DocumentCode :
8794
Title :
30-50 GHz high-gain CMOS UWB LNA
Author :
Ge Liang Yang ; Faen Liu ; Muhammad, Ajmal ; Zhigong Wang
Author_Institution :
Inst. of RF- & OE-ICs, Southeast Univ., Nanjing, China
Volume :
49
Issue :
25
fYear :
2013
fDate :
December 5 2013
Firstpage :
1622
Lastpage :
1623
Abstract :
A 30-50 GHz CMOS ultra-wideband (UWB) low-noise amplifier (LNA) with a flat high power gain (S21), along with a flat low-noise figure (NF) is demonstrated for the Atacama large millimetre array (ALMA) band-1 (31.3-45 GHz) system applications. The high S21 and low NF are achieved because the triple-well transistors are utilised with their respective source and body terminals connected together. Furthermore, the bandwidth extension and gain flatness is achieved due to the careful design of the inductive-peaking networks. The LNA has a measured S21 of 21.5 ± 1.5 dB, a minimum NF (NFmin) of 3.8 dB at 32.5 GHz, an average NF (NFavg) of 4.67 dB over the range of 30-50 GHz and an input third-order intercept point (IIP3) of 0 dBm, with a DC power consumption of 20.4 mW at 1.2 V supply. The proposed LNA outperforms all the reported commercial standard CMOS Q-band LNAs, with the highest gain bandwidth product and highest IIP3 suitable for the ALMA band-1 system applications.
Keywords :
CMOS analogue integrated circuits; low noise amplifiers; power consumption; radioastronomical techniques; ultra wideband technology; ALMA band-1 system applications; Atacama large millimetre array; CMOS Q-band LNA; CMOS ultra-wideband low-noise amplifier; DC power consumption; IIP3; NF; bandwidth extension; body terminals; flat high power gain; flat low-noise figure; frequency 30 GHz to 50 GHz; gain bandwidth; gain flatness; high-gain CMOS UWB LNA; inductive-peaking networks design; input third-order intercept point; power 20.4 mW; radio astronomical array; triple-well transistors; voltage 1.2 V;
fLanguage :
English
Journal_Title :
Electronics Letters
Publisher :
iet
ISSN :
0013-5194
Type :
jour
DOI :
10.1049/el.2013.2625
Filename :
6678462
Link To Document :
بازگشت