• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2002.04a
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• pp.43-43
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• 2002

인공위성은 일반적으로 추력기(thruster)에서 플룸(plume)을 거의 진공에 가까운 외부환경으로 사출하여 자세를 제어한다. 이 때, 사출되는 플룸에 의해 위성체의 고도에 영향을 줄 수 있는 교란추력/교란토크, 열하중(thermol loading), 정밀계측장비에 영향을 주는 오염(contamination) 등, 여러 부정적인 효과들이 야기될 수 있으며, 이들 효과들은 결론적으로 위성체의 수명을 단축하기 때문에 이들에 대한 정확한 예측은 위성체 설계단계에서 매우 중요하다.

• Computational Structural Engineering
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• v.8 no.3
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• pp.11-21
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• 1995

3차원 대규모 지하구조물의 동적응답을 결정하기 위한 일반적인 수치해석이 제안되었다. 지반과 구조물을 해석하기 위하여 Laplace 변환을 적용한 경계요소법을 설명하였고, 지반-구조물계에 작용하는 외부 동적하중과 지진파를 고려할 수 있도록 공식화하였다. 동적교란이 전파되는 경우에 시간영역의 응답을 얻기 위하여는 구해진 변화된 해를 수치적인 Laplce 역변환을 수행하여야 하지만 동적교란이 조화적인 경우에는 응답이 주파수 영역으로부터 직접 얻어지며, 역변환이 필요하지 않다. 이 방법의 특징은 높은 정확도와 효율성이며, 지반-구조물계에 대하여 초기조건 및 점탄성 재료의 거동을 쉽게 고려할 수 있다는 것이다. 그러므로 이 방법은 다양한 지하구조물의 동적거동과 지진에 대한 취약함을 연구하기 위한 적절한 도구로 사용되어 질 수 있다.

• Proceedings of the Korea Water Resources Association Conference
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• 2010.05a
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• pp.1760-1763
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• 2010

산지환경급변지역에서 집중호우에 의한 다량의 토사유출은 하천유역내 사회기반시설을 파괴하는 재해요인으로 작용할 수 있다. 본 연구에서는 산지환경급변지역 중 인위적인 지표교란 지역으로 대표되는 도로공사지역을 선정하여 집중호우가 발생하는 6월, 7월, 8월의 강우사상별 강우에너지와 토양침식 및 토사유출의 관계를 조사하였다. 조사결과 강우에너지가 커질수록 토양침식 및 토사유출량이 증가하는 결과를 나타내고 있다. 토양침식 조사를 위한 조사구에서 토양침식량은 식생요인과 관리상태에 따라 크게 영향을 받았다. 일반적으로는 강우에너지 증가에 따라 토양침식량이 증가한다. 도로공사지역에서는 심각한 지표교란뿐만 아니라 선행강우, 세류의 존재 여부, 그리고 외부적 요인들 때문에 상대적으로 작은 규모의 강우에 대해서도 다량의 토양침식량이 발생하는 것을 확인할 수 있었다. 교란이 발생하지 않은 인근 산지의 대조구와 공사에 의한 교란 나지사면 조사구를 비교해보았을 때, 평균 토양침식량은 약 7,352배의 차이를 보였으며, 섬유매트처리 및 사면포장처리 조사구처럼 인공적인 관리를 수행한 조사구와는 약 132배의 차이를 보였다. 또한, 인공적인 관리를 수행한 조사구는 지표사면관리의 영향과 야생종의 유입으로 지표가 안정되어 나지사면 조사구에 비해 상대적으로 적은 양의 토양침식이 발생하였다. 이는 지표교란이 심한 공사활동 지역에서는 지표특성에 따른 적합한 사면 응급처리 기법의 적용이 중요함을 나타내는 것이다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.3
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• pp.95-101
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• 2004

Stability rating of KSR-III rocket engine is conducted based on stability rating tests in the course of development of KSR-III rocket engine. Rocket engine is approved to have combustion stabilization ability when it can suppress the external perturbation or pressure oscillation with finite amplitude and recover the original stable combustion. Rocket engine in flight may be perturbed by unexpectedly large-amplitude pressure oscillation and thus a designer should not only assure combustion stabilization ability of the engine but also quantify the stabilization capacity. For this, principal quantitative parameters and their evaluation are introduced. To verify dynamic stability of KSR-III rocket engine, six stability rating tests have been conducted. Based on these test results, such parameters are quantified and thereby, the stabilization capacity of KSR-III rocket engine is evaluated.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.1
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• pp.69-77
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• 2005

To optimize and limit the axial length of the baffle of the KSR-III engine, stability rating tests using pulse gun as one of artificial disturbance devices have been done. Generally a rocket engine can be considered to be dynamically stable if a certain imposed external perturbation or pressure oscillation in rocket combustion chamber could be suppressed within a short time period. Decay time and other parameters for the evaluation of stabilization ability of an engine to external perturbation have been analyzed to quantify stabilization capacity of engine, in other words, dynamic stability margin. Baffle not covering flame zone enough which can be considered as collision region of injector wasn't be able to suppress external perturbation sufficiently. The limit of combustion stability margin of engine is assumed to be 50 mm length baffle of the KSR-III engine.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.41 no.8
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• pp.783-789
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• 2017

In terms of 3D orientation estimation based on nine-axis IMMU(inertial and magnetic measurement unit), there are two disturbance components decreasing estimation accuracy: one is external acceleration disturbing accelerometer's signals and the other is magnetic disturbance related to magnetometer's signals. In order to minimize effects by these two disturbances, two approaches including switching approach and model-based approach have been suggested and further research comparing these two has also been conducted. Nevertheless, effect of disturbance modeling differences on orientation estimation accuracy in model-based approach has not been studied before. This paper compares the recently reported two orientation estimation algorithms that have difference in disturbance models, in order to investigate the effect of disturbance models on accuracy of IMMU-based orientation estimation under various operating conditions. This research shows that the difference in disturbance models leads to difference in process noise covariance matrix. Consequently, this affected the orientation estimation, i.e., the estimation differences between the algorithms were root mean square errors of $1.35^{\circ}$ in average and $3.63^{\circ}$ in yaw estimation.

• The Journal of the Acoustical Society of Korea
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• v.28 no.2
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• pp.127-134
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• 2009

In this study, possibility of the laser eavesdropping is investigated on the window glasses with various thicknesses, Glass windows are excited by maximum length sequency (MLS) signal and the vibration sound is detected by a laser doppler vibrometer. From the detected sound, speech intelligibility is objectively estimated. Speech transmission index (STI), which is based on the modulation transfer function (MTF). is calculated for the estimation. Finally, disturbing wave effect on the speech intelligibility is analysed by using an outside speaker and a window shaker attached on the glass window. The purpose of the study is to estimate the possibility of remote eavesdropping by the laser sensor and to evaluate the performance of the homemade window shaker to protect from the remote eavesdropping.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.20 no.1
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• pp.222-229
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• 2016

Active synthetic aperture sonar on the small UUV is generated several trajectory disturbances under the influences of underwater environments, and causing a large error in the synthetic aperture processing. In this paper, we analyzed the effects of azimuth resolution for the phase mismatch of the synthetic aperture focus processing when the periodic or random trajectory disturbances was generated on the side direction. The simulation results show that ghost targets are generated and azimuth resolution is very deteriorated when disturbance amplitude is greater than $0.3{\lambda}$ and disturbance period is greater than $2L_{sa}$ in the periodic trajectory disturbances environments. And detection performance on the seabed small objects by the synthetic aperture processing is shown that there is a significant effects on the azimuth resolution depending on the types and conditions of the platform trajectory disturbance variations.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.21 no.1
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• pp.215-222
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• 2017

An active synthetic aperture sonar mounted on small UUV is generated various trajectory disturbances in the traveling path by the influence of external underwater environments. That is the phase mismatch occurs in the synthetic aperture processing of the signals reflected from seabed objects and fetches the detection performance decreases. In this paper, we compensated deteriorated images by the active SAS autofocus processing using DPC and analyzed the effects of detection performance when the periodic trajectory disturbances occur in the side direction at a constant velocity and straight movement of UUV. Through simulations, the deteriorated images according to the periodic disturbance magnitudes and period variations in the platform were compensated using difference phases processing of the overlapping displaced phase centers on the adjacent transmitted ping signals, and we conformed the improved performance characteristics of azimuth resolution and detection images at 3dB reference point.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.5
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• pp.79-87
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• 2002

Acoustic responses to pressure oscillations in axisymmetric combustion chamber are numerically investigated to examine the qualitative trend of acoustic instability in liquid rocket engine. Chamber operating condition and excitation frequency of oscillating pressure are selected as exciting parameters of acoustic instability. Artificial perturbation is simulated by total-pressure oscillation with sine wave at chamber inlet. Many approximations and simplifications are introduced without losing the essence of acoustic pressure response. First, steady-state solution for each operating condition is obtained and next, transient analysis is conducted. Depending on operating condition and excitation frequency, the distinct response characteristics are brought. Weak-strength flames and high-frequency excitation tend to cause sensitive acoustic pressure response leading to unstable pressure field. These results are analyzed based on the correlation with acoustic pressure responses from the previous works adopting laminar flamelet model.