• 한국통신학회논문지
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• 제27권6C호
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• pp.619-624
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• 2002

본 논문에서는 50%의 duty cycle 출력을 가지며, 디지털 방식으로 분주수를 제어할 수 있는 새로운 분주기 구조를 제안하였다. 그리고 0.25$\mu\textrm{m}$ 2-poly, 5-metal CMOS 공정 파라미터를 이용한 HSPICE 모의실험을 통해서 제안한 주파수 분주기를 이용한 900MHz 주파수 합성기를 설계하였다. 제안한 주파수 분주기의 동작은 0.657m 2-poly, 2-metal CMOS 공정을 사용하여 제작한 칩을 측정하여 확인하였다. 설계한 전압제어발진기(VCO)는 2.5V 전원전압 하에서 900Mh의 충간주파수, $\pm$10%의 동작 범위, 154MHz/V의 이득을 가진다. 또한 모의실험 결과 주파수 합성기의 settling time은 약 $1.5\mu\textrm{m}$이고 짝수와 홀수 분주시 50%의 duty cycle과 820MHz~1GHz의 동작 주파수 범위를 갖으며, 전력소모는 대략 70mW 임을 확인하였다.

• 한국전자파학회논문지
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• 제21권3호
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• pp.315-320
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• 2010

본 논문에서는 휴대 단말기에 내장이 가능한 소형화된 지상파 DMB(Digital Multimedia Broadcasting) 안테나의 설계 및 구현에 관하여 연구하였다. 제작된 안테나의 크기는 30 mm$\times$5 mm$\times$0.6 mm로서 Kapton 재질의 유전체전, 후면에 안테나 방사체가 미엔더 구조로 설계되어 있으며, 비아 홀을 통해 양쪽이 서로 연결되는 구조를 가진다. 또한 유전체 후면에 기생 소자를 배치하고 정합 소자로 220 nH의 인덕터를 사용함으로써, 안테나 소형화로 인해 부족해진 공진 길이를 보상하는 한편, 제한된 공간 내에서 정확한 공진 주파수를 가진 안테나를 구현할 수 있었다. 제안된 안테나의 이득은 중심 채널인 195 MHz에서 -13.01 dBi를 나타내었으며, 하위 채널인 174 MHz와 상위 채널인 216 MHz에서는 각각 -17.60 dBi와 -14.98 dBi의 이득 특성을 나타내었다.

• Journal of Electrical Engineering and Technology
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• 제13권5호
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• pp.2045-2049
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• 2018

An antenna arrays for a satellite navigation systems require more antenna elements to mitigate multiple jamming signals. In order to maintain the small array size while increasing the number of antenna elements, miniaturization technique is essential for antenna design. In this work, an electrically small circular microstrip patch antenna with a 3 dB hybrid coupler is designed as an element antenna, where the 3 dB hybrid coupler can yield the circularly polarized radiation characteristic. The miniaturized element antenna typically has too large capacitance in GPS L1 and GLONASS G1 bands, making it difficult to match with a single stand-alone non-Foster matching circuit (NFMC) in a stable state. Therefore, we propose a new matching technique, referred to as the hybrid matching method, which consists of a NFMC and a passive circuit. This passive tuning circuit manages reactance of antenna elements at an appropriate capacitance without a pole in the operating frequency range. The antenna array is fabricated, and the measured results show a reflection coefficient of less than -10 dB and an isolation of greater than 50 dB. In addition, peak gain of the proposed antenna is increased by 22.3 dB compared to the antenna without the hybrid matching network.

• 한국항행학회논문지
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• 제17권6호
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• pp.646-651
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• 2013

본 논문에서는 집중소자인 캐패시터 및 저항을 사용하여 특성조절이 가능한 소형 역-F 안테나를 제안하였다. 캐패시터는 안테나 크기 및 공진주파수의 조절을 위해 안테나 종단과 접지면 사이에 삽입된다. 반면에 $0{\Omega}$ 저항은 접지면과 단락되는 선로를 대체하여 구현한 것으로써, 단락점의 위치 이동은 안테나의 입력임피던스를 변화시킬 수 있다. 따라서 구조의 재설계 없이도 적절한 캐패시터 및 단락점 위치 선택으로 최적의 안테나 특성을 얻을 수 있다. 이와 같은 본 논문의 타당성 검증을 위하여 2.4 GHz 대역용 안테나를 설계 및 제작하여 지그비 무선 리모컨의 한 제품에 적용하였다. 적용된 안테나의 크기는 $8.5{\times}4.5mm^2$이며 재설계 없이도 대역폭 150 MHz 및 이득 2 dBi의 측정결과를 얻을 수 있다.

• Geomechanics and Engineering
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• 제14권2호
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• pp.161-174
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• 2018

The present study investigates the soil-structure interaction (SSI) effects on the seismic performance of smart base-isolated structures. The adopted control algorithm for tuning the control force plays a key role in successful implementation of such structures; however, in most studied carried out in the literature, these algorithms are designed without considering the SSI effect. Considering the SSI effects, a linear quadratic regulator (LQR) controller is employed to seismic control of a smart base-isolated structure. A particle swarm optimization (PSO) algorithm is used to tune the gain matrix of the controller in both cases without and with SSI effects. In order to conduct a parametric study, three types of soil, three well-known earthquakes and a vast range of period of the superstructure are considered for assessment the SSI effects on seismic control process of the smart-base isolated structure. The adopted controller is able to make a significant reduction in base displacement. However, any attempt to decrease the maximum base displacement results in slight increasing in superstructure accelerations. The maximum and RMS base displacements of the smart base-isolated structures in the case of considering SSI effects are more than the corresponding responses in the case of ignoring SSI effects. Overall, it is also observed that the maximum and RMS base displacements of the structure are increased by increasing the natural period of the superstructure. Furthermore, it can be concluded that the maximum and RMS superstructure accelerations are significant influenced by the frequency content of earthquake excitations and the natural frequency of the superstructure. The results show that the design of the controller is very influenced by the SSI effects. In addition, the simulation results demonstrate that the ignoring the SSI effect provides an unfavorable control system, which may lead to decline in the seismic performance of the smart-base isolated structure including the SSI effects.

• Advances in aircraft and spacecraft science
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• 제4권2호
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• pp.145-167
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• 2017

The presented paper gives an overview of several projects addressing the experimental characterization and control of the buffet phenomenon on 3D turbulent wings in transonic flow conditions. This aerodynamic instability induces strong wall pressure fluctuations and therefore limits flight domain. Consequently, to enlarge the latter but also to provide more flexibility during the design phase, it is interesting to try to delay the buffet onset. This paper summarizes the main investigations leading to the achievement of open and closed-loop buffet control and its experimental demonstration. Several wind tunnel tests campaigns, performed on a 3D half wing/fuselage body, enabled to characterize the buffet aerodynamic instability and to study the efficiency of innovative fluidic control devices designed and manufactured by ONERA. The analysis of the open-loop databases demonstrated the effects on the usual buffet characteristics, especially on the shock location and the separation areas on the wing suction side. Using these results, a closed-loop control methodology based on a quasi-steady approach was defined and several architectures were tested for various parameters such as the input signal, the objective function, the tuning of the feedback gain. All closed-loop methods were implemented on a dSPACE device able to estimate in real time the fluidic actuators command calculated mainly from the unsteady pressure sensors data. The efficiency of delaying the buffet onset or limiting its effects was demonstrated using the quasi-steady closed-loop approach and tested in both research and industrial wind tunnel environments.

• 한국전자파학회논문지
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• 제21권6호
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• pp.670-680
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• 2010

본 논문에서는 0.13 ${\mu}m$ CMOS 공정을 사용하여, 이동단말기 탑재에 적합한 저 전력, 저 잡음 구조 개별 소자 (LNA, Mixer, VCO, frequency doubler, signal generator, down converter)들을 제안하고, 나아가 이를 하나의 칩으로 집적화 시킨 60 GHz 단일 칩 수신기 구조를 제안한다. 저전력화를 위해 current re-use 구조를 적용시킨 LNA의 경우, 11.6 mW 의 전력 소모 시, 56 GHz부터 60 GHz까지 측정된 잡음지수(NF)는 4 dB 이하이다. 저전력화를 위한 resistive mixer의 경우, Cgs의 보상 회로를 통하여 낮은 LO 신호 크기에서도 동작 가능하도록 하였다. -9.4dB의 변환 이득을 보여주며, 20 dB의 LO-RF isolation 특성을 가진다. Ka-band VCO는 4.99 mW 전력 소모 시측정된 출력 신호 크기는 27.4 GHz에서 -3 dBm이 되며, 26.89 GHz에서부터 1 MHz offset 기준으로 -113 dBc/Hz의 phase noise 특성을 보인다. 49.2 dB의 원신호 억제 효과를 보이는 Frequency Doubler는 총 전력 소모가 9.08 mW일 경우, -4 dBm의 27.1 GHz 입력 신호 인가 시 -53.2 dBm의 fundamental 신호(27.1 GHz)와 -4.45dBm의 V-band second harmonic 신호(54.2 GHz)를 얻을 수 있었으며, 이는 -0.45 dB의 변환 이득을 나타낸다. 60 GHz CMOS 수신기는 LNA, resistive mixer, VCO, frequency doubler, 그리고 drive amplifier로 구성되어 있으며, 전체 전력 소모는 21.9 mW이다. WLAN과의 호환 가능성을 위하여, IF(Intermediate Frequency) bandwidth가 5.25GHz(4.75~10 GHz)이며, RF 3 dB bandwidth는 58 GHz를 중심으로 6.2 GHz이다. 이때의 변환 손실은 -9.5 dB이며, 7 dB의 NF와 -12.5 dBm의 높은 입력 P1 dB를 보여주고 있다. 이는 60 GHz RF 회로의 저전력화, 저가격화, 그리고 소형화를 통한 WPAN용 이동단말기의 적용 가능성을 입증한다.

• 한국광학회지
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• 제15권5호
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• pp.455-460
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• 2004

1.064 $\mu\textrm{m}$ 파장의 연속발진 Nd:YAG 레이저를 펌핑 광원으로 하여 적외선 영역에서 광대역으로 파장 가변되는 연속발진 및 극초단펄스 C $r^{4+}$ :YAG 레이저를 자체 제작하였다. C $r^{4+}$ :YAG 레이저의 연속발진 및 펄스의 출력특성과 파장 가변 영역은 다음과 같다. 연속발진일 경우 1.436 $\mu\textrm{m}$에서 600 mW의 평균출력을 보였으나, 복굴절 필터를 삽입했을 경우는 1.492 $\mu\textrm{m}$근처에서 400 mW의 평균출력을 보였다. 펄스발진일 경우 1.436 $\mu\textrm{m}$에서 최초로 평균출력 320 mW의 모드록킹된 펄스가 발생하였지만 물 흡수대의 영향으로 불안정함을 피할 수 없었다. 따라서, 복굴절 필터를 사용하여 중심파장을 1.492 $\mu\textrm{m}$로 이동시켰으며 이 영역에서 안정한 상태의 모드록킹된 43 fs의 극초단 펄스를 생성하였다. 이 때의 평균출력은 280 mW이고, 반치폭(FWHM)은 45 nm이었다.

• 대한조선학회논문집
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• 제55권5호
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• pp.401-414
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• 2018

Planing hull type ships are often equipped with interceptor or trim tab to improve the excessive trim angle which leads to poor resistance and sea keeping performances. The purpose of this study is to design a controller to control the attitude of the ship by controllable stern interceptor and validate the effectiveness of the attitude control by the towing tank test. Embedded controller, servo motor and controllable stern interceptor system were equipped with planing hull type model ship. Prior to designing the control algorithm, a model test was performed to identify the system dynamic model of the planing hull type ship including the stern interceptor. The matrix components of model were optimized by Genetic Algorithm. Using the identified model, PID controller which is a classical controller and sliding mode controller which is a nonlinear robust controller were designed. Gain tuning of the controllers and running simulation was conducted before the towing tank test. Inserting the designed control algorithm into the embedded controller of the model ship, the effectiveness of the active control of the stern interceptor was validated by towing tank test. In still water test with small disturbance, the sliding mode controller showed better performance of canceling the disturbance and the steady-state control performance than the PID controller.

• Asian-Australasian Journal of Animal Sciences
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• 제32권12호
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• pp.1836-1843
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• 2019

Objective: Social genetic effects (SGE) are an important genetic component for growth, group productivity, and welfare in pigs. The present study was conducted to evaluate i) the feasibility of the single-step genomic best linear unbiased prediction (ssGBLUP) approach with the inclusion of SGE in the model in pigs, and ii) the changes in the contribution of heritable SGE to the phenotypic variance with different scaling ${\omega}$ constants for genomic relationships. Methods: The dataset included performance tested growth rate records (average daily gain) from 13,166 and 21,762 pigs Landrace (LR) and Yorkshire (YS), respectively. A total of 1,041 (LR) and 964 (YS) pigs were genotyped using the Illumina PorcineSNP60 v2 BeadChip panel. With the BLUPF90 software package, genetic parameters were estimated using a modified animal model for competitive traits. Giving a fixed weight to pedigree relationships (${\tau}:1$), several weights (${\omega}_{xx}$, 0.1 to 1.0; with a 0.1 interval) were scaled with the genomic relationship for best model fit with Akaike information criterion (AIC). Results: The genetic variances and total heritability estimates ($T^2$) were mostly higher with ssGBLUP than in the pedigree-based analysis. The model AIC value increased with any level of ${\omega}$ other than 0.6 and 0.5 in LR and YS, respectively, indicating the worse fit of those models. The theoretical accuracies of direct and social breeding value were increased by decreasing ${\omega}$ in both breeds, indicating the better accuracy of ${\omega}_{0.1}$ models. Therefore, the optimal values of ${\omega}$ to minimize AIC and to increase theoretical accuracy were 0.6 in LR and 0.5 in YS. Conclusion: In conclusion, single-step ssGBLUP model fitting SGE showed significant improvement in accuracy compared with the pedigree-based analysis method; therefore, it could be implemented in a pig population for genomic selection based on SGE, especially in South Korean populations, with appropriate further adjustment of tuning parameters for relationship matrices.