• Bulletin of the Korean Chemical Society
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• 제15권8호
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• pp.631-636
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• 1994

For the Schlogl model with the second order transition under the influence of the multiplicative noise singular at the unstable steady state, the detailed discussions are presented for various kinds of stochastic phenomena, suchas the effects of parameters on stationary probability distribution, noise-induced phase transitions and escape rate.

• Journal of Power Electronics
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• 제16권4호
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• pp.1513-1525
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• 2016

Rapid and accurate phase synchronization is critical for the reliable control of grid-tied inverters. However, the commonly used software phase-locked loop methods do not always satisfy the need for high-speed and accurate phase synchronization under severe grid imbalance conditions. To address this problem, this study develops a novel open-loop phase locking scheme based on a synchronous reference frame. The proposed scheme is characterized by remarkable response speed, high accuracy, and easy implementation. It comprises three functional cascaded blocks: fast orthogonal signal generation block, fast fundamental-frequency positive sequence component construction block, and fast phase calculation block. The developed virtual orthogonal signal generation method in the first block, which is characterized by noise immunity and high accuracy, can effectively avoid approximation errors and noise amplification in a wide range of sampling frequencies. In the second block, which is the foundation for achieving fast phase synchronization within 3 ms, the fundamental-frequency positive sequence components of unsymmetrical grid voltages can be achieved with the developed orthogonal signal construction strategy and the symmetrical component method. The real-time grid phase can be consequently obtained in the third block, which is free from self-tuning closed-loop control and thus improves the dynamic performance of the proposed scheme. The proposed scheme is adaptive to severe unsymmetrical grid voltages with sudden changes in magnitude, phase, and/or frequency. Moreover, this scheme is able to eliminate phase errors induced by harmonics and random noise. The validity and utility of the proposed scheme are verified by the experimental results.

• 한국음향학회지
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• 제33권1호
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• pp.10-20
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• 2014

본 연구에서는 입수 충격에 의한 수중 순간 소음을 연구하기 위해, 황해에서 발사대를 이용하여 해상 실험을 진행하였다. 해상시험선인 청해호 우현상에서 발사대를 이용하여 실린더 몸체를 수직으로 발사하였으며, 이때 발생하는 소음을 하이드로폰으로 측정하였다. 실험에서는 원통형, 원뿔형, 반구형 두부 형상을 가진 3가지 종류의 실린더 몸체가 사용되었다. 측정된 신호는 시간적으로 확연하게 구분되어 3단계로 전시되었다 : (1) 초기 충돌 및 물체 진동단계, (2) 개방 공동 유동 단계, (3) 공동 붕괴 및 거품 진동 단계. 대부분의 경우, 거품 진동 단계의 파형이 초기 충돌 및 물체 진동 단계에 비해 우세하게 나타났다. 공동이 붕괴되기 시작하는 핀치 오프 시간은 0.18 ~ 0.2 s에 발생하였으며, 평균 거품 지속 시간은 0.9 ~ 1.3 s로 지속되었다. 입수 충격 소음은 100 Hz 이하의 대역에서 에너지가 집중되어 있었으며, 생성되는 소음은 두부 형상, 물체 질량, 발사 속도에 의해 영향을 받았다. 결과적으로, 거품 주파수에서 에너지 스펙트럼 밀도의 크기는 원통형, 원뿔형, 반구형 순으로 나타났으며, 동일 입수체에 대해서는 초기 에너지가 클수록 거품 주파수에서 에너지 스펙트럼 밀도가 크게 나타났다. 최종적으로, 버블이 폭발하는 물리적 현상을 기반으로 모의된 신호와 계측 값간 비교 결과 만족스러운 결론을 얻을 수 있었다.

• 전기전자학회논문지
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• 제26권4호
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• pp.577-583
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• 2022

위상고정루프에 대해 선형 위상-도메인 모델링을 진행하여 시스템의 안정성을 고려한 각 블록의 설계 매개 변수들을 설정한 이후 빠른 동작 특성을 확인하기 위해 Verilog-HDL 기반의 모델링을 수행할 수 있다. 이때 단순한 동작 특성뿐 아니라 위상잡음 및 비선형 특성까지 모델링에 반영할 수 있는데, 본 논문에서는 디지털-시간 변환기(DTC)의 비선형 특성 및 디지털 조정 발진기(DCO)의 위상잡음 모델링을 추가로 소개한다. 동작 모델을 사용하여 시스템 레벨의 설계를 마치면 시간-도메인 영역에서 과도 응답 시뮬레이션을 진행하여 설계 타당성을 확인할 수 있으며, 출력 신호 결과를 위상잡음 그래프로 나타내어 이를 이상적인 위상잡음 그래프와 비교함으로써 동작과 성능에 대한 검증이 가능함을 나타내었다. 시간-도메인 영역에서 시뮬레이션 소요시간 비교를 위해 TSMC 0.18-㎛ 공정을 사용한 아날로그 위상고정루프의 설계 결과와 비교하였으며, 6 us의 과도 응답 해석을 진행했을 때 1.43초로 트랜지스터 레벨의 아날로그 설계 방식(692초) 대비 484배 빠른 시뮬레이션 시간을 나타내었다.

• 한국ITS학회 논문지
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• 제4권2호
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• pp.73-79
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• 2005

본 논문에서는 3가지 형태의 CMOS 직교 신호 발생 전압 제어 발진기를 설계 및 제작하여 위상 잡음 특성을 비교하였다. 첫 번째 구조는 PMOS를 이용하여 두개의 Colpitts 발진기를 구성한 후 이를 상호 결합시킨 구조이다. 두 번째와 세번째 구조는 각각 일반적인 LC VCO와 펼형 콜피츠 구조에 주파수 2분주기를 연결하여 직교신호를 얻는 구조이다. 모의실험 결과 콜피츠 구조를 사용한 구조가 LC 발진기를 사용하였을 때에 비해 위상 잡음 특성이 6 dB 이상 개선되었다.

• International Journal of Aeronautical and Space Sciences
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• 제9권2호
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• pp.48-57
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• 2008

The noise is one of the serious problems concerning helicopters operations. The issue of helicopter external noise generated mainly from a helicopter rotor has always affected the use of rotorcrafts, especially in the urban environment. The noise sources depend on the flight configurations. In particular, a noise generated by the interaction between blades and tip vortices mainly occurs during descent flight. This noise is called blade-vortex interaction (BVI) noise, and this BVI noise is particularly penalizing for helicopters. In this paper, a numerical study to capture the BVI noise is carried out. The numerical study is performed in two phases. In the first phase, a 2D simulation based on parallel BYI event of Kitapliglu et al experiment is performed. In the second phase, 3D simulation based on HART Ⅱ experiment is performed. Several experimental data such as thrust, torque, blade sectional load, its derivative and vortex location are compared with calculation results and the comparison showed reasonably good agreement.

• 한국소음진동공학회논문집
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• 제19권12호
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• pp.1260-1268
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• 2009

Three methods(the stepped sine method, the statistical method(random excitation method) and the maximum-length sequence(MLS) method) for head-related transfer functions(HRTFs) are experimentally compared in view point of accuracy and efficiency. First, the stepped sine method has high signal-to-noise ratio, but low efficiency. Second, the statistical method is fast measurement speed, but weak to noise than the other methods. Finally, the MLS method shows both good efficiency and high signal-to-noise ratio, but it needs additional software or equipment such as MLS signal generator. For comparison of measurement accuracy, HRTFs of KEMAR dummy are measured for various azimuths and elevations. Error norms for magnitude and phase of HRTFs are defined and calculated for the measured HRTFs. The calculated error norms show that the methods give similar results in magnitude and phase except a little phase difference in the MLS method.

• ETRI Journal
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• 제33권1호
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• pp.125-127
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• 2011

This letter presents a new type of resonator, namely, the split quarterwave microstrip resonator (SQMR), to improve the poor harmonic suppression and low Q-factors in conventional quarterwave microstrip resonators. An oscillator incorporating the proposed SQMR is designed, fabricated, and tested to demonstrate that, not only the second harmonic suppression, but also the phase noise of the oscillator can be improved. The oscillator with the SQMR shows improved second harmonic suppression of -74.59 dBc and phase noise figure of merit of -169.77 dBc/Hz at 1 MHz offset.

• 전기학회논문지
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• 제62권12호
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• pp.1700-1705
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• 2013

A second harmonic millimeter wave oscillator utilizing sub-harmonic injection-synchronization is presented. A 8.7GHz oscillator with MES-FET is designed, and is driven as a harmonic output oscillator at 17.4GHz by means of sub-harmonic injection-synchronization. The oscillator operates as a multiplier as well as a oscillator in this scheme. Adopting this method, a high sable, high frequency millimeter wave source is obtainable even though self-oscillating frequency of an oscillator is relatively low. The range of injection-synchronization is about 26MHz, and is proportional to the input sub-harmonic power. The spectrum analysis of the 2nd harmonic output frequency shows remarkably decreased the phase noise level.

• Journal of electromagnetic engineering and science
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• 제8권3호
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• pp.134-137
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• 2008

This paper proposes a novel quadrature VCO(QVCO) based on direct back-gate second harmonic coupling. The QVCO directly couples the current sources of the conventional LC VCOs through the back-gate instead of front-gate to generate quadrature signals. By the second harmonic injection locking, the two LC VCOs can generate quadrature signals without using on-chip transformer, or stability problem that is inherent in the direct front-gate second harmonic coupling. The proposed QVCO is implemented in $0.18{\mu}m$ CMOS technology operating at 2 GHz with 5.0 mA core current consumption from 1.8 V power supply. The measured phase noise of the proposed QVCO is - 63 dBc/Hz at 10 kHz offset, -95 dBc/Hz at 100 kHz offset, and -116 dBc/Hz at 1 MHz offset from the 2 GHz output frequency, respectively. The calculated figure of merit(FOM) is about -174 dBc/Hz at 1 MHz offset. The measured image band rejection is 46 dB which corresponds to the phase error of $0.6^{\circ}$.