• 한국항공우주학회지
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• 제37권10호
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• pp.992-997
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• 2009

본 논문에서는 제한된 센서 조건에서 유도탄 동체의 각속도를 계산하는 법을 보이고 Flight Motion Simulator(FMS)를 이용한 각속도 계산식 검증을 다룬다. 일반적으로 유도탄 동체의 각속도는 동체에 탑재하는 각속도 자이로를 이용하여 측정하지만, 유도탄 동체에 탑재하는 관성 센서 중에 피치와 요 각속도 자이로가 없는 제한된 센서 조건을 가정한다. 이와 같은 제한된 센서 조건에서 김블 탐색기 자이로, 동체의 롤 각속도 자이로, 김블의 자세 측정값 및 자세 변화율을 이용하여 유도탄 동체의 각속도를 계산할 수 있음을 보인다. 제안한 각속도 계산식을 검증하기 위하여 FMS를 이용한 실험을 수행하였다.

• 한국항공우주학회지
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• 제40권6호
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• pp.492-498
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• 2012

DBD(Dielectric Barrier Discharge) 플라즈마 액츄에이터의 설계 파라미터에 따른 특성을 연구하였다. 방전전압, 주파수, 전극의 간격, 폭, 길이, 유전체 두께에 따른 DBD 플라즈마 액츄에이터의 유속 및 소모전력을 측정하였다. 방전전압과 주파수가 클수록 유속과 소모전력은 증가하였다. 전극간격은 클수록 소모전력은 감소하면서 유속은 증가하였으나, 플라즈마 방전을 위해 높은 전압이 요구되었다. 상부전극폭은 좁을수록, 하부전극폭은 넓을수록 일정한 소모전력으로 유속을 증가시킬 수 있었다. 주어진 방전조건과 전극형상에서 DBD 플라즈마 액츄에이터의 성능을 예측할 수 있을 것으로 기대된다.

• 천문학회보
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• 제46권2호
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• pp.71.1-71.1
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• 2021

We perform disk-halo decomposition of the Large Magellanic Cloud (LMC) using a novel HI velocity field extraction method, aimed at better deriving its HI kinematics and thus mass distribution in the galaxy including both baryons and dark matter. We decompose all the line-of-sight velocity profiles of the combined HI data cube of the LMC, taken from the Australia Telescope Compact Array (ATCA) and Parkes radio telescopes with an optimal number of Gaussian components. For this, we use a novel tool, the so-called BAYGAUD which performs profile decomposition based on Bayesian MCMC techniques. From this, we disentangle turbulent non-ordered HI gas motions from the decomposed gas components, and produce an HI bulk velocity field which better follows the global circular rotation of the galaxy. From a 2D tilted-ring analysis of the HI bulk velocity field, we derive the rotation curve of the LMC after correcting for its transverse, nutation and precession motions. The dynamical contributions of baryons like stars and gaseous components which are derived using the Spitzer 3.6 micron image and the HI data are then subtracted from the total kinematics of the LMC. Here, we present the bulk HI rotation curve, the mass models of stars and gaseous components, and the resulting dark matter density profile of the LMC.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2002년도 춘계학술대회 논문집
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• pp.719-722
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• 2002

Cylindrical cam mechanisms are used commonly in many automatic machinery. But the cylindrical cam is very difficult to design and manufacture the shape. The motion analysis of the cylindrical cam can check the accuracy between designed data and manufactured data of the cam shape and can reproduce without the cam design data. The motion analysis of the cylindrical cam consists of displacement analysis, velocity analysis and acceleration analysis. This paper performs the motion analysis of a cylindrical cam with translating follower by using a relative velocity method and a central difference method. The displacement is calculated by using the central difference method and the velocity is calculated by the relative velocity method. The relative velocity method is defined by the relative motion between follower and cam at a center of a follower roller. The central difference method is derived in the 3 dimensional space.

• 제어로봇시스템학회논문지
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• 제14권6호
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• pp.603-607
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• 2008

This paper proposes a fast acquisition method using INS velocity and multiple correlators for high speed vehicles. In order to reduce acquisition time in GPS receiver, the method utilizes inertial velocity information and multiple correlators. Search range of the Doppler frequency is reduced by using INS velocity and the number of cells at one search can be increased by using multiple correlators. By using both multiple correlators and the INS velocity in the acquisition, search space can be greatly reduced. Experimental results show that the method gives faster signal acquisition performance than the conventional method.

• Journal of Positioning, Navigation, and Timing
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• 제12권3호
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• pp.315-321
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• 2023

In this paper, we propose an algorithm that jointly estimates the location and velocity of a near-field moving target in a pulse radar system. The proposed algorithm estimates the location and velocity corresponding to the outcome of orthogonal matching pursuit (OMP) in a 4-dimensional (4D) location-velocity space. To address the high computational complexity of 4D parameter joint estimation, we propose an algorithm that iteratively estimates the target's 2D location and velocity sequentially. Through simulations, we analyze the estimation performance and verify the computational efficiency of the proposed algorithm.

• 한국산학기술학회논문지
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• 제17권7호
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• pp.713-719
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• 2016

암모니아를 환원제로 사용하는 선택적 촉매 환원법에서 Mn-Cu-$TiO_2$ 촉매와 $V_2O_5$/$TiO_2$ 촉매를 사용하여 반응 조건에 따른 질소 산화물 전환 특성을 연구하였다. 반응 온도와 공간 속도를 변경시키면서 촉매의 질소 산화물 전환 효율 변화를 측정하였다. Mn-Cu-$TiO_2$ 촉매의 질소 산화물 제거 활성은 반응 온도와 공간 속도가 증가할수록 감소하였으나, $V_2O_5$/$TiO_2$ 촉매의 경우 반응 온도 증가에 따라 촉매의 질소 산화물 제거 활성 또한 증가하였다. Mn-Cu-$TiO_2$ 촉매의 경우 $200^{\circ}C$ 이하의 온도에서 저온 활성이 우수하였으며, 이를 $H_2$-TPR 및 XPS 분석 실험을 통해 확인할 수 있었다. 초기 반응 온도의 변경 실험을 통해 Mn-Cu-$TiO_2$ 촉매의 경우 고온에서 열적 쇼크를 일부 받으나, $V_2O_5$/$TiO_2$ 촉매의 경우는 거의 영향을 받지 않음을 확인할 수 있었다. 공간 속도에 따른 질소 산화물 전환 효율 변화는 C 촉매의 경우 전 구간에 걸쳐 공간 속도가 증가할수록 질소 산화물 전환 효율도 감소하는 경향을 보였다. 그러나 D 촉매의 경우 공간 속도가 증가할수록 질소 산화물 전환 효율은 감소하였으나, 감소 정도가 C 촉매 보다는 훨씬 적었다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2012년도 제45회 KOSCO SYMPOSIUM 초록집
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• pp.159-162
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• 2012

Combustion in a narrow space has been interested as a model of meso-scale combustors (or micro-combustors). Premixed flames have been used to overcome flame quenching in a narrow space and non-premixed flames have been used to improve flame stabilization. In this study, overall characteristics of premixed flame and non-premixed flame in narrow combustion spaces were reviewed. Various effects such as the flow velocity distribution, thermal interaction, enhanced mass diffusion were discussed and an eventual structure of the flame at the extinction limit was introduced.

• 천문학회보
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• 제45권1호
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• pp.44.2-44.2
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• 2020

The Korea Astronomy and Space Science Institute (KASI) has been collaborating with the NASA Goddard Space Flight Center (GSFC), to install a diagnostic coronagraph on the International Space Station (ISS). The coronagraph is designed to obtain simultaneous measurements of electron density, temperature, and velocity using multiple filters in the 3-10 Rs range. In 2019, we developed a new coronagraph and launched it on a stratospheric balloon (BITSE) from Fort Sumner, New Mexico in USA. As the next step, the coronagraph will be further developed, installed and operated on the ISS (CODEX) in 2023 to understand the physical conditions in the solar wind acceleration region, and enable and validate the next generation space weather models. In this presentation, we will report recent progress and introduce future plan.