• 제어로봇시스템학회논문지
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• 제22권7호
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• pp.562-569
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• 2016

This paper proposes a navigation system with a robust localization method for an underwater unmanned vehicle. For robust localization with IMU (Inertial Measurement Unit), a DVL (Doppler Velocity Log), and depth sensors, the EKF (Extended Kalman Filter) has been utilized to fuse multiple nonlinear data. Note that the GPS (Global Positioning System), which can obtain the absolute coordinates of the vehicle, cannot be used in the water. Additionally, the DVL has been used for measuring the relative velocity of the underwater vehicle. The DVL sensor measures the velocity of an object by using Doppler effects, which cause sound frequency changes from the relative velocity between a sound source and an observer. When the vehicle is moving, the motion trajectory to a target position can be recorded by the sensors attached to the vehicle. The performance of the proposed navigation system has been verified through real experiments in which an underwater unmanned vehicle reached a target position by using an IMU as a primary sensor and a DVL as the secondary sensor.

• 한국생산제조학회지
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• 제20권6호
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• pp.773-777
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• 2011

Conventional ultrasonic thickness measurement is to be considered as the assumption that the ultrasonic velocity is known. In actual applications the velocity is often not well known and access is often limited to one side. This paper aims at determining the ultrasonic velocity and thickness of plates with parallel or wedged surfaces using contact measurements made on one surface only. For wedged plates the thickness at one point and the wedge angle are determined. Equations are used for determining the ultrasonic velocity, thickness and wedge angle of the plate based on the times-of-flight measured by two contact transducers coupled to one surface. The time-of-flight of the obliquely reflected longitudinal wave echo was measured as a function of the separation between the two transducers. In addition, a simulation was made for comparing the experimental data and a FEM image. Experiments and simulations were performed on flat and wedged plates of aluminium materials; the calculated results for the unknown quantities are generally agreed with them to some degree.

• Journal of Chest Surgery
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• 제22권4호
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• pp.589-593
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• 1989

The frequency spectrum of the metallic closing sound and its loudness were measured by non invasive techniques in 66 patients. They had examined a total of 7 Carbomedics valve, 10 Duromedics valve, 11 St. Jude heart valve in mitral position and 8 Carbomedics, 10 Duromedics, 20 St. Jude heart valve prostheses functioning normally in aortic position. Statistical comparison of the loudness from sound produced by the three valves in each position, the following; The Carbomedics valve has the lowest average loudness, followed by the St. Jude medical valve, and finally the Edward Duromedics valve. And we analysis the changing factor of the loudness of valve sound, only the velocity of the flow through the valve influenced to the valve sound.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.779-782
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• 2002

We examine the problem in which porous/viscoelastic compliant thin plates are subject to pressure fluctuations under transitional or turbulent boundary layer. Measurements are presented of the frequency spectra of the near-field pressure and radiated sound by compliant surface. A porous plate consisting of 5mm thick, open-cell foam with fabric covering and a viscoelastic painted plate of 1mm thick over an acoustic board of 4m thick were placed over a rigid surface in an anechoic wind tunnel. Streamwise velocity and wall pressure measurements were shown to highly attenuate the convective wall pressure energy when the convective wavenumber ($k_{ch}$) was 3.0 or more. The sound source localization on the compliant walls is applied to the measurement of radiated sound by using an acoustic mirror system.

• 대한기계학회논문집B
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• 제27권3호
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• pp.294-301
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• 2003

We examine a problem in which porous/viscoelastic compliant thin plates are subject to pressure fluctuations under transitional or turbulent boundary layer. Measurements are presented of the frequency spectra of the near-field pressure and radiated sound by compliant surface. A porous plate consisting of 5mm thick. open-cell foam with fabric covering and a viscoelastic-painted plate of 1mm thick over an acoustic board of 4mm thick were placed over a rigid surface in an anechoic wind tunnel. Streamwise velocity and wall pressure measurements were shown to highly attenuate the convective wall pressure energy when the convective wavenumber (k$_{c}$h) was 3.0 or more. The sound source localization on the compliant walls is applied to the measurement of radiated sound by using an acoustic mirror system.

• 한국음향학회지
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• 제28권5호
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• pp.424-431
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• 2009

본 연구는 지구물리검층을 통해서 동해 울릉분지의 가스하이드레이트 함유지층과 비함유지층에서의 음파전달속도 (종파)의 특성차이를 규명하였다. 지구물리 검층 자료는 울릉분지의 중앙지역에서 취득하였다. 음파전달속도는 가스하이드레이트 함유지층의 경우 최대 속도값이 약 2200 m/s의 높은 값에서 1600 m/s의 낮은 값을 갖는다. 반면에 비함유지층에서는 약 1500 m/s 내외에서 1400 m/s보다 더 낮은 값을 갖기도 한다. 일반 해양퇴적물에서의 값 (약 $1500{\sim}1600$ m/s)보다 높은 값을 보이는 것은 가스하이드레이트가 퇴적물내에 함유되어 있기 때문이다. 가스하이드레이트 비함유구간중 해수의 속도보다 낮은 값을 보이는 구간은 해저면에서 약 140 m 이하의 해저모방반사면 (Bottom Simulating Reflector)의 하부층에 존재하는 자유가스 때문이다. 전기비저항값도 가스하이드레이트 함유구간에서 최대 150 Ohm-m까지 높게 나타나 비함유구 간에서의 값과 차이가 크다. 각 물성간의 상관관계를 보면 가스하이드레이트 함유지층과 비함유지층의 구분이 명확하게 나타나고 있으며 그 상관관계도 일반적인 해양 미고결퇴적물에서 보이는 값과는 상이한 양상을 보여주고 있다. 따라서 가스하이드레이트가 존재하는 지층의 물성과 음향특성을 해석할 때에는 가스하이드레이트의 존재 형태나 함량 등에 대한 연구가 병행되어야 할 것으로 생각된다.

• 한국콘텐츠학회논문지
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• 제16권8호
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• pp.427-434
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• 2016

본 논문은 인간이 인지할 수 있는 감각들 중 인체의 회전, 방향 변화 및 움직임의 정도를 알 수 있는 근감각에서 시각 및 청각 요소로의 변환 알고리즘을 이용하여 ARM Cortex-M4에 기반한 실시간 임베디드시스템으로 구현한 방법에 초점을 맞추었다. 근감각의 입력 방식으로는 자세측정장치(AHRS : Attitude Heading Reference System)를 이용해 롤(Roll), 피치(Pitch) 및 요(Yaw) 값을 실시간 획득하고, 이들 각각의 색을 표현하는 HSI 컬러 모델의 명도(Intensity), 색상(Hue) 및 채도(Saturation)에 대응하여 변환하였다. 최종 컬러신호는 HSI 에서 RGB 컬러모델로 변환하여 획득하였다. 또한, 근감각의 세 가지 입력 값들을 음을 표현하는 요소인 옥타브(Octave), 음계(Scale) 및 음의 세기(Velocity)에 대응하여 변환한 값을 MIDI(Musical Instrument Digital Interface)를 이용해 사운드를 합성하여 출력하였다. 출력 컬러신호 및 사운드를 분석한 결과, 근감각 입력 신호가 제안한 변환 방식에 따라 실시간으로 정확하게 색과 음으로 변환, 출력됨을 확인하였다.

• 한국도로학회논문집
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• 제15권6호
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• pp.79-91
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• 2013

PURPOSES : The methods of measuring the sound from the noise source are Pass-by method and NCPX (Noble Close Proximity) method. These measuring methods were used to determine the linkage of TAPL (Total Acoustic Pressure Level) and SPL (Sound Pressure Level) in terms of frequencies. METHODS : The frequency analysis methods are DFT (Discrete Fourier Transform) and FFT (Fast Fourier Transform), CPB (Constant Percentage Bandwidth). The CPB analysis was used in this study, based on the 1/3 octave band option configured for the frequency analysis. Furthermore, the regression analysis was used at the condition related to the sound attenuation effect. The MPE (Mean Percentage Error) and RMSE (Root Mean Squared Error) were utilized for calculating the error. RESULTS : From the results of the CPB frequency analysis, the predicted SPL along the frequency has 99.1% maximum precision with the measured SPL, resulting in roughly 1 dB(A) error. The TAPL results have precision by 99.37% with the measured TAPL. The predicted TAPL results at this study by using the SPL prediction model along the frequency have the maximum precision of 98.37% with the vehicle velocity. CONCLUSIONS : The Predicted SPL model along the frequency and the TAPL result by using the predicted SPL model have a high level of accuracy through this study. But the vehicle velocity-TAPL prediction model from the previous study by using the log regression analysis cannot be consistent with the TAPL result by using the predicted SPL model.

• 한국소음진동공학회논문집
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• 제14권3호
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• pp.253-263
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• 2004

The problem considered in this paper is about the collocation of sensor and actuator for the active control of sound and vibration. It is well-known that a point collocated sensor-actuator pair offers an unconditional stability with very high performance when it is used with a direct velocity feedback (DVFB) control, because the pair has strictly positive real (SPR) property. In order to utilize this SPR characteristics, a matched piezoelectric sensor and actuator pair is considered. but this pair suffers from the in-plane motion coupling problem with the out-of-plane motion due to the piezo sensor and actuator interaction. This coupling phnomenon limits the stability and performance of the matched pair with DVFBcontrol. As a new alternative, a point sensor and distributed piezoelectric actuator pair is also considered, which provides SPR property in all frequency range when the pair is implemented on a clamped-clapmed beam. The use of this sensor-actuator pair is highly expected for the applications to more practical active control of sound and vibration systems with the DVFB control strategy.

• 한국소음진동공학회논문집
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• 제22권2호
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• pp.179-186
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• 2012

The potential hazards resulting from a low-velocity impact(bird-strike, tool drop, runway debris, etc.) on aircraft structures, such as engine nacelle or leading edges has been a long-term concern to the aircraft industry. Certification authorities require that exposed aircraft components must be tested to prove their capability to withstand low-velocity impact without suffering critical damage. In most of the past research studies unloaded specimens have been used for impact tests, however, in reality it is much more likely that a composite structure is exposed to a certain stress state when it is being impacted, which can have a significant effect on the impact performance. And the radiated impact sound induced by impact is analyzed for the damage detection evaluation. In this study, an investigation was undertaken to evaluate the effect in-plane loading on the impact force and sound of composite laminates numerically.