• Architectural research
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• 제14권3호
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• pp.99-108
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• 2012

An innovative multi-story Semi-Active Tuned Mass Damper (SATMD) building system is proposed to control seismic response of existing structures. The application of adding new stories as large tuned mass and semi-active (SA) resettable actuators as central features of the control scheme is derived. For the effective control of the structures, the optimal tuning parameters are considered for the large mass ratio, for which a previously proposed equation is used and the practical optimal stiffness is allocated to the actuator stiffness and rubber bearing stiffness. A two-degree-of freedom (2-DOF) model is adopted to verify the principal efficiency of the suggested structural control concept. The simulations for this study utilizes the three ground motions, from SAC project, having probability of exceedance of 50% in 50 years, 10% in 50 years, and 2% in 50 years for the Los Angeles region. 12-story moment resisting frames, which are modified as '12+2' and '12+4' story structures, are investigated to assess the viability and effectiveness of the system that aims to reduce the response of the buildings to earthquakes. The control ability of the SATMD scheme is compared to that of an uncontrolled and an ideal Passive Tuned Mass Damper (PTMD) building system. From the performance results of suggested '12+2' and '12+4' story retrofitting case studies, SATMD systems shows significant promise for application of structural control where extra stories might be added.

• 전기학회논문지
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• 제60권9호
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• pp.1733-1740
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• 2011

In this research, a MEMS vibratory gyroscope with dual-mass system in the sensing mode has been proposed to increase the stability of the device using wide bandwidth. A wide flat region between the two resonance peaks of the dual-mass system removes the need for a frequency matching typically required for single mass vibratory gyroscopes. Bandwidth, mass ratio, spring constant, and frequency response of the dual-mass system have been analyzed with MATLAB and ANSYS simulation. Designed first and second peaks of sensing mode are 5,917 and 8,210Hz, respectively. Driving mode resonance frequency of 7,180Hz was located in the flat region between the two resonance peaks of the sensing mode. The device is fabricated with anodically bonded silicon-on-glass substrate. The chip size is 6mm x 6mm and the thickness of the silicon device layer is $50{\mu}m$. Despite the driving mode resonance frequency decrease of 2.8kHz and frequency shift of 176Hz from the sensing mode due to fabrication imperfections, measured driving frequency was located within the bandwidth of sensing part, which validates the utilized dual-mass concept. Measured bandwidth was 768Hz. Sensitivity calculated with measured displacement of driving and sensing parts was 22.4aF/deg/sec. Measured slope of the sensing point was 0.008dB/Hz.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.42-47
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• 2001

The heat (mass) transfer characteristics on the blade surface of a first-stage turbine rotor cascade for power generation has been investigated by employing the naphthalene sublimation technique. A four-axis profile measurement system is successfully developed for the measurements of the local heat (mass) transfer coefficient on the curved blade surface. The experiment is carried out at the free-stream Reynolds number and turbulence intensity of $2.09\times10^5$ and 1.2%. The results on the blade surfaces show that the local heat (mass) transfer on the suction surface is strongly influenced by the endwall vortices, but that on the pressure surface shows a nearly two-dimensional nature. The pressure surface has a more uniform distribution of heat load than the suction one.

• 천문학논총
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• 제30권2호
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• pp.401-403
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• 2015

We present the results of the analysis of FLS 1718+59, a galaxy-galaxy gravitational lens system in the Spitzer First Look Survey (FLS) field. A background galaxy ($z_s=0.245$) is severely distorted by a nearby elliptical galaxy ($z_l=0.08$), via gravitational lensing. The system is analysed by several methods, including surface brightness fitting, gravitational lens modeling, and spectral energy distribution fitting. From Galfit and Ellipse we measure basic parameters of the galaxy, such as the effective radius and the average surface brightness within it. gravlens yields the total mass inside the Einstein radius ($R_{Ein}$), and MAGPHYS gives us an estimate of the stellar mass inside $R_{Ein}$. By comparing these parameters, we confirm that the lens galaxy is an elliptical galaxy on the Fundamental Plane and calculate the stellar mass fraction inside $R_{Ein}$, and discuss the results with regards to the initial mass function.

• 대한원격탐사학회지
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• 제36권6_3호
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• pp.1681-1690
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• 2020

532와 1064 nm 두 파장 관측 채널을 구비하고 수평으로 360° 스캐닝 관측이 가능한 스캐닝 라이다 시스템을 개발하였다. 또한, 두 파장에서의 후방산란계수를 이용하여 미세먼지를 PM2.5-10(조대)와 PM2.5(미세)입자로 구분하는 분석도 개발하여 스캐닝 라이다 시스템의 데이터 분석에 적용하였다. 개발된 스캐닝 라이다를 이용한 울산 온산공단에서 관측에서 각각 22 - 110 ㎍/㎥과 7 - 78 ㎍/㎥의 분포를 보이는 PM10과 PM2.5의 질량 농도를 성공적으로 산출하였다. 분석된 결과는 라이다 관측 영역 주변에서 지상에서 측정된 질량농도와 유사한 값을 보였으며, 공장 등에서 배출되는 지점에서는 이 각각 80-110 ㎍/㎥과 60-78 ㎍/㎥의 고농도가 측정되는 사례를 확인하였다.

• 한국추진공학회지
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• 제5권3호
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• pp.33-40
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• 2001

본 연구에서는 초음속 증기 이젝터의 작동특성을 조사하기 위하여 압축성 축대칭 Navier-Stokes 방정식의 수치계산을 행하였다. 2차 유동측의 압력 및 배압을 변화시켜 이들 압력이 혼입유량에 미치는 영향을 조사하였다. 연구의 결과로부터 초음속 증기 이젝터에서 2차 유동측 압력 및 배압은 임계 혼입유량에 상당한 영향을 미치며, 1차구동노즐의 형상과 2차유동의 압력이 주어지는 경우 임계혼입 유량비를 예측할 수 있음을 알았다. 수치계산 결과는 실험에서 얻은 임계혼입유량비를 잘 예측하였다.

• Smart Structures and Systems
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• 제13권2호
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• pp.235-255
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• 2014

This paper mainly introduces recently developed technologies pertaining to the design and implementation of Active Mass Damper (AMD) control system on a high-rise building subjected to wind load. Discussions include introduction of real structure and the control system, the establishment of analytical model, the design and optimization of a variety of controllers, the design of time-varying variable gain feedback control strategy for limiting auxiliary mass stroke, and the design and optimization of AMD control devices. The results presented in this paper demonstrate that the proposed AMD control systems can resolve the issues pertaining to insufficient floor stiffness of the building. The control system operates well and has a good sensitivity.

• 전자공학회논문지SC
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• 제43권5호
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• pp.80-88
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• 2006

본 논문에서는 치밀 유방영상에서 mass형 암 검출을 목적으로 하는 시스템을 개발한다. 본 논문에서 제시하는 방법과 기존의 방법과의 차이점은 1) mass 영역의 중심의 위치와 반경을 영상신호의 불규칙성에 영향을 받지 않고 안정적으로 결정하는 방법을 제시하고, 2) mass형 유방암 영상에 적용하기 적합한 방사형 필터를 개발하며, 3) mass형 유방암 검출을 위해 mass 경계선의 불규칙성, mass 영역 중심부의 homogeneity, mass 영역의 이심율에 근거하여 다중 특징 함수 개발에 있다. 본 논문에서 제안한 시스템은 기존의 시스템보다 치밀 유방에 적용하였을 때 false alarm은 영상 당 1개 정도 높으나 true alarm 비율은 10%이상 향상 되었다.

• Journal of Astronomy and Space Sciences
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• 제12권2호
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• pp.179-195
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• 1995

RT Per has been known as a close binary of which the orbital period has unpredictably varied so far. Although there are no agreements with the working mechanism for the changes of the period, two interpretations have been suggested and waiting for to be tested: 1) light-time effects due to the unseen 3rd and 4rd bodies (Panchatsaram 1981), 2) Abrupt period-changes, due to internal variations of the system (e.g. mass transfer or mass loss) superimposing to the light-time effect by a 3rd body (Frieboes-Conde & Herczeg 1973). In the point of view that the former interprepation models could predict the behavior of the changes of the orbital period theoretically, we checked whether the recent observed times of minimum lights follow the perdictions by the first model or not. We confirmed that the observed times of minimum lights have followed the variations calculated by the light-times effects due to the 3rd and 4rd bodies suggested by Panchatsatam. In this paper a total of 626 times of minimum lights were reanalyzed in terms of the light-time effects by the 3rd and 4rd bodies. We concluded that the eclipsing pair in SVCam system moves in an elliptic orbit about center of mass of the triple system with a period of about $42.^y2$, while the mass center of the triplet is in light-time orbit about the center of mass of the quadruple system with a period of $120^y$. The mean masses deduced for the 3rd and 4rd bodies were $0.89m_\odot$ and $0.82m_\odot$, respectively.

• Journal of Astronomy and Space Sciences
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• 제20권4호
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• pp.375-382
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• 2003

위성을 설계함에 있어 질량제어 계획을 작성하고 질량자료를 유지하며 시스템의 질량특성을 계산하고 제어하는 것은 기계 시스템 담당자가 수행하는 임무 중에 하나이다. 위성의 질량특성은 자료수집, 특성예측 그리고 실제 측정의 순서로 설계 및 제작이 진행됨에 따라 수행된다. 질량특성 데이터베이스는 설계과정을 통하여 작성하게 되며 질량특성 측정 시험을 수행하여 데이터베이스의 신뢰성을 확인할 수 있어야 한다. 본 논문에서는 위성에서의 질량 제어계획의 일반적인 내용과 시스템 수준의 질량중심 및 관성 모멘트 계산과 관련된 여러 가지 구체적인 사항을 고려한 이론적 질량 특성 데이터베이스를 개발하고, 다목적실용위성 2호 개발을 수행하면서 얻게 된 실제적인 자료와 경험을 토대로 본 연구에서 개발된 데이터베이스의 신뢰성을 확인하였다.