Planck Pre-Launch Status Papers - APC - Université Paris Diderot ...
Planck Pre-Launch Status Papers - APC - Université Paris Diderot ... Planck Pre-Launch Status Papers - APC - Université Paris Diderot ...
M. Bersanelli et al.: Planck pre-launch status: Design and description of the Low Frequency InstrumentFig. 4. The LFI instrument in the configuration for instrument level testcryogenic campaign.Fig. 3. LFI RAA. Top:drawingoftheintegratedinstrumentshowingthe focal plane unit, waveguide bundle and back-end unit. The elementsthat are not part of LFI hardware (HFI front-end, cooler pipes, thermalshields) are shown in light grey. Bottom: moredetailsarevisibleintheexploded view, as indicated in the labels.the payload module after integrating the HFI 4 K box. Figure 5shows the LFI within the Planck satellite.3.3. Receiver designThe LFI receivers are based on an additive correlation concept,or pseudo-correlation, analogous to schemes used in previousapplications in early works (Blum 1959), as well as inrecent CMB experiments (Staggs et al. 1996; Jarosik et al. 2003).The LFI design introduces new features that optimise stabilityand immunity to systematics within the constraints imposed bycryogenic operation and by integration into a complex payloadsuch as Planck.TheFEMcontainsthemostsensitivepartofthereceiver, where the pseudo-correlation scheme is implemented,while the BEM provides further RF amplification and detection.In each radiometer (Fig. 6), after the OMT, the voltagesof the signal from the sky horn, x(t), and from the referenceload, y(t), are coupled to a 180 ◦ hybrid that yields the mixedsignals (x + y)/ √ 2and(x − y)/ √ 2atitstwooutputports.Thesesignals are then amplified by the cryogenic low-noise amplifiers(LNAs) characterised by noise voltage, gain, and phase n F1 , g F1 ,φ F1 and n F2 , g F2 , φ F2 .Oneofthetwosignalsthenrunsthroughaswitchthatshiftsthephasebetween0and180 ◦ at a frequencyof 4096 Hz. A second phase switch is mounted for symmetry andredundancy on the other radiometer leg, but it does not introduceany switching phase shift. The signals are then recombined by asecond 180 ◦ hybrid coupler, thus producing an output, which isasequenceofsignalsproportionaltox(t) andy(t) alternatingattwice the phase switch frequency.In the back-end modules (Fig. 6), the RF signals are furtheramplified in the two legs of the radiometers by room temperatureamplifiers characterised by noise voltage, gain and phase n B1 ,g B1 , φ B1 and n B2 , g B2 , φ B2 .Thesignalsarefilteredandthendetectedby square-law detector diodes. A DC amplifier then booststhe signal output, which is connected to the data acquisition electronics.The sky and reference load DC signals are integrated,digitised, and then transmitted tothegroundastwoseparatedstreams of sky and reference load data.The sky and reference load signals recombined after the secondhybrid in the FEM have highly correlated 1/ f fluctuations.This is because, in each radiometer leg, both the sky and thereference signals undergo the same instantaneous fluctuationsdue to LNAs intrinsic instability. Furthermore,thefastmodulationdrastically reduces the impact of 1/ f fluctuations comingfrom the back-end amplifiers and detector diodes, since theswitch rate ∼4 kHzismuchhigherthanthe1/ f knee frequencyof the BEM components. By taking the difference between thePage 7 of 21
A&A 520, A4 (2010)Fig. 6. LFI receiver scheme, shown in the layout of a radiometer chainassembly (RCA). Some details in the receiver components (e.g., attenuators,filters, etc.) differ slightly for the different frequency bands.temperature ∼4.5 K), plus a small contribution from inherent radiometerasymmetry. To compensate for this effect, a gain modulationfactor r is introduced in software to null the output bytaking the difference ¯p = V sky − rV load ≈ 0. In the next section,we discuss the signal model in more detail.Fig. 5. Top:schematicofthePlanck satellite showing the main interfaceswith the LFI RAA on the spacecraft. Bottom:backviewofPlanckshowing the RAA integrated on the PPLM. The LFI Back-end unit is thebox below the lowest V-groove and resting on the top panel of the SVM.DC output voltages V sky and V load ,therefore,the1/ f noise ishighly reduced.Differently from the WMAP receivers, the LFI phaseswitches and second hybrids have been placed in the front end.This allows full modularity of the FEMs, BEMs, and waveguides,which in turns simplifies the integration and test procedure.Furthermore, this design does not require that the phase bepreserved in the waveguides, a major advantage given the complexrouting imposed by the LFI-HFI integration and the potentiallysignificant thermo-elastic effects from the cryogenic interfacesin the Planck payload.In principle, for a null differential output corresponding toaperfectlybalancedsystem,fluctuationswouldbefullysuppressedin the differenced data. In practice, for LFI, a residualoffset will be necessarily present due to input asymmetrybetween the sky arm (∼2.7 Kfromthesky,plus∼0.4 Kfrom the reflectors) and the reference load arm (with physical3.3.1. Signal modelIf x(t) andy(t) aretheinputvoltagesateachcomponent,thenthe transfer functions for the hybrids, the front-end amplifiers,the phase switches, and the back-end amplifiers can be written,respectively, as{ x + yf hybrid : {x,y}→ √ , x − y }√2 2famp FE : {x,y}→{ }g F1 (x + n F1 )e i φ F 1 ,gF2 (y + n F2 )e i φ F 2f sw : {x,y}→ { x,y √ A j e i θ j}, j = 1, 2f BEamp : {x,y}→{ g B1 (x + n B1 )e i φ B 1 ,gB2 (y + n B2 )e i φ B 2}, (11)where θ 1 and θ 2 are the phase shifts in the two switch states(nominally, θ 1 = 0andθ 2 = 180 ◦ ), n F and n B represent the whitenoise of the front-end and back-end amplifiers, and A 1 and A 2represent the fraction of the signal amplitude that is transmittedafter the phase switch in the two states (for a lossless switchA 1 = A 2 = 1). Based on these transfer functions and on thetopology of the LFI receiver discussed above, we developed adetailed analytical description of the receiver and evaluated itssusceptibility to systematic effects by studying the impact of deviationfrom ideal radiometer behaviour on the differenced output(Seiffert et al. 2002; Mennella et al. 2002a). In addition tothe analytical treatment, a numerical model of the RCA signalshas been developed (Battaglia et al. 2009).For small phase mismatches and assuming negligible phaseswitch imbalance, the power output of the differenced signal afterapplying the gain modulation factor is given by[(∆p=akβ ˜T A,sky (G − rI)−r ˜T A,load G − 1 ) ]r I +(1 − r)T sys . (12)Page 8 of 21
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A&A 520, A4 (2010)Fig. 6. LFI receiver scheme, shown in the layout of a radiometer chainassembly (RCA). Some details in the receiver components (e.g., attenuators,filters, etc.) differ slightly for the different frequency bands.temperature ∼4.5 K), plus a small contribution from inherent radiometerasymmetry. To compensate for this effect, a gain modulationfactor r is introduced in software to null the output bytaking the difference ¯p = V sky − rV load ≈ 0. In the next section,we discuss the signal model in more detail.Fig. 5. Top:schematicofthe<strong>Planck</strong> satellite showing the main interfaceswith the LFI RAA on the spacecraft. Bottom:backviewof<strong>Planck</strong>showing the RAA integrated on the PPLM. The LFI Back-end unit is thebox below the lowest V-groove and resting on the top panel of the SVM.DC output voltages V sky and V load ,therefore,the1/ f noise ishighly reduced.Differently from the WMAP receivers, the LFI phaseswitches and second hybrids have been placed in the front end.This allows full modularity of the FEMs, BEMs, and waveguides,which in turns simplifies the integration and test procedure.Furthermore, this design does not require that the phase bepreserved in the waveguides, a major advantage given the complexrouting imposed by the LFI-HFI integration and the potentiallysignificant thermo-elastic effects from the cryogenic interfacesin the <strong>Planck</strong> payload.In principle, for a null differential output corresponding toaperfectlybalancedsystem,fluctuationswouldbefullysuppressedin the differenced data. In practice, for LFI, a residualoffset will be necessarily present due to input asymmetrybetween the sky arm (∼2.7 Kfromthesky,plus∼0.4 Kfrom the reflectors) and the reference load arm (with physical3.3.1. Signal modelIf x(t) andy(t) aretheinputvoltagesateachcomponent,thenthe transfer functions for the hybrids, the front-end amplifiers,the phase switches, and the back-end amplifiers can be written,respectively, as{ x + yf hybrid : {x,y}→ √ , x − y }√2 2famp FE : {x,y}→{ }g F1 (x + n F1 )e i φ F 1 ,gF2 (y + n F2 )e i φ F 2f sw : {x,y}→ { x,y √ A j e i θ j}, j = 1, 2f BEamp : {x,y}→{ g B1 (x + n B1 )e i φ B 1 ,gB2 (y + n B2 )e i φ B 2}, (11)where θ 1 and θ 2 are the phase shifts in the two switch states(nominally, θ 1 = 0andθ 2 = 180 ◦ ), n F and n B represent the whitenoise of the front-end and back-end amplifiers, and A 1 and A 2represent the fraction of the signal amplitude that is transmittedafter the phase switch in the two states (for a lossless switchA 1 = A 2 = 1). Based on these transfer functions and on thetopology of the LFI receiver discussed above, we developed adetailed analytical description of the receiver and evaluated itssusceptibility to systematic effects by studying the impact of deviationfrom ideal radiometer behaviour on the differenced output(Seiffert et al. 2002; Mennella et al. 2002a). In addition tothe analytical treatment, a numerical model of the RCA signalshas been developed (Battaglia et al. 2009).For small phase mismatches and assuming negligible phaseswitch imbalance, the power output of the differenced signal afterapplying the gain modulation factor is given by[(∆p=akβ ˜T A,sky (G − rI)−r ˜T A,load G − 1 ) ]r I +(1 − r)T sys . (12)Page 8 of 21