• 한국윤활학회:학술대회논문집
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• 한국윤활학회 1999년도 제29회 춘계학술대회
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• pp.73-79
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• 1999

Finite element equations by using fast Fourier transformation were formulated for studying temperatures resulting from frictional heating in sliding systems. The equations include the effect of velocity of moving components. The program developed by using FFT-FEM that combines Fourier transform techniques and the finite element method, was applied to the sliding bearing system. Numerical prediction obtained by FFT-FEM was in an excellent agreement of experimental temperature measurements.

• Tribology and Lubricants
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• 제16권3호
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• pp.218-222
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• 2000

Finite element equations by using fast Fourier transformation were formulated for studying temperatures resulting from frictional heating in sliding systems. The equations include the effect of velocity of moving components. The program developed by using FFT-FEM that combines Fourier transform techniques and the finite element method, was applied to the sliding bearing system. Numerical prediction obtained by FFT-FEM was in an excellent agreement of experimental temperature measurements.

• 한국음향학회지
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• 제41권2호
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• pp.159-165
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• 2022

본 논문에서는 수중 음향통신에서 Binary Phase Shift Keying(BPSK) 변조방식에 대한 프레임 동기 구조를 제안하였다. 제안된 프레임 동기 구조는 크게 두 가지로 나뉜다. 우선, 비동기 방식 상관과 Sliding 고속 푸리에 변환 방식으로 프레임의 대략적인 위치와 주파수 옵셋을 획득한다. 두번째는 주파수 오차를 신호에 보상한 후, 동기 방식 상관으로 정확한 프레임의 위치를 확인한다. 프레임 동기 구조의 성능 확인을 위해 해상실험을 수행하였다. 수신신호는 채널 특성으로 인해 전력이 크게 감소함을 확인하였으며, 이를 통해 비동기 방식 상관과 Sliding 고속 푸리에 변환 방식의 한계를 확인하였다. 결과적으로, 주파수 오차를 보상한 후 동기 방식 상관방식을 사용함으로써 안정적인 프레임 동기를 획득할 수 있었다.

• 대한전자공학회논문지SP
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• 제48권4호
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• pp.160-168
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• 2011

주파수 영역 빔형성기 (frequency domain beamformer)는 시간 영역 빔형성기에 비해 연산량 측면에서 효율성이 높아 다수의 빔과 센서가 요구되는 수동 소나 시스템에서 널리 사용되고 있다. 주파수 영역 빔형성기에서는 푸리에 변환을 통한 입력 신호의 스펙트럼 분석 과정이 필수적이며, 이 과정의 효율성에 따라 전체 시스템의 성능이 결정된다. 또한 기본적으로 실시간 신호처리가 요구되는 실제 전장 환경에서 이러한 스펙트럼 연산 과정 최적화의 중요성이 더욱 부각되고 있다. 따라서 본 논문에서는 실시간으로 수신되는 협대역 신호의 효율적인 국부 스펙트럼 분석 (partial spectrum analysis)을 위해, TD (transform decomposition) 기법과 GSFFT (generalized sliding fast Fourier transform) 기법의 장점을 모두 적용한 pruned-GSFFT 기법을 제안한다. 또한 제안된 기법의 구현상의 특성을 분석하고 요구되는 연산량을 기존 기법들과 비교한다.

• Journal of Power Electronics
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• 제10권4호
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• pp.412-418
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• 2010

This paper proposes a new algorithm to generate a reference signal for an active power filter using a sliding-window FFT operation to improve the steady-state performance of the active power filter. In the proposed algorithm the sliding-window FFT operation is applied to the load current to generate the reference value for the compensating current. The magnitude and phase-angle for each order of harmonics are respectively averaged for 14 periods. Furthermore, the phase-angle delay for each order of harmonics passing through the controller is corrected in advance to improve the compensation performance. The steady-state and transient performance of the proposed algorithm was verified through computer simulations and experimental work with a hardware prototype. A single-phase active power filter with the proposed algorithm can offer a reduction in THD from 75% to 4% when it is applied to a non-linear load composed of a diode bridge and a RC circuit. The active power filter with the proposed reference generation method shows accurate harmonic compensation performance compared with previously developed methods, in which the THD of source current is higher than 5%.

• 한국정보과학회:학술대회논문집
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• 한국정보과학회 2008년도 한국컴퓨터종합학술대회논문집 Vol.35 No.1 (A)
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• pp.92-97
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• 2008

적절한 촉각자극과 결합된 효과음은 실감성을 향상시킨다고 알려져 있다. 예를 들어, 영화나 게임의 총소리 효과음에 진동자극이 결합되면 훨씬 몰입감이 증진된다. 영화의 경우, 미디어 파일 내에 진동효과 관련한 정보를 부가하는 연구가 진행되기도 하였으나 대중화되지는 못했다. 게임의 경우, 진동을 유발시키도록 프로그래밍하는 방식을 사용하기도 한다. 하지만 진동을 고려하여 개발하는 게임은 전체 10% 미만일 정도로 일반화되어 있지 않다. 따라서 효과음향을 실시간으로 감지하여 진동을 발생시키는 시스템이 바람직하다. 본 논문에서는 이러한 시스템에서 특정 효과음을 실시간으로 감지하는 알고리즘을 제안한다. 이 알고리즘에서는 감지하고자 하는 효과음의 주파수 분포를 미리 분석해서 저장해 놓는다. 입력되는 효과음에 대해 실시간으로 주파수를 분석하여 저장된 값과의 차이를 비교하여 특정 효과음을 감지하게 된다. 실시간 주파수 분포에는 sliding fast Fourier transform (SFFT)를 사용한다. 이는 특정 효과음의 시작순간을 명확히 알 수 없기 때문이다. 제안 알고리즘을 First Person Shooting (FPS) 게임에 적용하여 성능분석을 하였다. 소음이 없을 경우, 감지율은 $80{\sim}90%$였으나, 소음 정도가 커질수록 감지율이 선형적으로 반비례하였다. 또한 감지에 걸리는 시간은 효과음 발생순간부터 0.45초 이내였다.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2002년도 제35회 춘계학술대회
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• pp.34-39
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• 2002

The surfaces of machine components in sliding contact such as bearing, gears and pistons etc. frequently operate under the condition of mixed lubrication due to high load, high speed and slip. These machine components often undergo the inception of scuffing in practical application. The scuffing failure is a critical problem in modern machine components, especially for the requirement of high efficiency and small size. However, it is difficult to find a universal mechanism to explain all scuffing phenomena because there are so many factors affecting the onset of scuffing. In this study, scuffing experiments are conducted using Acoustic Emission(AE) measurement by an indirect sensing approach to detect scuffing failure. Acoustic Emission(AE) signal has been widely utilized to monitor the interaction at the friction interface. Using AE signals we can get an indication about the state of the friction processes, about the quality of solid and liquid layers eon the contacting surfaces in real time. The FFT(Fast Fourier Transform)analyses of the AE signal are used to understand the interfacial interaction and the relationship between the AE signal and the state of contact is presented

• Tribology and Lubricants
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• 제18권5호
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• pp.351-356
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• 2002

The surfaces of machine components in sliding contact such as bearing, gears and pistons etc. frequently operate under the condition of mixed lubrication due to high load, high speed and slip. These machine components often undergo the inception of scuffing in practical application. The scuffing failure is a critical problem in modern machine components, especially for the requirement of high efficiency and small size. However, it is difficult to find a universal mechanism to explain all scuffing phenomena because there are so many factors affecting the onset of scuffing. In this study, scuffing experiments are conducted using Acoustic Emission(AE) measurement by an indirect sensing approach to detect scuffing failure. Acoustic Emission(AE) signal has been widely utilized to monitor the interaction at the friction interface. Using AE signals we can get an indication about the state of the friction processes, about the quality of solid and liquid layers on the contacting surfaces in real time. The FFT(Fast Fourier Transform) analyses of the AE signal are sued to understand the interfacial interaction and the relationship between the AE signal and the state of contact is presented.

• International Journal of Naval Architecture and Ocean Engineering
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• 제12권1호
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• pp.102-115
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• 2020

In this study, the SST k - ω turbulence model and the sliding mesh technology based on RANS method have been adopted to simulate the exciting force and hydrodynamic of a pump-jet propulsor in different oblique inflow angle (0°, 10°, 20°, 30°) and different advance ratio (J = 0.95, J = 1.18, J = 1.58).The fully structured grid and full channel model have been adopted to improved computational accuracy. The classical skewed marine propeller E779A with different advance ratio was carried out to verify the accuracy of the numerical simulation method. The grid independence was verified. The time-domain data of pump-jet propulsor exciting force including bearing force and fluctuating pressure in different working conditions was monitored, and then which was converted to frequency domain data by fast Fourier transform (FFT). The variation laws of bearing force and fluctuating pressure in different advance ratio and different oblique flow angle has been presented. The influence of the peak of pulsation pressure in different oblique flow angle and different advance ratio has been presented. The results show that the exciting force increases with the increase of the advance ratio, the closer which is to the rotor domain and the closer to the blades tip, the greater the variation of the pulsating pressure. At the same time, the exciting force decrease with the oblique flow angle increases. And the vertical and transverse forces will change more obviously, which is the main cause of the exciting force. In addition, the pressure distribution and the velocity distribution of rotor blades tip in different oblique flow angles has been investigated.