• 한국추진공학회:학술대회논문집
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• 한국추진공학회 1997년도 제8회 학술강연회논문집
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• pp.121-129
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• 1997

Wave propagation was studied for an unidirectionally reinforced composite materials. The velocities, the particle directions and the amplitudes of reflected and transmitted waves were obtained. This analysis involves an immersion C-scan procedure. Snell's law was modified to get the velocities of waves. This analysis could be applied to the detection of flaws in a transversely isotropic composite motor case.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2002년도 하계학술대회 논문집 D
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• pp.2659-2661
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• 2002

The development of guided missile requires complex guidance schemes and hardware units because of high maneuver, delicate and variable missions. In this point of view, simulation systems and facilities which test missile hardwares and softwares are needed. This paper introduces the hardware-in-the loop simulation system and facilities which include the real-time computation systems and 3 Axis FMS(Flight Motion Simulator).

• 한국군사과학기술학회지
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• 제23권5호
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• pp.466-474
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• 2020

Semi-active laser missile systems with high accuracy are necessary to asymmetric threats, such as UAV(Unmanned Aerial Vehicle). They are usually used to attack stationary or slow moving targets, therefore we should study on the laser designator which can detect and track fast moving targets in order to deal with UAV. In this study, design specifications are came up through performance analysis of existing laser designators, and laser designation method for fast moving target is developed. The detection and tracking performance of developed laser designator are verified through inside/outside tests on ground/aerial stationary/moving targets. Through this study, we obtain laser designator techniques that could be applied to actual semi-active laser missile systems.

• 한국군사과학기술학회지
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• 제22권4호
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• pp.536-544
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• 2019

During the assembly and function inspection of missile system, flight simulation process is required. In the conventional flight simulation check of missiles, an inertial navigation system simulator was used to transmit the navigation output data acquired in HILS. There are several disadvantages in terms of check configuration complexity and data synchronization when using the simulator. So we proposed a new flight simulation method that utilizes the nonvolatile built-in memory of the aviation control unit. The data processing procedure and operation procedure of the proposed method for type I and type II missiles are presented. And we analyzed the causes of the difference between proposed method result and the HILS result for type II missile. By comparing the results obtained by the experiments using the proposed method with the results of HILS, the validity of proposed method was confirmed.

• 한국군사과학기술학회지
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• 제13권6호
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• pp.1019-1025
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• 2010

This paper describes on methods in test and evaluation of the guided rocket munitions of the domestic new generation multiple launcher rocket system. We modified and refer to the present model of air-to-air missile(AAM) and surface-to-air missile(SAM). Also we suggested a method of surface-to-surface missile(SSM) based on the characteristics of the guided rocket in test and evaluation(T&E). According to this study, the suggested activity of T&E should be observed methods compatible with each item on the established model. Therefore, we expect that the proposed research material will be a good guide to the study of a surface-to-surface missile(SSM) installed GPS/INS integration navigation guidance & control systems in the future.

• 한국항행학회논문지
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• 제19권5호
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• pp.363-369
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• 2015

본 논문은 잠수함 발사 탄도미사일(SLBM) 탐지를 위한 해상 센서플랫폼의 배치에 관한 연구이다. 최근 북한은 SLBM의 수중 사출시험을 실시하였으며 이는 국제사회에 심각한 안보 위협이 되고 있다. 이러한 위협에 효과적으로 대응하기 위해 기동이 가능한 해상 센서플랫폼은 SLBM의 탐지 가능성이 높은 위치에 배치되어야 한다. 그러나 전형적인 레이더 센서체계의 최대탐지거리 특성은 표적의 비행궤적과 레이더 반사 단면적(RCS)에 따라 달라진다. 이러한 관점에서 본 연구는 SLBM의 전술적 특성에 따른 비행궤적을 분석하고, RCS를 계산하였다. 또한 센서 플랫폼의 위치에 따른 탐지 시간을 분석하여 효과적으로 SLBM을 탐지할 수 있는 해상 센서 플랫폼의 위치를 제시하였다.

• 한국시뮬레이션학회논문지
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• 제15권4호
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• pp.69-77
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• 2006

위치 선정이나 설비배치문제를 기존의 정성적 접근방법에서 벗어나 수학적 방법을 통해 해결하려는 시도가 여러 분야에서 이루어지고 있다. 지역담당모형은 이러한 연구 분야중 하나로 주어진 문제를 수학적으로 현실과 유사하게 구현시킬 수 있고 모형에 대한 해법절차도 다양하기 때문에 여러 형태의 배치문제들에도 폭넓게 적용되어 왔으며 최근 들어서는 군사설비분야에서도 그 활용도가 높아지고 있다. 본 연구는 미사일 방어를 위하여 한국해군 KDX 함정의 최적배치에 대한 시뮬레이션 모델을 구축하였다. 시뮬레이션 모델은 부분지역담당모형을 바탕으로 공격자와 방어자의 측면을 단계적으로 평가하는 방법으로 구현되어 있으며, 구축된 모형에 대하여 가능한 시나리오를 설정하고 실험을 통하여 결과를 분석하였다. 구현된 모형실험은 공격자의 공격계획과 공격계획에 따른 최적의 KDX 배치선정과 방어미사일 할당에 대한 의사결정방안을 제시하고 있다. 본 연구의 최적배치모형은 한국적 미사일방어 체계구축을 위하여 도입될 최신무기체계의 위치선정에 대한 최적의 대안을 제시하고 효율적인 부대배치를 위한 참고자료로 활용할 수 있을 것이다.

• 한국군사과학기술학회지
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• 제18권6호
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• pp.808-815
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• 2015

For performance improving of C-band radar altimeter used in a missile system, Ku-band radar altimeter is developed. To utilize the time delay devices which are used in testing C-band radar altimeter, we proposed C-band and Ku-band frequency conversion method and implemented it as a part of missile system test equipment. In this paper we present design contents, development results and test application results of radar altimeter test equipments.

• 한국군사과학기술학회지
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• 제17권6호
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• pp.733-743
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• 2014

Since the technology of anti-ship missiles has advanced rapidly, defending battleships from the threat of anti-ship missiles is a crucial factor for the survival of warships. In this paper, we analyze the performance of an anti-ship missile defense system whose name is Close-In-Weapon-System. We show the survival probability of a warship equipped with the Close-In-Weapon-System as the number of anti-ship missiles attacking the warship varies. Because of the complex and dynamic operational characteristics surrounding the Close-In-Weapon-System such as speed of missiles, different range of an individual weapon in the weapon system, and the continuous change of the kill probability of the missiles corresponding to the distance of missiles from ships, few work has been done for the performance of Close-In-Weapon-System. We present a model to incorporate all the dynamic characteristics of the system using absorbing Markov Chain. With our results, we expect commanders of warships equipped with Close-In-Weapon-System to be provided with more helpful information on how to deal with the anti-ship missiles.

• 한국군사과학기술학회지
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• 제18권3호
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• pp.253-259
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• 2015

This paper introduces a signal processing technique for discrimination of missile target. In order to detect and discriminate the target, a seeker radar makes use of chirp waveform and stretch processing to generate high resolution range profiles(HRRPs). RELAX(relaxation) algorithm, which is one of the spectral estimation techniques, was used to find scattering centers of a missile from HRRP. From the information on the distribution of one-dimensional(1-D) scattering centers on a target, we can discriminate the target without noise.