• 한국군사과학기술학회지
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• 제17권1호
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• pp.108-114
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• 2014

This paper describes a method to set an intensity-based initial validation gate for tracking filter while preserves the ability of tracking a target with maximum speed. First, we collected real data set of signal versus distance of an airplane target. And at each data point, we computed maximum distance the target can move. And a function is modeled to expect the maximum moving pixels on the lateral direction based on the intensity of the detected target in IR image sequence. The initial prediction error covariance can be computed using this function to decide the size of the initial validation gate. The simulation results show the proposed method can set the appropriate initial validation gates to track the targets with the maximum speed.

• 한국안전학회지
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• 제9권1호
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• pp.89-94
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• 1994

Two methods, the numerical method of CPQRA and the manual method of IAEA, were used to estimate the effect distance from release and dispersion of toxic materials. The Gaussian plume model which has a weather stability class D with wind velocity of 5m/s was applied to calculate dispersion of toxic materials. Also, probit function were employed to evaluate the human fatality as a result of exposure to toxic gases. Furthermore, concentration of toxic materials corresponding to LC$_{50}$ for 30 min could be determined by setting Pr as 5.0 and solving the probit function. Calculations were conducted by employing chlorine and ammonia as toxic materials because they are not only most commonly used In chemical plants but also very harmful to humans. Calculated results by employing toxic materials indicated that the effect distance from the CPQRA method was between the minimum and maximum distance from the method proposed by IAEA.A.

• 전기전자학회논문지
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• 제25권4호
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• pp.584-590
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• 2021

본 논문에서는 초음파 센서로 거리를 측정할 때 간섭에 의해 발생하는 유령 신호를 배제하고 올바른 신호를 인식하는 초음파 센서 간 신호 간섭 제거 방안을 제시한다. 제안하는 기법에서는 이전 거리 측정 값과 현재 거리 측정 값을 비교하여 거리의 변화가 한계값을 벗어나면 유령 신호로 인식하고 배제한다. 기존 기법에서는 한계값이 고정되어 있어서 초음파 센서나 대상 물체가 급격하게 움직일 경우 유령 신호를 제대로 배제하기 어렵지만, 제안하는 기법에서는 한계값을 고정하지 않고 초음파 센서나 대상 물체가 움직일 경우 상대 속도에 따라 한계값을 적응적으로 결정하는 알고리즘을 사용하여 정확도를 높인다. 초음파 센서로 물체까지의 거리를 측정할 때 간섭이 가장 잘 일어나는 동종의 초음파 센서를 다수 사용하여 간섭 신호를 발생시키는 실험을 진행하였고 제안하는 기법이 효과적으로 유령 신호를 배제하는 것을 확인하였다.

• 대한기계학회논문집B
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• 제30권12호
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• pp.1164-1172
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• 2006

Measurements of the local heat transfer coefficients on hemispherical convex and concave surfaces with a turbulent impinging jet were made. The Reynolds number used was 11000, 23000, 50000 and the nozzle- to- surface distance was L/d=2, 4, 6, 8, and 10 and the jet angle was a = $0^{\circ}$, $15^{\circ}$, $30^{\circ}$ and $40^{\circ}$. In case of concave surface, the Nusselt number at the stagnation point decreases as the jet angle increases and has the maximum value for L/d=6. The X-axis Nusselt number distributions exhibit secondary maxima at $0^{\circ}$ $\leq$ a $\leq$ $15^{\circ}$, L/d $\leq$ 4 for X/d<0(upstream) and at $0^{\circ}$ $\leq$ a $\leq$ $40^{\circ}$, L/d $\leq$ 4 and at $30^{\circ}$ $\leq$ a $\leq$ $40^{\circ}$, 4 < L/d $\leq$ 6 for X/d<0(downstream). The secondary maximum occurs at long distance from the stagnation point as the jet angle increases or the nozzle-to-surface distance decreases. In case of convex, correlations of the stagnation point Nusselt number according to Reynolds number, jet-to-surface distance ratio and dimensionless surface angle are presented. In the stagnation point, in term of Ren, n ranges from 0.43 in case of 2 $\leq$ L/d $\leq$ 6 to 0.45 in case of 6 < L/d $\leq$ 10, there agrees roughly appears to be laminar boundary layer result. The maximum Nusselt number, in this experiment, occurred in the direction of upstream. The displacement of the maximum Nusselt number from the stagnation point increases with increasing surface angle or decreasing nozzle-to-surface distance. On this condition about surface curvature D/d=10, the maximum displacement is about 0.7 times of the jet nozzle diameter. The ratio of the maximum Nusselt number to the stagnation Nusselt number increases as the jet angle increases.

• 비파괴검사학회지
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• 제10권1호
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• pp.10-17
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• 1990

Recently, object recognition ultrasonic sensor is being used with automatization of industrial machine. Points which characterize the object can be deleted by measuring the propagation time of ultrasonic impulse and azimuth which gives its maximum amplitude, and from these points shape, position and orientation of the object are deduced. A new measuring method is adopted, where the distance to the object is calculated by sound reflection time which is measured from O-cross point of sound wave, and azimuth is measured by angle indicating maximum amplitude. The measuring accuracy of 1.0mm for distance and $0.5-2^{\circ}$ for azimuth have been accomplished. By rotational scanning of sensor the characteristic point of an object can be known and it gives the information of its shape, position and orientation. Experimental results showed that the object of some complicated shape can be recognized, which suggest its applicability to robot.

• 한국인터넷방송통신학회논문지
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• 제9권5호
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• pp.85-91
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• 2009

IT기술의 발전과 함께 유비쿼터스 (Ubiquitous)환경이 도래하여, 무선 센서 네트워크(Wireless Sensor Networks)기반 연구가 다방면에서 활발히 진행 중에 있다. 본 논문에서는 무선 센서 네트워크에서 센서간 거리를 전방위로 측정할 수 있는 간단한 방안에 대해 제안한다. 그리고 이를 직접 설계하고 구현하여 실험을 통해 검증해 본다. 전방향성 장치를 이용하면 거리 측정 최대 거리는 줄어드는 단점이 있지만 $360^{\circ}$ 방향을 측정 할 수 있다는 장점이 있다. 본 논문에서는 실제 환경에서 실험을 통하여 전방향성 장치가 존재할 경우와 그렇지 않은 경우에 대하여 초음파를 통한 거리측정 방식의 누락율 및 정확도를 분석해 본다.

• 한국기계가공학회지
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• 제15권4호
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• pp.148-154
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• 2016

A study on the micro particle blasting was conducted to find the optimum conditions of the blasted surface of aluminum 6061. The particle type such as $Al_2O_3$ and SiC, nozzle diameter, pressure, standoff distance and injection time were used as blasting conditions. Statistical method of orthogonal arrays(ANOVA) was used to find optimum conditions of maximum depth and maximum diameter of blasted surface. Particle type, nozzle diameter, and pressure were found to be the main factors of maximum blasted depth and diameter. Maximum blasted diameter was affected by increasing pressure and nozzle diameter but saturated maximum diameter. Maximum blasted depth was affected by pressure and nozzle diameter when aluminum 6061 was blasted with $Al_2O_3$ particle. The value of surface roughness was increased as pressure and nozzle diameter increased when aluminum 6061 was blasted with SiC.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.1846-1851
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• 2003

Approximate optimization has become popular in engineering field such as MDO and Crash analysis which is time consuming. To accomplish efficient approximate optimization, accuracy of approximate model is very important. As surrogate model, Kriging have been widely used approximating highly nonlinear system . Because Kriging employs interpolation method, it is adequate for deterministic computer simulation. Because there are no random errors and measurement errors in deterministic computer simulation, instead of classical DOE ,space filling experiment design which fills uniformly design space should be applied. In this work, various space filling designs such as maximin distance design, maximum entropy design are reviewed. And new design improving maximum entropy design is suggested and compared.

• 예술인문사회 융합 멀티미디어 논문지
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• 제7권4호
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• pp.551-559
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• 2017

본 논문에서는 베어링 고장진단 성능을 개선하기 위해 실시간 학습 방법을 제안한다. 기존 베어링 고장진단의 문제점은 학습되지 않은 상태에 대해 올바른 분류를 할 수 없다는 점이다. 제안한 4단계 실시간 학습 방법은 새로운 상태를 실시간으로 인지 및 학습하여 새로운 상태의 데이터를 올바르게 분류할 수 있다. 1단계에서는 학습 정보에서 각 클래스의 무게중심과 그 클래스 내 각 특징벡터 사이의 유클리디안 거리를 계산하여 각 클래스별로 거리의 최대값을 계산한다. 2단계에서는 새로 취득된 데이터의 특징벡터와 각 클래스의 무게중심 사이의 유클리디안 거리를 계산하고 각 클래스별 최대 허용 거리와 비교한다. 3단계에서는 새로 취득된 데이터들과 각 클래스 내 무게중심 사이의 거리가 각 클래스의 최대 허용 거리보다 모두 클 경우 새로운 상태의 데이터로 인지하고 새로운 상태 인지 횟수를 증가시킨다. 마지막 4단계에서는 새로운 상태 인지 회수가 10보다 클 경우 새로운 상태의 클래스를 생성하기 위해 새로운 상태로 인지된 10개의 데이터를 새로운 상태의 클래스로 지정하고 분류기를 재학습시킨다. 제안한 방법의 성능을 검증하기 위해 실제 베어링 결함 데이터를 사용하여 제안한 실시간 학습 방법의 효율성을 검증하였다.

• 설비공학논문집
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• 제12권4호
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• pp.371-380
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• 2000

The turbulent heat transfer from a round oblique impinging jet on a concave surface were experimentally investigated. The transient measurement method using liquid crystal was used in this study. In this measurement, a preheated wall was suddenly exposed to an impinging jet while recording the response of liquid crystals to measure surface temperature. The Reynolds numbers were 11000, 23000 and 50000, nozzle-to-surface distance ratio was from 2 to 10 and the surface angles were a =$0^{\circ}\;15^{\circ},\;30^{\circ}and\;40^{\circ}$. Correlations of the stagnation point Nusselt numbers with Reynolds number, jet-to-surface distance ratio and dimensionless surface angle, which account for the surface inclined angle, are presented. The maximum Nusselt numbers, in this experiment, occurred in the direction of upstream. The displacement of the maximum Nusselt number from the stagnation point increases with increasing surface angle or decreasing nozzle-to-surface distance. In this experiment, the maximum displacement is about 0.7 times of the jet nozzle diameter when surface curvature, D/d is 10.