• Composites Research
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• 제27권2호
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• pp.47-51
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• 2014

본 논문은 기존의 유/공압 및 전기식 모터를 대체할 수 있는 경량, 고성능 지능소자 구동기를 설계/제작하고 이를 소형 무인비행체의 조종익 시스템에 적용 가능성을 연구한 것이다. 또한 압전 복합재료 작동기에 대한 성능평가를 수행하였으며, 유니모프 및 바이모프 형태의 작동기를 제작하여 각각의 작동 특성을 확인하였다. 이와 같은 성능시험 평과 결과를 통해 바이모프 형태의 작동기가 하중 유무와 무관하게 선형적인 받음각 변화를 가짐을 알 수 있었다. 이러한 지능소자 구동 시스템은 소형 로봇, 유도무기 및 MAV, UAV의 조종익 제어 시스템으로 사용될 수 있는 가능성을 확인하였다.

• 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.

• 한국군사과학기술학회지
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• 제10권3호
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• pp.120-128
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• 2007

In order to reduce the lead-time and cost, the technology of rapid prototyping(RP) has been widely used. This paper describes the methodology to fabricate a large object by using the principle of rapid prototyping. By laminating thick and sloping polystyrene foam plates, we can make the large model which has three dimensional, continuous surfaces faster and easier than conventional processes. Estimated error was much smaller than other RP products which have stepped effect. For accuracy improvement and post processing, machined metal plates are added between the thick plates. To keep the continuity of surface and strengthen the model, pilot holes and guide rods are applied. By the methodology described in this paper, a missile body with flush air intake was fabricated.

• 한국군사과학기술학회지
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• 제9권1호
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• pp.60-71
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• 2006

With the increased reliance on M & S(Modeling & Simulation) in military training, defense analysis, and system acquisition. The credibility of M & S becomes even more critical issue in the M & S application community. In this paper, we have introduced the VV & A(Verification, Validation and Accreditation) concept of M & S for the assurance of its credibility, and proposed the VV & A model applicable to a military simulator development with the illustrative example of MSAM(Medium range-Surface to Air Missile) system simulator.

• 한국시뮬레이션학회논문지
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• 제29권4호
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• pp.33-46
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• 2020

전자전은 상대방 전자전 무기체계나 장비에 대한 교란, 무력화, 공격 및 파괴를 목적으로 한다. 대공제압(SEAD: Suppression of Enemy Air Defense) 임무는 적의 방공망에 대한 무력화, 파괴, 혹은 일시적 기능 저하를 목적으로 하며, 전자전을 수행하는 대표적인 임무이다. 본 연구는 SEAD 임무의 효과도 분석을 위하여 DEVS(Discrete Event Systems Specification) 기반의 시뮬레이터를 개발하고 사례 분석을 통해 유용성을 입증한다. SEAD 임무는 SSJ(Self Screening Jamming), SOJ(Stand Off Jamming) 상황 하에서 적 지역으로 침투하여 HARM(High Speed Anti Radiation Missile)을 발사하는 단계까지로 한다. SAM의 대응은 SSJ, SOJ에 의해 성능의 저하가 초래되는 상태에서 임무를 수행하는 것으로 가정한다. 시뮬레이터는 전자전 장비의 제원(파라미터)과 운용전술(파리미터 혹은 알고리즘)의 조합이 임무효과도에 미치는 영향을 분석하는 것을 목적으로 하였다.

• 한국컴퓨터정보학회논문지
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• 제11권4호
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• pp.35-45
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• 2006

본 논문에서는 휴대용 회전 유도탄 체계의 모델링과 성능분석에 사용할 수 있는 실시간 병렬처리 시뮬레이터 개발에 대하여 기술한다. 실시간 병렬처리 시뮬레이터는 항공기의 적외선 형상을 만드는 탐색기 에뮬레이터, 실시간 컴퓨터, 시스템 유닛. 유도 조종 장치 및 탐색기 프로세서 등과 같은 하드웨어 실물장치와 실시간 컴퓨터에 내장된 수학적 모델, 6 자유도 모델 및 공력 모델 등을 구현한 응용 소프트웨어 및 호스트 컴퓨터에 내장된 사용자 프로그램 등으로 구성되었다. 실시간 컴퓨터는 병렬로 연결된 여섯 개의 TI사 C-40 프로세서로 설계되었으며, 기계적 장치와 결합된 아날로그 전자회로를 이용하여 탐색기 에뮬레이터를 설계하였다. 시스템 유닛은 구성 요소간의 임피던스 정합 기능과 미세 신호를 처리하며, 시뮬레이터와 실물 유도탄 발사 장치의 연결이 가능하다. 개발된 실시간 병렬처리 시뮬레이터를 휴대용 회전 유도탄의 성능분석 장치로 사용하기 위하여 현장실험을 통한 결과 검증시험을 수행하였다.

• 한국항공우주학회지
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• 제45권12호
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• pp.1084-1093
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• 2017

전장에서 임무를 수행하는 항공기의 생존성이 위협을 받음에 따라 항공기의 생존성을 향상시키기 위한 연구의 필요성이 커지고 있다. 본 연구에서는 항공기 Plume IR 신호에 관련된 무인전투기의 생존성을 분석하였다. 항공기의 생존성을 분석하기 위해 먼저 항공기의 IR 탐지거리인 Lock-on Range와 미사일 격추 범위인 Lethal Envelope 개념을 도입하였다. 또한 수직면 기준 분석을 포함하는 지대공 미사일에 대한 Lethal Envelope를 계산하는 기법을 개발하였다. 계산결과 무인전투기의 Red Zone이 고도 위 방향과 아래 방향의 특성 뿐만 아니라 정량적인 Zone 사이즈에서 상당한 차이가 생김을 확인하였다.

• 제어로봇시스템학회논문지
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• 제11권1호
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• pp.84-91
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• 2005

In this paper, we describe the real-time parallel processing simulator developed for the use of performance analysis of rolling missiles. The real-time parallel processing simulator developed here consists of seeker emulator generating infrared image signal on aircraft, real-time computer, host computer, system unit, and actual equipments such as auto-pilot processor and seeker processor. Software is developed from mathematic models, 6 degree-of-freedom module, aerodynamic module which are resided in real-time computer, and graphic user interface program resided in host computer. The real-time computer consists of six TIC-40 processors connected in parallel. The seeker emulator is designed by using analog circuits coupled with mechanical equipments. The system unit provides interface function to match impedance between the components and processes very small electrical signals. Also real launch unit of missiles is interfaced to simulator through system unit. In order to apply the real-time parallel processing simulator to performance analysis equipment of rolling missiles it is essential to perform the performance verification test of simulator.

• 한국군사과학기술학회지
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• 제9권3호
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• pp.25-32
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• 2006

Weapon systems composed of several subsystems execute various engagement missions in distributed combat environments in cooperation with a large number of subordinate/adjacent weapon systems as well as higher echelons through tactical data links. Such distributed weapon systems require distributed real-time simulation test beds to integrate and test their operational software, analyze their performance and effects of cooperated engagement, and validate their requirement specifications. These demands present significant challenges in terms of real-time constraints, time synchronization, complexity and development cost of an engagement simulation test bed, thus necessitate the use of high-performance distributed real-time simulation architectures, and modeling and simulation techniques. In this paper, in order to meet these demands, we presented a distributed real-time simulation system based on High Level Architecture(HLA) and Discrete Event System Specification(DEVS). We validated its performance by using it as a test bed for developing the Engagement Control System(ECS) of a surface-to-air missile system. The proposed technique can be employed to design a prototype or model of engagement-level distributed real-time simulation systems.

• Strategy21
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• 통권31호
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• pp.57-84
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• 2013

North Korea's continuous threats and provocative behaviors have aggravated tension on the Korean peninsula particularly with the recent nuclear weapons test. South Korea's best way to cope with this situation is to maintain the balance among three policy directions: dialogue, sanctions, and deterrence. Among the three, I argue that deterrence should be prioritized. There are different sources of deterrence such as military power, economic power, and diplomatic clouts. States can build deterrence capability independently. Alternatively, they may do so through relations with other states including alliances, bilateral relations, or multilateral relations in the international community. What South Korea needs most urgently is to maintain deterrence against North Korea's local provocations through the enhancement of independent military capability particularly by addressing the asymmetric vulnerability between militaries of the South and the North. Most of all, the South Korean government should recognize the seriousness of the negative consequences that North Korea's 'Nuclear shadow strategy' would bring about for the inter-Korea relations and security situations in Northeast Asia. Based on this understanding, it should develop an 'assertive deterrence strategy' that emphasizes 'multi-purpose, multi-stage, and tailored deterrence whose main idea lies in punitive retaliation.' This deterrence strategy requires a flexible targeting policy and a variety of retaliatory measures capable of taking out all targets in North Korea. At the same time, the force structures of the army, the air force, and the navy should be improved in a way that maximizes their deterrence capability. For example, the army should work on expanding the guided missile command and the special forces command and reforming the reserve forces. The navy and the air force should increase striking capabilities including air-to-ground, ship-to-ground, and submarine-to-ground strikes to a great extent. The marine corps can enhance its deterrence capability by changing the force structure from the stationary defense-oriented one that would have to suffer some degree of troop attrition at the early stage of hostilities to the one that focuses on 'counteroffensive landing operations.' The government should continue efforts for defense reform in order to obtain these capabilities while building the 'Korean-style triad system' that consists of advanced air, ground, and surface/ subsurface weapon systems. Besides these measures, South Korea should start to acquire a minimum level of nuclear potential within the legal boundary that the international law defines. For this, South Korea should withdraw from the Nuclear Non-proliferation Treaty. Moreover, it should obtain the right to process and enrich uranium through changing the U.S.-South Korea nuclear cooperation treaty. Whether or not we should be armed with nuclear weapons should not be understood in terms of "all or nothing." We should consider an 'in-between' option as the Japanese case proves. With regard to the wartime OPCON transition, we need to re-consider the timing of the transition as an effort to demonstrate the costliness of North Korea's provocative behaviors. If impossible, South Korea should take measures to make the Strategic Alliance 2015 serve as a persisting deterrence system against North Korea. As the last point, all the following governments of South Korea should keep in mind that continuing reconciliatory efforts should always be pursued along with other security policies toward North Korea.