• Journal of Positioning, Navigation, and Timing
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• 제3권2호
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• pp.53-62
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• 2014

In the guided missile and unmanned vehicle system, the navigation system is one of the most important components. Recently, low-cost effective smart projectiles and guided bomb are being developed using MEMS based navigation system which has high-G, low-cost and small size. In this paper, locally developed MEMS based GPS/INS integrated navigation system will be introduced in comparison with the state of the art of MEMS based navigation system. And technical design and development method is described to satisfy the required performance of GPS receiver, MEMS inertial sensor assembly, navigation computer and software.

• 제어로봇시스템학회논문지
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• 제21권10호
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• pp.917-923
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• 2015

In this paper, the TSE (Triangulation based target Size Estimator) algorithm is presented to estimate static target size at IIR (Imaging Infrared) environment. The size information is important factor for accurate IIR target tracking. But the IIR sensor can't generate distance between missile and target to calculate target size. In order to overcome the problem, we propose TSE algorithm which based on triangulation measurement. The performance of proposed method is tested at target intercept scenario. The experiment results show that the proposed algorithm has suitable performance for the accurate static target size estimating.

• 산업경영시스템학회지
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• 제35권2호
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• pp.155-162
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• 2012

This work describes identification of essential considerations when we develop OMS/MP for the shipboard weapon systems. It is compulsory to develop OMS/MP which describes quantity of what mode to have and how often to operate. In this point of view, relationships between OMS/MP and shipboard weapon systems are analyzed. From the analysis, considerations of OMS/MP development for the weapon systems are presented.

• International Journal of Aeronautical and Space Sciences
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• 제12권4호
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• pp.385-395
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• 2011

An ejector was developed for man-portable missiles. The ejector can be separated from the missile after the completion of the ejection function even without any additional separation devices. This paper introduces the particular separation mechanism of the ejector and presents the methodology, based on a probabilistic design method, to predict the ejection-and-separation reliability. This approach using Monte Carlo simulation can also be applicable to the reliability prediction of one-shot items suffering from difficulties in estimating or in demonstrating their reliability due to the lack of the number of tests available.

• 제어로봇시스템학회논문지
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• 제7권12호
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• pp.1024-1030
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• 2001

In this paper, a horizontal LOS(line of sight) rate estimator for conventional sea skimming ASM(anti-ship missile) is proposed. A LOS rate dynamics model for a 2-axis gimbal system and the homing geometry is derived. A new LOS rate estimator is proposed by applying the Kalman filter theory to the LOS rate dynamics model. The proposed filter estimates LOS rates by taking roll motions into account. Simulation results show that the proposed filter produces smaller estimation errors than a conventional method.

• 시스템엔지니어링학술지
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• 제15권1호
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• pp.9-15
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• 2019

DIRCM is a device that deception missiles by directing the light source to missile seeker with infra-red laser based turret. The effectiveness of the device is affected by changes of the turret's Field of View (FoV), and also influence of the interference devices determines the effect of the DIRCM's effectiveness. Therefore finding mounting location for DIRCM is critical parameter for the DIRCM's effectiveness. so we applied stiffness review, interference analysis, FoV analysis and simulation analysis method to Multi-purpose helicopter for the find DIRCM location. As a result, in case of 1 DIRCM mounted at helicopters bottom shows 30~40% survivability. case of 2 DIRCM mounted at both side shows 70~80% survivability.

• 전기학회논문지
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• 제68권4호
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• pp.566-572
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• 2019

This paper proposes a new composite guidance law that can intercept moving targets and satisfy look angle rate constraint. In order to obtain the composite guidance law, we first develop a new look angle rate control guidance law which can maintain the maximum look angle rate limitation. And then, we propose the composite guidance scheme on the basis of the look angle rate control guidance and the proportional navigation guidance. To investigate the capturablity and characteristics of the proposed guidance, we also derive closed-form solutions and perform various numerical simulations. The proposed composite guidance only requires the line-of-sight rate, closing velocity, and missile's speed, thereby easily implementing in practical homing missiles.

• 한국인터넷방송통신학회논문지
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• 제20권2호
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• pp.87-96
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• 2020

다기능 레이다는 자원관리를 통해 표적을 탐색함과 동시에 추적한다. 한정된 자원에서 표적이 많을수록, 추적 갱신률이 빠를수록 추적에 할당되는 자원이 증가하여 탐색 자원 할당량이 감소하게 된다. 탐색 자원이 감소하면 표적의 탐지 재방문 시간, 포착 기회 수, 추적 등의 여러 레이다 탐색 성능이 저하된다. 자함 방어와 같은 복합전술 상황에서 탐지성능 저하는 유도탄의 방어 확률을 감소시킨다. 본 논문에서는 이러한 복합적인 전술상황에서의 자함 방어 분석을 위해 다기능 레이다를 탑재한 자함 모델, 레이다 모델, 표적 모델, 방어 모델 등을 구성하여 M&S도구를 개발하였다. 이를 통해 다양한 표적 환경 및 추적 성능에 따른 자함 방어의 영향성을 복합적으로 분석하였다.

• Strategy21
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• 통권44호
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• pp.142-176
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• 2018

So far, the main threat to South Korea was North Korea. That is why South Korea established a strategy based on the threat of North Korea and most of the budget on defense was used to deter North Korea. Even though the neighboring countries(China, Japan, and Russia) are growing as a real threat with abilities and intentions based on their powerful naval forces, South Korea has not yet been able to establish a strategy that regards neighboring countries as a threat. But the decades-old structural mechanism of the Korean security environment is undergoing a radical change on April 27, 2018, through the South-North summit and the Panmunjom Declaration. Under the changing security environment, South Korea was placed in a complicated dilemma that had to deal with threats of two axes(China), three axes(China, Japan), and four axes(Japan, Russia). If the one axis threat(North Korea) is dominated by land threats, the second, third and fourth axis threats are threats from the sea. This paper analyzed the maritime strategy of Korea within the framework of maritime-geopolitics, in other words recognition and expansion of the sphere of maritime. I have designed that the maritime defense space that we can deny from threats is divided into three lines of defense: 1 line (radius 3,000km), 2 lines (2,000km), and 3 lines (1,000km). The three defense zones of the three lines were defined as an active defense(1 line), defensive offense(2 line), active offense(3 line). The three defense zones of the three lines were defined as the sphere of core maritime, As a power to deny the sphere of core maritime, it was analyzed as a maneuvering unit, a nuclear-powered submarine, the establishment of missile strategy, and the fortification of islands station. The marine strategy of South Korea with these concepts and means was defined as 'Offensive Maritime Denial Strategy'.

• 한국전자파학회논문지
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• 제20권7호
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• pp.617-624
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• 2009

본 논문에서는 가역 정리에 기초한 반응 이론을 이용하여 유도탄 및 항공기 등에 적용되는 원뿔형 비구면 레이돔에 대한 전자파 성능 해석 방법을 제안하였으며 제작된 레이돔에 대한 전자파 성능 측정 결과를 해석 결과와 비교함으로써 제안한 해석 방법의 타당성을 검증하였다. 안테나는 "X" 형태의 2축 모노펄스 구조를 갖는 도파관 슬롯 배열 안테나로 가정하였다. 레이돔 형상은 본 칼만 형태로 가정하였으며, 레이돔 길이 대 직경비를 2:1 로 가정하였다. 실제 제작된 레이돔에 대한 전자파적 특성은 레이돔 전용 측정 장비를 이용하여 측정하였으며, 레이돔 측정 결과가 본 논문에서 제시한 해석 기법을 이용하여 해석한 결과와 잘 일치하는 것을 확인하였다. 본 논문에서 개발한 해석 기법은 유도탄이나 항공기용 레이돔 개발에 적용할 수 있을 것으로 기대된다.