• Journal of the Korea Institute of Military Science and Technology
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• v.10 no.1
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• pp.5-13
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• 2007

The trajectory of an current artillery munition is subject to a variety of different error sources resulting in more or less big deviation from the nominal predicted flight path. The 1D CCM(Course Correction Munition) has appeared to solve this problem and the mechanism of 1D CCM is a simple and low cost one using the influence of drag to range behavior of an artillery munition. In the paper 1D CCM concept has been simulated using wind tunnel experiment results of the specified Korean munition with CCF(Course Correction Fuze) and calculated the performance of its rang error reduction. From the simulated results it can be numerically explained that the possibility of adaptation of 1D CCM concept to Korean artillery munitions.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.11
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• pp.965-972
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• 2016

This paper presents results of flight experiments on a navigation algorithm including multiplicative extended Kalman filter for estimating attitude of the guided munition. The filter describes orientation of aircraft by data fusion with low-cost sensors where measurement update is done by multiplication, rather than addition, which is suitable for quaternion representation. In determining attitude from vector observations, the existing approach utilizes a 3-axis accelerometer as a 2-axis inclinometer by measuring gravity to estimate pitch and roll angles, while GNSS velocity is used to derive heading of the vehicle. However, during accelerated maneuvers such as coordinated flight, the accelerometer provides inadequate inclinometer measurements. In this paper, the measurement update process is newly defined to complement the vulnerability by using different vector observations. The acceleration measurement is considered as a result of a centrifugal force and gravity during turning maneuvers and used to estimate roll angle. The effectiveness of the proposed method is verified through flight experiments.

• Proceedings of the Korea Water Resources Association Conference
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• 2017.05a
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• pp.201-201
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• 2017

서울시 효자배수분구(광화문 지역)는 2010년, 2011년 호우로 인해 침수 피해가 많이 발생했던 지역으로 당시 주요 침수피해 원인은 광화문 사거리 및 경복궁역 인근에 위치하고 있는 굴곡 관로의 손실수두 증가(유입, 만곡, 마찰손실 등), 지하매설물로 인한 통수단면 감소 등으로 조사되었다. 따라서 대상지역의 침수 원인을 정확히 분석하기 위해서는 관거의 만곡, 급 확대 및 급 축소에 따른 손실계수의 적용이 요구된다. 손실계수는 유입부, 만곡부에 대한 계산식을 이용하여 산정하고 모형에 적용하였으며 적정 손실계수 값을 얻기 위해 손실계수에 대한 민감도 분석을 수행하였다. 모의 검토 대상기간은 우수관거내 수심 측정자료가 존재하는 4개의 이벤트를 선정하였으며 같은기간에 해당하는 AWS 매분단위 강우자료를 취득하여 모의에 적용하였다. 또한, 적정 손실계수를 선정하기 위해 관측치와 모의치의 적합도를 평가하였으며, 평가지표는 자료 개수에 관계없이 절대적으로 평가할 수 있는 NSE(Nash-Sutcliffe Efficiency)를 사용하였다. 손실계수 적용 여부에 따른 분석결과 손실계수를 적용한 모의치가 관측치의 오차가 미적용한 모의치보다 적합도의 평가지표가 우수하게 분석되었다. 손실계수 민감도 분석 결과는 경험식에 의해 산정된 손실계수를 적용한 Case3의 NSE가 가장 우수하게 분석되었다. 이와같이 도시 지역의 침수분석에 있어 우수관거에 대한 손실계수 적용으로 분석모형의 정밀도를 높일 수 있는 것으로 판단된다.

• Journal of the Korea Society for Simulation
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• v.29 no.4
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• pp.47-54
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• 2020

North Korea has recently developed and deployed missiles with various ranges as asymmetrical forces. Among them, short-range ballistic missiles with improved accuracy are expected to aim at achieving tactical goals by hitting important military facilities in Korea with a small number of missiles. Damage to the air force airfields, one of North Korea's main targets of missiles attack, could limit the operation of air force fighters essential to gaining air superiority. Based on the attack by the short range ballistic missiles, the damage probability of military airfields was simulated. And as the one of the concepts of passive defense, the way to reduce the loss of combat power was studied through the changes of the air force squadrons deployment. As a result, the effective deployment plan could be obtained to reduce the amount of power loss compared to the current deployment.