• 한국소음진동공학회논문집
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• 제16권7호
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• pp.777-783
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• 2006

In this study, quantitative ground vibration values and damping coefficient produced by underwater blasting were measured and analyzed. Also, hydrospace noise in aquafarm and noise in atmosphere as well as ground vibrations were measured, and maximum values of these results were 86,8 dB(A), 147,8dB(A), 0.244 cm/s, respectively, With these results, vibration influence about snakehead (channa argus) and structures were examined. the damage of those was proved that is not. Equations of vibration ($V_{50%}=1.507SD^{-0.536},\;V_{95%}=2,171SD^{-0.536}$) and hydrospace noise ($SL=293.2SD^{-0.164}$) were presented from quantitative experiment results. respectively. The results of the study may be applied for the evaluation of the influence on aquafarm as a basic data before having main underwater blasting at construction sites.

• 한국구조물진단유지관리공학회 논문집
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• 제12권5호
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• pp.47-54
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• 2008

본 연구에서는 수중발파로 인해 발생되는 지반의 진동과 수중소음, 진동의 감쇠정도를 계측 및 분석하였다. 실험과 신뢰성이론으로 부터 진동추정식을 $V=K(SD)^{-0.536}$으로 제시하였으며, 발파상수 K값은 신뢰도 50%, 90%, 99.9%에 따라 1.507, 2.005, 2.939로 각각 얻어졌다. 수중발파로 인한 육상의 소규모 저수지(양식어장)의 수중소음추정식은 실측된 수중소음 자료를 이용하여 $SL=293.2SD^{-0.164}$로 제시하였으며, 수중에서는 최대 86.8dB(A), 대기중에서는 최대 147.8dB(A)의 소음이 계측되었다. 이러한 연구결과들을 고려하여 수중발파 설계 및 영향성 평가가 가능한 흐름도를 제시하였다. 수중발파에 대한 영향평가 연구는 이제 시작하는 단계로써 지속적이고 다양한 경우에 대한 연구가 보완되어야 할 것으로 판단된다.

• Journal of Hydrospace Technology
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• 제2권1호
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• pp.18-26
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• 1996

It is normal practice to consider bending wave modes only, when one applies SEA (Statistical Energy Analysis) to ship structures because of complexities in SEA modeling and evaluation of coupling loss factors for inplane modes. According to the result of Tratch[1], the inplane wave modes becomes important for the analysis of a foundation structure as the distance from the source and receiver increases. In this paper, the effect of inplane wave modes on structure-borne noise propagation in ship structures is presented. It is shown that the inplane wave could increase the noise level more than 10 dB compared with the results without inplane wave modes at high frequency bands for compartments far from the source location.

• Journal of Hydrospace Technology
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• 제1권1호
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• pp.75-88
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• 1995

Auto-Pilot System uses heading angle information via the position sensor and the rudder device to control the ship's direction. Most of the control logics are composed of the state estimation and control algorithms assuming that the measurement device and the actuator have no fault except the measurement noise. But such asumptions could bring the danger in real situation. For example, if the heading angle measuring device is out of order the control action based on those false position information could bring serious safety problem. In this study, the control system including improved method for processing the position information is applied to the Auto-Pilot System. To show the difference between general state estimator and F.D.F., BJDFs for the sensor and the actuator failure detection are designed and the performance are tested. And it is shown that bias error in sensor could be detected by state-augmented estimator. So the residual confined in the 2-dimension in the presence of the sensor failure could be unidirectional in output space and bias sensor error is much easier to be detected.