp<strong>le</strong>ment thePlateau de Bure Interferometer. Short-spacing information canalso be in part recovered with a secondary array of smal<strong>le</strong>r antennasand shorter baselines (e.g. the CARMA interferometer).In the ALMA project, the short-spacing information will be derivedby a combination of four 12 m-sing<strong>le</strong>-dish antennas andan interferometer of 12 antennas of 7 m cal<strong>le</strong>d ACA (AtacamaCompact Array).From the software point-of-view, two main families of algorithmsexist in the standard processing of mosaics. Either theshort-spacing information is combined on the deconvolved image(i.e., the interferometer data is imaged and deconvolved separa<strong>tel</strong>y)through a hybridization in the Fourier plane (see e.g.Pety et al. 2001), or the long and short-spacing informationis imaged and/or deconvolved jointly. In this category, we findthe pseudo-visibility technique, which produces interferometriclikevisibilities from sing<strong>le</strong>-dish maps (see e.g. Pety et al. 2001;Rodríguez-Fernández et al. 2008, and references therein), andthe multi-resolution deconvolution algorithms, which work onimages containing different spatial frequency ranges.In the next two sections, we show how wide-field synthesisnaturally processes the short-spacing information either fromsing<strong>le</strong>-dish or from heterogeneous arrays.6 The notion of averaging linepath has been introduced in Sect. 3.1(see in particular Eq. (16)).Page 12 of 216.3. Processing short spacings from sing<strong>le</strong>-dishmeasurementsThe sing<strong>le</strong>-dish measurement equation can be written as∫(I sd (α) = S sd (α) B sd α ′ − α ) I ( α ′) dα ′ , (61)α ′where I sd is the measured sing<strong>le</strong>-dish intensity, S sd the sing<strong>le</strong>dishsampling function, and B sd the sing<strong>le</strong>-dish antenna powerpattern. As already stated in the introduction, the above integralis identical to the ideal measurement equation of interferometricwide-field imaging taken in u p = 0. If we define a sing<strong>le</strong>-dishvisibility function as(V sd up = 0,α ) ∫(≡ B sd α ′ − α ) I ( α ′) dα ′ , (62)α ′we can thus write the measured sing<strong>le</strong>-dish intensity asI sd (α) = S sd (α) V sd(up = 0,α ) . (63)The recognition that the sing<strong>le</strong>-dish measurement equation isa particular case of the interferometric wide-field measurementequation opens the way to treating both the sing<strong>le</strong>-dish and interferometricdata sets through exactly the same processing steps.We just have to define a hybrid sampling function, S hyb ,asS hyb(up 0,α ) = S ( u p ,α ) (64)S hyb(up = 0,α ) = S sd (α) , (65)the Fourier transform of the hybrid primary beam, B hyb ,asB hyb(up 0, u ′) = B ( u p − u ′) (66)B hyb(up = 0, u ′) = B sd( −u′ ) , (67)and a hybrid weighting function, W hyb ,asW hyb(up 0, u ′ + u ′′ − u p)= Whyb(up , u ′ + u ′′ − u p), (68)W hyb(up = 0, u ′ + u ′′) = W sd( u ′ + u ′′) . (69)All the processing steps described in the previous sections (includinga potential gridding step of sing<strong>le</strong>-dish, on-the-fly data)can then be directly applied to the hybrid data set. Using thewide-field synthesis formalism, we can easily write∫(I hyb (u) = D hyb u ′ , u − u ′) I ( u ′) du ′ , (70)u ′withI hyb (u) = I dirty (u) + W sd (u) I sd (u) (71)andD hyb( u ′ , u ′′) = D ( u ′ , u ′′) +W sd( u ′ +u ′′) S sd( u′′ ) B sd( −u′ ) . (72)We thus see that I hyb is a linear combination of the informationmeasured by the sing<strong>le</strong>-dish (I sd ) and by the interferometer(I dirty ). There, W sd (u) plays a particular ro<strong>le</strong> for two reasons.First, its dependency on the spatial frequency (u) enab<strong>le</strong>s us tofilter out the highest spatial frequencies that are measured by thesing<strong>le</strong>-dish antenna with low accuracy. Second, it is well-knownthat the relative weight of the sing<strong>le</strong>-dish to interferometric datais a critical parameter in the processing of the short spacingsfrom sing<strong>le</strong>-dish data (see e.g. Rodríguez-Fernández et al. 2008).
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UNIVERSITÉ PIERRE ET MARIE CURIEHA
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Table des matières1 Rapport de sou
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Rapport après soutenanceHabilitati
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Chapitre 2Curriculum vitaetel-00726
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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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4.2 ETUDES DIRECTES EN ÉMISSION 19
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4.4 LA LUMINOSITY CO PAR MOLÉCULE
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356 E. Falgarone et al.: Extreme ve
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5.2 UNE PHYSIQUE BIEN CONTRAINTE ET
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A&A 435, 885-899 (2005)DOI: 10.1051
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