• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2001년도 추계학술대회 논문집
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• pp.410-413
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• 2001

In this paper, we present results of this that design of the multi-layer VCO(Voltage Controlled Oscillator), which is composed of the resonation circuit and the oscillation circuit, using EM simulator and nonlinear RF circuit simulator. EM simulator is used for acquiring EM(Electromagnetic) characteristics of conductor pattern as well as designing multi-layer VCO, Acquired EM characteristics of the circuit pattern was used like real components at nonlinear RF circuit simulator. Finally VCO is simulated at nonlinear RF circuit simulator. The material for the circuit pattern was Ag and the dielectric was Dupont ＃9599, which is applied for LTCC process. The structure is constructed with 4 conducting layer. Simulated results showed that the output level was about 1[dBm], the phase noise was 102 [dBc/Hz] at 30[kHz] offset frequency, the harmonics -8dBc, and the control voltage sensitivity of 30[MHz/V] with a DC current consumption of 10[mA].

• 한국정보전자통신기술학회논문지
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• 제7권4호
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• pp.188-194
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• 2014

본 논문은 LTE (0.746 ~ 0.798 GHz), GSM(0.824 ~ 0.960 GHz), DCS(1.71 ~ 1.88 GHz), WCDMA(1.91 ~ 2.17 GHz) 대역에서 사용 가능한 다중 대역 모바일 안테나에 대하여 제안하였다. 제안된 안테나는 기본적인 PIFA 구조에 두 개의 브랜치 라인을 추가하여 다중대역을 형성하고, 커플링 급전 방식을 사용하여 대역폭을 향상시킨 안테나이다. 안테나의 크기는 $122mm{\times}50mm{\times}0.8mm$이며, FR4(${\epsilon}_r=4.4$)를 사용하였으며, 측정결과 VSWR < 2(${\leq}-10dB$)을 기준으로 모든 주파수 대역을 만족하였다. 제안된 다중대역 안테나는 낮은 주파수대역에서 0.93 ~ 1.92 dBi의 이득과 49.60 ~ 76.35 %의 방사효율 특성을 보이고, 높은 주파수대역에서는 2.19 ~ 4.66 dBi의 이득과 60.40 ~ 80.01 %의 방사효율 특성을 보였다. 따라서 본 논문에서 제안한 다중대역 안테나는 현재 상용화 되어있는 이동통신 단말기용 안테나에 비해 전 대역에서 우수한 특성을 확인하였다. 이와 같은 우수한 특성으로 인하여 본 연구에서 제안된 안테나는 4세대 모바일 단말기뿐만 아니라 향후 개발하고 있는 B4G용 안테나로 적용 가능 할 것으로 판단된다.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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• pp.27.1-27.1
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• 2008

KASI (Korea Astronomy and Space Science Institute) is developing a compact wide-field survey space telescope system, MIRIS (The Multi-purpose IR Imaging System) to be launched in 2010 as the main payload of the Korea Science and Technology Satellite 3. Through recent System Design Review (SDR) and Preliminary Design Review (PDR), most of the system design concept was reviewed and confirmed. The near IR imaging system adopted short F/2 optics for wide field low resolution observation at wavelength band 0.9~2.0 um minimizing the effect of attitude control system. The mechanical system is composed of a cover, baffle, optics, and detector system using a $256\times256$ Teledyne PICNIC FPA providing a $3.67\times3.67$ degree field of view with a pixel scale of 51.6 arcsec. We designed a support system to minimize heat transfer with Muti-Layer Insulation. The electronics of the MIRIS system is composed of 7 boards including DSP, control, SCIF. Particular attention is being paid to develop mission operation scenario for space observation to minimize IR background radiation from the Earth and Sun. The scientific purpose of MIRIS is to survey the Galactic plane in the emission line of Pa$\alpha$ ($1.88{\mu}m$) and to detect the cosmic infrared background (CIB) radiation. The CIB is being suspected to be originated from the first generation stars of the Universe and we will test this hypothesis by comparing the fluctuations in I (0.9~1.2 um) and H (1.2~2.0 um) bands to search the red shifted Lyman cutoff signature.