• Advances in aircraft and spacecraft science
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• 제5권2호
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• pp.225-237
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• 2018

The difficulties of satellite vibration testing are due to the commonly expressed qualification requirements being incompatible with the limited performance of the entire controlled system (satellite + interface + shaker + controller). Two features cause the problem: firstly, the main satellite modes (i.e., the first structural mode and the high and low tank modes) are very weakly damped; secondly, the controller is just too basic to achieve the expected performance in such cases. The combination of these two issues results in oscillations around the notching levels and high amplitude beating immediately after the mode. The beating overshoots are a major risk source because they can result in the test being aborted if the qualification upper limit is exceeded. Although the abort is, in itself, a safety measure protecting the tested satellite, it increases the risk of structural fatigue, firstly because the abort threshold has been already reached, and secondly, because the test must restart at the same close-resonance frequency and remain there until the qualification level is reached and the sweep frequency can continue. The beat minimum relates only to small successive frequency ranges in which the qualification level is not reached. Although they are less problematic because they do not cause an inadvertent test shutdown, such situations inevitably result in waiver requests from the client. A controlled-system analysis indicates an operating principle that cannot provide sufficient stability: the drive calculation (which controls the process) simply multiplies the frequency reference (usually called cola) and a function of the following setpoint, the ratio between the amplitude already reached and the previous setpoint, and the compression factor. This function value changes at each cola interval, but it never takes into account the sensor signal phase. Because of these limitations, we firstly examined whether it was possible to empirically determine, using a series of tests with a very simple dummy, a controller setting process that significantly improves the results. As the attempt failed, we have performed simulations seeking an optimum adjustment by finding the Least Mean Square of the difference between the reference and response signal. The simulations showed a significant improvement during the notch beat and a small reduction in the beat amplitude. However, the small improvement in this process was not useful because it highlighted the need to change the reference at each cola interval, sometimes with instructions almost twice the qualification level. Another uncertainty regarding the consequences of such an approach involves the impact of differences between the estimated model (used in the simulation) and the actual system. As limitations in the current controller were identified in different approaches, we considered the feasibility of a new controller that takes into account an estimated single-input multi-output (SIMO) model. Its parameters were estimated from a very low-level throughput. Against this backdrop, we analyzed the feasibility of an LQG control in cancelling beating, and this article highlights the relevance of such an approach.

• 한국전자파학회논문지
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• 제20권10호
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• pp.1031-1041
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• 2009

본 논문에서는 다중 대역에서 매크로-마이크로 주파수 튜닝이 가능한 소형의 패치 모노폴 안테나를 소개하였다. 제안된 재구성 안테나는 PCB 기판(FR-4: $\varepsilon_r=4.4$ and tan $\delta=0.02$) 위에 미앤더(meander) 형태의 안테나로 설계하였고, Wibro(2.3~2.4 GHz)와 WLAN a/b(2.4~2.5 GHz/5.15~5.35 GHz)대역에서 일정한 이득을 유지하면서 각각의 서비스 대역에서 동작한다. 두 개의 다이오드, 핀 다이오드와 버렉터 다이오드가 주파수 튜닝을 위해 안테나 상에 내장되었으며, 핀 다이오드는 2 GHz와 5 GHz의 대역을 스위칭(매크로 튜닝)하기 위해 사용되었으며, 버렉터 다이오드는 2.3~2.5 GHz와 5.15~5.35 GHz의 서비스 대역 내 미세 주파수 튜닝(마이크로 튜닝)을 위하여 사용되었다. 또한, 두 주파수 대역(2 GHz와 5 GHz) 사이에서의 불요 공진(spurious resonance)은 미앤더(meander) 사이의 갭을 조정하여 제거되었다. 안테나는 각각의 서비스 대역에서 2 dBi 이상의 일정한 이득을 보인다. 제안된 안테나의 측정 결과는 매크로-마이크로 주파수 튜닝 기술이 재구성 가능한 다중 대역 다중 모드(Multi-Mode Multi-Band: MMMB) 무선 통신 시스템에서 유용하게 사용될 수 있음을 보여준다.

• 한국광학회지
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• 제34권6호
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• pp.241-247
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• 2023

본 연구에서는 355 nm 파장의 나노초 레이저를 비정질 실리콘 박막에 조사하여 형성된 주기적 laser-induced periodic surface structure (LIPSS) 구조의 분광학적 특성을 연구하였다. 지름 196 ㎛의 가우시안 빔을 단위면적당 레이저 펄스 190-280회, 레이저 빔의 세기는 100-130 mJ/cm² 범위에서 'ㄹ' 자 형태로 2차원 스캔하였다. 그 결과 Si 박막 표면에 ~300 nm 주기의 LIPSS 구조가 레이저 편광에 수직 방향으로 정렬되었다. 시료의 투과율 스펙트럼을 측정하여 transverse-electric 편광과 transverse-magnetic 편광에 대해서 각각 700 nm, 500 nm 근방에서 dip이 관측되었다. 이 현상을 설명하기 위해 1차원 격자구조 모델을 이용하여 rigorous coupled-wave analysis를 이용한 시뮬레이션을 하여 편광에 따른 도파모드 공진에 의한 특성임을 규명하였다.

• 방송공학회논문지
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• 제19권5호
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• pp.726-735
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• 2014

최근 초고화질(UHD) 영상시스템의 출현으로 인해 고해상도, 대용량의 4K-UHD급 LCD TV 신호 전송은 높은 해상도와 데이터 확장에 따른 케이블 및 커넥터 수의 증가로 서로 다른 케이블 간의 EMI, 스큐(Skew) 문제로 시스템 구현에 한계가 있다. 차세대 V-by-One HS 인터페이스는 초고해상도 영상처리 IC 및 TCON 간의 새로운 인터페이스 기술로써 600Mbps에서 3.75Gbps의 다양한 데이터 속도로 효율적인 전송이 가능하여 한계를 극복할 수 있다. 본 논문에서는 V-by-One HS IBIS(Input/Output Buffer Information Specification) 모델 시뮬레이션을 통하여 주파수 공진모드의 전압 분포와 PCB 설계 방법을 제안하고 고속영상 신호에 대한 신호 무결성의 검증 방법을 제안하였다.

• 수산해양교육연구
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• 제21권1호
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• pp.68-77
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• 2009

In this study it will be discussed how to solve the problem of discomfort from rolling motion on the small fishing boats. Up to now, the equipments of reducing rolling system can be examined by various case, but difficult to apply small vessel by function, space and costly establishment. A way of improving the feeling of getting on a boat through the equipped sail at stern edge of bulwark top was researched and developed. The author has tested the sailing performance of the experimental skiff boat, from the signals obtained by the inclinometer in irregular waves and compared with the results got in sail on and off mode operation for 10 minutes duration at the conditions of stop and underway. These data has been analyzed in the application statistical methods. Eventually we summarize the analyzed results obtained from the vessel while stationary and underway for two cases, the vessel with a sail and the vessel without a sail. The field test was done in Jeju outer harbor. The ratio of the motion responses at resonance for the sail with and without cases indicate that under given conditions the motion was reduced by the efficiency of diminution is 4.726%, 2.792% in the stopping and 11.663%, 3.282% in the underway and mean rolling periods are 2.158, 2.142, 2.421, 2.412sec. and 1.968, 1.963, 2.089, 2.051sec. respectively. Consequently the efficiency of diminution was higher when the ship is underway and rolling periods got longer in the equipped sail.

• Journal of Microbiology and Biotechnology
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• 제18권10호
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• pp.1659-1662
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• 2008

Pseudomonas chlororaphis O6 exhibits induced systemic resistance (ISR) against P. syringae pv. tabaci in tobacco. To identify one of the ISR metabolites, O6 cultures were extracted with organic solvents, and the organic extracts were subjected to column chromatography followed by spectroscopy analyses. The ISR bioassay-guided fractionation was carried out for isolation of the metabolite. High-resolution mass spectrometric analysis of the metabolite found $C_{9}H_{9}O_{3}N$ with an exact mass of 179.0582. LC/MS analysis in positive mode showed an $(M+H)^{+}$ peak at m/z 180. Nuclear magnetic resonance ($^{1}H,\;^{13}C$) analyses identified all protons and carbons of the metabolite. Based on the spectroscopy data, the metabolite was identified as 4-(aminocarbonyl) phenylacetate (4-ACPA). 4-ACPA applied at 68.0 mM exhibited ISR activity at a level similar to 1.0 mM salicylic acid. This is the first report to identify an ISR metabolite produced by P. chlororaphis O6 against the wildfire pathogen P. syringae pv. tabaci in tobacco.

• 한국항공우주학회지
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• 제38권5호
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• pp.456-466
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• 2010

전형적인 하이브리드 모터의 연소 불안정 현상인 DC-Shift는 비선형적 특성을 갖는다. DC-Shift는 두 가지 형태로 나타나게 되는데, 압력이 급격하게 상승하는 양의 DC-shift와 연소 도중에 압력이 갑자기 감소하는 음의 DC-shift로 구분된다. 이 논문에서는 산화제 공급 유동 조건을 다양하게 변화시켜 음의 DC-shift 현상을 유도하고 산화제 공급 유동조건과 하이브리드 로켓이 갖고 있는 기본적인 주파수와 Helmholtz 주파수, 음향모드와의 공진을 유도하여 음의 DC-shift 현상의 발생 조건과 특징에 대하여 알아보았다. 실험 결과 연소 중 수백 Hz 대역의 압력 주파수 이동을 확인하였으며, 음의 DC-Shift가 연소로 발생하는 주파수와 유동의 흐름으로 인한 주파수간 위상이 상호 감쇠되어 발생한 것으로 나타났다. 향후 연소 중 나타나는 주파수의 변화에 따른 DC-Shift 현상에 대해서는 계속 연구되어야 한다.

• 한국전산유체공학회지
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• 제15권2호
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• pp.7-13
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• 2010

Flight vehicles such as wheel wells and bomb bays have many cavities. The flow around a cavity is characterized as an unsteady flow because of the formation and dissipation of vortices brought by the interaction between the free stream shear layer and the internal flow of the cavity. The resonance phenomena can damage the structures around the cavity and negatively affect the aerodynamic performance and stability of the vehicle. In this study, a numerical analysis was performed for the cavity flows using the unsteady compressible three-dimensional Reynolds-Averaged Navier-Stokes (RANS) equation with Wilcox's turbulence model. The Message Passing Interface (MPI) parallelized code was used for the calculations by PC-cluster. The cavity has aspect ratios (L/D) of 5.5 ~ 7.5 with width ratios (W/D) of 2 ~ 4. The Mach and Reynolds numbers are 0.4 ~ 0.6 and $1.6{\times}10^6$, respectively. The occurrence of oscillation is observed in the "shear layer and transient mode" with a feedback mechanism. Based on the Sound Pressure Level (SPL) analysis of the pressure variation at the cavity trailing edge, the dominant frequencies are analyzed and compared with the results of Rossiter's formula. The dominant frequencies are very similar to the result of Rossiter's formula and other experimental datum in the low aspect ratio cavity (L/D = ~4.5). In the high aspect ratio cavity, however, there are other low dominant frequencies of the leading edge shear layer with the dominant frequencies of the feedback mechanism.

• 한국구조물진단유지관리공학회 논문집
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• 제17권3호
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• pp.20-27
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• 2013

본 논문에서는 고유진동수를 구하기 Simple Iteration Method을 제시하였다. 이 방법은 임의의 단면과 지점을 갖고 임의의 하중을 받는 보나 탑의 진동모드와 관련된 고유진동수를 간편하면서도 정확하게 계산할 수 있는 획기적인 방법이다. 이 방법에는 공진상태에서 관성력에 기인한 부재의 처짐 모드를 구하게 된다. 진동해석을 위하여 처짐의 영향을 고려한 다양한 방법이 검토되었다. 이러한 목적으로 본 논문에서는 유한차분법을 사용하였다. 고유진동수에 대한 $D_{22}$ 휨강성의 영향을 철저하게 검토하였다. 본 논문에서는 구조 요소의 하중 분포 또는 상이한 단면에 따른 고유진동수에 대한 영향을 연구하였으며 그 결과를 제시하였다. 이 방법은 첨단복합재료를 포함한 2차원 문제에도 적용할 수 있다.

• 대기
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• 제23권2호
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• pp.205-220
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• 2013

Upper ocean response to typhoon Ewiniar (0603) and its impact on the following typhoon Bilis (0604) are investigated using observational data and numerical experiments. Data used in this study are obtained from the Ieodo Ocean Research Station (IORS), ARGO, and satellite. Numerical simulations are conducted using 3-dimensional Princeton Ocean Model. Results show that when Ewiniar passes over the western North Pacific, unique oceanic responses are found at two places, One is in East China Sea near Taiwan and another is in the vicinity of IORS. The latter are characterized by a strong sea surface cooling (SSC), $6^{\circ}C$ and $11^{\circ}C$ in simulation and observation, under the condition of typhoon with a fast translation speed (8m $s^{-1}$) and lowering intensity (970 hPa). The record-breaking strong SSC is caused by the Yellow Sea Bottom Cold Water, which produces a strong vertical temperature gradient within a shallow depth of Yellow Sea. The former are also characterized by a strong SSC, $7.5^{\circ}C$ in simulation, with a additional cooling of $4.5^{\circ}C$ after a storm's passage mainly due to enhanced and maintained upwelling process by the resonance coupling of storm translation speed and the gravest mode internal wave phase speed. The numerical simulation reveals that the Ewiniar produced a unfavorable upper-ocean thermal condition, which eventually inhibited the intensification of the following typhoon Bilis. Statistics show that 9% of the typhoons in western North Pacific are influenced by cold wakes produced by a proceeding typhoon. These overall results demonstrate that upper ocean response to a typhoon even after the passage is also important factor to be considered for an accurate intensity prediction of a following typhoon with similar track.