Design, development and verification of the 30 and 44 GHz front-end modules for the Planck Low Frequency Instrument

We give a description of the design, construction and testing of the 30 and 44 GHz Front End Modules (FEMs) for the Low Frequency Instrument (LFI) of the Planck mission to be launched in 2009. The scientific requirements of the mission determine the performance parameters to be met by the FEMs, including their linear polarization characteristics. The FEM design is that of a differential pseudo-correlation radiometer in which the signal from the sky is compared with a 4-K blackbody load. The Low Noise Amplifier (LNA) at the heart of the FEM is based on indium phosphide High Electron Mobility Transistors (HEMTs). The radiometer incorporates a novel phase-switch design which gives excellent amplitude and phase match across the band. The noise temperature requirements are met within the measurement errors at the two frequencies. For the most sensitive LNAs, the noise temperature at the band centre is 3 and 5 times the quantum limit at 30 and 44 GHz respectively. For some of the FEMs, the noise temperature is still falling as the ambient temperature is reduced to 20 K. Stability tests of the FEMs, including a measurement of the 1/f knee frequency, also meet mission requirements. The 30 and 44 GHz FEMs have met or bettered the mission requirements in all critical aspects. The most sensitive LNAs have reached new limits of noise temperature for HEMTs at their band centres. The FEMs have well-defined linear polarization characteristcs.Comment: 39 pages, 33 figures (33 EPS files), 12 tables. Planck LFI technical papers published by JINST: http://www.iop.org/EJ/journal/-page=extra.proc5/1748-022

Recursive receiver down-converters with multiband feedback and gain-reuse for low-power applications

Power minimization in wireless transceivers has become increasingly critical in recent years with the emergence of standards for short-distance applications in the 900 MHz and 2.4 GHz industrial, scientific and medical (ISM) radio bands. The demand for long battery life and better portability in such applications has led to extensive research on low power radio architectures. This dissertation introduces receiver topologies for low-power systems and presents a theoretical performance analysis of the topologies. Two fully integrated receiver down-converters that demonstrate the concept are implemented in a 0.13-[mu]m CMOS technology. These topologies employ merged mixers and IF amplifiers in order to reduce power dissipation for a given dynamic range performance. In the described topologies, the input stage of a mixer is used to simultaneously provide conversion gain and baseband amplification. This is achieved by applying the down-converted IF signal to input of the mixer. Consequently, the effective conversion gain of the design is greatly enhanced with current requirement primarily determined by the input transconductor. Potential degradation mechanisms related to instability and second-order distortion are identified and solved by the use of appropriate circuit techniques. Noise and linearity performance of the down-converters is analyzed and compared to that of conventional cascaded design counterparts. The potential for enhancement of IIP3 performance through cancellation of nonlinear products is discussed. Potential extensions of the above work including feedback-based architectures that exploit multiple loops for further maximizing the power efficiency of receiver front-ends are also presented.Electrical and Computer Engineerin

The linearity response of the Planck-LFI flight model receivers

In this paper we discuss the linearity response of the Planck-LFI receivers, with particular reference to signal compression measured on the 30 and 44 GHz channels. In the article we discuss the various sources of compression and present a model that accurately describes data measured during tests performed with individual radiomeric chains. After discussing test results we present the best parameter set representing the receiver response and discuss the impact of non linearity on in-flight calibration, which is shown to be negligible.Comment: this paper is part of the Prelaunch status LFI papers published on JINST: http://www.iop.org/EJ/journal/-page=extra.proc5/jinst; This is an author-created, un-copyedited version of an article accepted for publication in JINST. IOP Publishing Ltd is not responsible for any errors or omissions in this version of the manuscript or any version derived from it. The definitive publisher authenticated version is available online at 10.1088/1748-0221/4/12/T12011