• 한국정보통신학회논문지
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• 제5권2호
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• pp.385-391
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• 2001

본 연구는 해저면의 뻘, 모래, 자갈, 패류 등을 초음파를 이용하여 형태별로 신호패턴을 데이터베이스로 구축한 후, 바다 현장에서 어군탐지기에 수신된 아날로그 신호를 A/D변환기를 사용하여 디지털 신호로 변환하고, 이 신호를 컴퓨터에서 가공, 분석한 후 DB에 있는 신호패턴과 실시간으로 비교하여 해저면 목표물을 인식할 수 있는 판독시스템을 개발하는 것이다. 지금까지 연구한 결과를 바탕으로 많은 실험을 거친 후(수조 및 현장 실험 등) 침전물의 데이터를 세밀히 샘플링하여 분석하면 해저면의 저질 상태 및 침전물들의 정확한 정보를 알아낼 수 있다. 또한, 수중에서 어종별로 어체에서 반사되는 초음파 특성과, 해저면에서 뻘과 딱딱한 패류 껍질, 모래, 자갈 등에서 반사되는 초음파 특성 등을 1차 신호와 2차, 3차 신호들에 대한 성분을 분석하여, 해저 목표물을 나타내는 1차 신호의 필요한 값은 추출하고, 그 외의 2차, 3차 신호는 필터링 시키는 해저면 판독시스템을 개발하는 것이다.

• 대한전기학회논문지:전기물성ㆍ응용부문C
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• 제52권4호
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• pp.153-158
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• 2003

This thesis deal with ferroelectric and ferromagnetic materials. PZT/Ferrite ceramics were made by the making process using PZT powder and garnet ferrite powder. PZT and ferrite are mixed as much 90%-10%, 50%-50%, and so on. After making samples, we are polishing samples until thickness is 0.1~0.2mm. We measured all kinds of samples in room temperature and applied magnetic field from -4500 to 4500 Oersted and conducted test of magnetical and electrical measurement using VSM and lpC resolution electrometer calibrated with RT66A pulsed tester. From this measurement, we can calculate tunability of these samples using C value obtained from P-E loop. As a result, it was able to measure magnetic characteristic when two matter had each other component ratio, and it was compound. However, it confirmed the possibility that was able to have ferroelectric characteristic with you in PZT 90% and ferrite 10%. Therefore, If this thing comes for PZT 50% and ferrite 50% have ferroelectric characteristic as him in a compound sample ore, can use this in an oscillator, supersonic waves detector in addition to a piezoelectric element. It may contribute to multipurpose of an element and demands such as a miniaturization of equipment, efficiency, reduce of a price which can use a characteristic of two components.

• 한국철도학회논문집
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• 제8권2호
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• pp.145-154
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• 2005

Traffic accidents at highway-rail crossing result in larger social and economic damages than the accidents at the typical highway intersections. The traditional control and warning systems of the highway-rail crossing have limitations in that 1) they do not recognize the differences of the trains' arrival times because they rely on the distance-based control system, rather than the time-based one, and 2) thereby they usually cause longer delays of vehicles and pedestrians at the highway-rail crossings. The objective of this study is to develop a time-based railroad crossing control system which takes into account the speed and expected arrival time of trains. using the spot speeds and acceleration rates of trains measured at three points, the developed system was found to be able to accurately estimate the arrival time of train. VISSIM simulation package was utilized to compare system effect of the developed time-based railroad crossing control system with that of the conventional distance-based one. It was found that the developed time-based railroad crossing control system reduced the average travel time, maximum delay length, average delay time, and average number of stop-experienced vehicles as much as 7.0$\%$, 75.6$\%$, 12.7$\%$, and 60.0$\%$, respectively, compared with those from the conventional distance-based one.

• 한국군사과학기술학회지
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• 제17권4호
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• pp.463-470
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• 2014

Stealth technology of combat aircraft is most significant capability in recent air battlefield. As the detector of IR missiles is being developed, IR stealth capability which is evaluated by IR signature level become more important than it was in previous generation. Among IR signature of aircraft from various sources, aerodynamic heating dominates in long-wavelength IR spectrum of $8{\sim}12{\mu}m$. Skin temperature change by aerodynamic heating which is derived by effects of Mach number and structure. The 4th and 5th generation aircraft are selected for calculation of the skin temperature, and its height and velocity in numerical conditions are 10,000 m and Ma 0.9~1.9 respectively. Aircraft skin temperature is calculated by computing convection of fluid and conduction, convection and radiation of surface. As the aircraft accelerates to higher Mach number, maximum skin temperature increases more rapidly than average temperature and temperature distribution changes in more sharp, interactive ways. The 4th generation aircraft whose shape is more complex than that of the 5th generation aircraft have complicated temperature distribution. On the other hand, the 5th generation aircraft whose shape is relatively simple shows plain temperature distribution and lower skin temperature in terms of both average and maximum value.