• The Journal of the Acoustical Society of Korea
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• v.34 no.5
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• pp.377-384
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• 2015

An active noise control (ANC) algorithm for noise canceling headphone is proposed. In this study, the feedback ANC operated with the filtered-x least mean square algorithm (FxLMS) algorithm is used to attenuate the undesired noise. Also an adaptive residual music canceller (RMC) is proposed for enhancing the accuracy of the reference signal of the feedback ANC. Simulation results show that a high quality of music sound can be consistently achieved in a time-varying secondary path situation.

• Proceedings of the IEEK Conference
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• 1998.10a
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• pp.1179-1182
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• 1998

광대역 능동잡음제거는 수 백개의 적응필터 탭 수를 갖는다. 탭 수가 긴 적응필터는 많은 계산량이 요구된다. 본 논문에서는 적응계수 벡터가 서브밴드로 계산되는 M-채널 QMF 필터뱅크와 적응필터를 이용한 자동차 소음제거 모델을 제안한다. 분해 필터뱅크와 합성 필터뱅크는 cosine-modulated pseudo QMF 필터를 사용한다. 오차경로의 전달특성을 온라인 인식하기 위한 기준신호는 적응필터의 출력신호와 저주파대역의 서브밴드 출력신호와의 차신호를 사용한다. 따라서 제안한 자동차 소음제거 모델은 계산량이 적고 수렴속도가 빠른 견실한 시스템이 되도록 제안한다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2010.05a
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• pp.742-743
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• 2010

• Journal of KSNVE
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• v.2 no.1
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• pp.3-14
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• 1992

음장의 공간적 변환(Spatial Transformation of Sound Field; STSF)기법의 주요 원리를 간단히 소개한 뒤, STSF에서 Reference 신호의 사용을 보다 상세히 취급하고자 한다. Reference의 보통의 형태(표준 Reference)는 음장 모델에 포함될 전체음장의 일부분, 즉 이 Reference의 연관이 있어 포함될 부분을 결정한다. 결국 한 개 의 표준 Reference는 항상 적용되어져야 한다. 2번째 Reference의 형태(삭제용 Reference)는 모델로부터 원치 않는 무관한 음장성분을 제거하는데 적용된다. 이 Reference와 밀접한 음장 부분이 모델로부터 제거될 것이고, 그렇지 않는 경우는 포함된다. 실제 예에서는 삭제용 Reference가 암소음의 억제와, 음원의 어떤 독립 적인 성분의 억제를 위해 어떻게 적용되는가를 보인다.

• The Journal of the Acoustical Society of Korea
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• v.41 no.6
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• pp.691-697
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• 2022

In this work, a straightforward component design of a direct current (DC) relay equipped in electric vehicles is discussed. The work aims to provide and evaluate effective measures for reducing high-frequency sound from the DC relay carrying electric power. From the operation experiments for the relay, it is observed that noise is caused by the resonance from the forced vibration by the electromagnetic repulsive force originating at the area of electric contacts with a resonance frequency of around 710 Hz ~ 730 Hz. A finite element model for the relay was established to conduct vibration mode analysis, consisting of stationary and movable contacts and a contact spring. Vibration mode analysis indicates that in the resonance frequency, the movable contact with two-point contacts experiences rotational vibration mode. For the proposed relay with a three-point contact, vibration mode analyses give reasonable results of reducing noise at that frequency. Furthermore, for the fabricated relays with the three-point contact, similar results have been obtained. In conclusion, one can see that the proposed measures provide one of the feasible solutions to the reduction of relay noise.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.16 no.7 s.112
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• pp.677-682
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• 2006

In the case of aeroacoustic test in windtunnel, measurement accuracy is reduced by not only Doppler effects but also by the microphone self noise due to airflow and high turbulence in the wall boundary layer. Microphone array measurements can be easily utilized for the solutions of these problems. In this paper, geometrical optics approach and diagonal term elimination of cross spectral matrix was introduced to the de-dopplerization and self noise reduction methods for the microphone array measurement. For the validation, beamforming tests for sinusoidal point source were performed in the closed type test section of windtunnel, and their performances of beam width and sidelobe rejection were significantly improved.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2005.11a
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• pp.822-825
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• 2005

In the case of aeroacoustic test in windtunnel, measurement accuracy is reduced by not only Doppler effects but also by the microphone self noise due to airflow and high turbulence in the wall boundary layer. Microphone array measurements can be easily utilized for the solutions of these problems. In this paper, geometrical optics approach and diagonal term elimination of cross spectral matrix was introduced to the de-dopplerization and self noise reduction methods for the microphone array measurement. For the validation, beamforming tests for sinusoidal point source were performed in the closed type test section of windtunnel, and their performances of beam width and sidelobe rejection were significantly improved.

• Journal of the Korea Institute of Information Security & Cryptology
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• v.32 no.5
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• pp.881-890
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• 2022

As individual and group users actively use drones, the risks (Intrusion, Information leakage, and Sircraft crashes and so on) in no-fly zones are also increasing. Therefore, it is necessary to build a system that can detect drones intruding into the no-fly zone. General acoustic drone detection researches do not derive location-independent performance by directly learning drone sound including environmental noise in a deep learning model to overcome environmental noise. In this paper, we propose a drone detection system that collects sounds including environmental noise, and detects drones by removing noise from target sound. After removing environmental noise from the collected sound, the proposed system predicts the drone sound using Mel spectrogram and CNN deep learning. As a result, It is confirmed that the drone detection performance, which was weak due to unstudied environmental noises, can be improved by more than 7%.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1994.10a
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• pp.217-224
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• 1994

변속기에서 발생하는 치타음을 클러치를 통하여 해결하려는 방법으로 자동차 중립시와 주행시 각기 다른 비틀림특성을 갖는 클러치를 대상으로 한 실험으로부터 엔진플라이휠, 인풋기어, 변속기 케이스의 진동을 측정하고 분석함으로써 다음과 같은 결론을 얻었다. 자동차 중립시나 주행시에 수동변속기에서 발생하는 치타음은 클러치를 통하여 해결될 수 있음을 알 수 있었다. 클러치의 프리댐퍼와 메인댐퍼의 비틀림강성과 히스테리시스는 중립시와 주행시 치타음에 대해 각기 다른 특성을 갖게 되는데 메인 댐퍼만으로 구성된 클러치는 주행시에는 치타음을 제거하는데 효과적이지만 중립시에는 인풋기어의 비틀림 공진에 의하여 변속기가 가진되어 치타음이 발생하였다. 주행시 변속기 치타음 제거효과를 감소시키지 않고 중립시 변속기에서 발생하는 치타음을 제거하기 위해 메인댐퍼만으로 이루어진 클러치디스크에 프리댐퍼 부분을 첨가하여 보았는데 자동차 주행시의 치타음 제거효과를 유지하면서 중립시의 치타음을 제거시킬 수 있다는 것을 확인하였다.

• The Journal of the Acoustical Society of Korea
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• v.39 no.4
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• pp.364-370
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• 2020

Rocket noise generated from the exhaust plume produces the enormous acoustic loading, which adversely affects the integrity of the electronic components and payload (satellite) at liftoff. The prediction of rocket noise consists of two steps: the supersonic jet exhaust is simulated by a method of the Computational Fluid Dynamics (CFD), and an acoustic transport method, such as the Helmholtz-Kirchhoff integral, is applied to predict the noise field. One of the difficulties in the CFD step is to remove the boundary reflection artifacts from the finite computation boundary. In general, artificial damping, known as a sponge layer, is added nearby the boundary to attenuate these reflected waves but this layer demands a large computational area and an optimization procedure of related parameters. In this paper, a cost-efficient way to separate the reflected waves based on the two microphone method is firstly introduced and applied to the computation result of a laboratory-scale supersonic jet noise without sponge layers.