• 제목/요약/키워드: Missile defense

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미국의 탄도미사일 방어체계와 THAAD (U.S. Ballistic Missile Defense System and THAAD)

  • 박영철;박태용
    • 한국정보통신학회:학술대회논문집
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    • 한국정보통신학회 2015년도 추계학술대회
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    • pp.455-457
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    • 2015
  • 제2차 세계대전 중에 최초의 탄도미사일인 V-2가 등장한 이후 발전하는 과학기술에 힘입어 미사일의 사거리, 정밀도 등이 비약적으로 향상됨에 따라 탄도미사일의 위협은 나날이 커지고 있다. 미국은 탄도미사일의 위협으로부터 자국 및 동맹국을 보호하기 위해 탄도미사일 방어체계(BMDS, Ballistic Missile Defense System)를 운용하고 있다. 센서에 의해 탐지된 탄도미사일은 요격 체계의 종류에 따라 부스트단계(Boost phase), 중간단계(Midcourse phase), 종말단계(Terminal phase) 등에서 요격하게 되며, THAAD(Terminal High Altitude Area Defense)는 고고도 종말단계에서 요격하는 체계이다. 본 논문에서는 미국의 탄도미사일 방어체계의 개념에 대해 간략히 설명하고, 그 중 THAAD의 운용 및 기술적 특징에 대해 집중적으로 조사하여 정리하였다.

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Arrow 미사일 방어체계 개발 현황 (Development Status of Arrow Missile Defense System)

  • 박태용
    • 한국정보통신학회:학술대회논문집
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    • 한국정보통신학회 2018년도 춘계학술대회
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    • pp.283-284
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    • 2018
  • 이스라엘의 미사일 방어체계인 Arrow 체계는 미국과 이스라엘 간 전략적 협력관계를 통해 개발되었다. 미국 레이건 행정부의 전략방위구상(Strategic Defense Initiative, SDI) 연구에 이스라엘이 1986년에 협력함으로써 전술탄도미사일 방어체계 개발이 시작되었고, 두 차례의 획기적인 성능개량을 통해 현재 Arrow 3까지 개발되어있다. 주변국으로부터 탄도미사일 위협을 직접적으로 받고 있고, 전장의 종심이 짧은 이스라엘의 지정학적 환경에 맞도록 개발되고 지속적으로 업그레이드되고 있는 Arrow 미사일 방어체계의 개발 사례는 한반도 환경에 적합한 탄도미사일 방어체계를 구축함에 있어 모범적 사례가 될 수 있다.

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미사일 방어를 위한 방공포대 최적 배치 문제 (The Optimal Deployment Problem of Air Defense Artillery for Missile Defense)

  • 김재권;설현주
    • 산업경영시스템학회지
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    • 제39권1호
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    • pp.98-104
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    • 2016
  • With the development of modern science and technology, weapon systems such as tanks, submarines, combat planes, radar are also dramatically advanced. Among these weapon systems, the ballistic missile, one of the asymmetric forces, could be considered as a very economical means to attack the core facilities of the other country in order to achieve the strategic goals of the country during the war. Because of the current ballistic missile threat from the North Korea, establishing a missile defense (MD) system becomes one of the major national defense issues. This study focused on the optimization of air defense artillery units' deployment for effective ballistic missile defense. To optimize the deployment of the units, firstly this study examined the possibility of defense, according to the presence of orbital coordinates of ballistic missiles in the limited defense range of air defense artillery units. This constraint on the defense range is originated from the characteristics of anti-ballistic missiles (ABMs) such as PATRIOT. Secondly, this study proposed the optimized mathematical model considering the total covering problem of binary integer programming, as an optimal deployment of air defense artillery units for defending every core defense facility with the least number of such units. Finally, numerical experiments were conducted to show how the suggested approach works. Assuming the current state of the Korean peninsula, the study arbitrarily set ballistic missile bases of the North Korea and core defense facilities of the South Korea. Under these conditions, numerical experiments were executed by utilizing MATLAB R2010a of the MathWorks, Inc.

공력 조종면 데이터베이스 확장을 통한 저 충실도 해석자의 정확도 개선 (Accuracy Improvement of Low Fidelity Solver by Augmentation of Fin Aerodynamic Database)

  • 강은지;김영화;임경진;이재은;강경태
    • 한국군사과학기술학회지
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    • 제25권1호
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    • pp.45-54
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    • 2022
  • There has been necessity to supplement the fin database to improve the accuracy of low-fidelity aerodynamic solver for missile configuration. In this study, fin database is expanded by in-house solver, utilized in the triservice data the previously established into regions beyond means of CFD. Fin alone data of CFD analysis results in the original region is matched well with triservice data originated from the wind tunnel tests. Extensive fin aerodynamic data from CFD analysis is added to the existing database of the low-fidelity solver. For confirmation, aerodynamic characteristics of body-tail and body-canard-tail missile configurations is computed using upgraded low-fidelity solver at transonic region. The result using improved solver shows good agreements with wind tunnel test and CFD analysis results, which implies that it becomes more accurate.

단거리 대공방어유도탄체계와 이기종 함정 전투체계간 최적의 연동 설계 기법 (Optimal Interface Design between Short-Range Air Defense Missile System and Dissimilar Combat Systems)

  • 박현우
    • 한국군사과학기술학회지
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    • 제18권3호
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    • pp.260-266
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    • 2015
  • The warship is run based on the combat system which shares tactical information collected by target detection systems and navigation devices across a network, and conducts the command and control of weapons from target detection to kill assessment. The short-range air defense missile system defends a warship from anti-ship missiles, aircraft, helicopter and other threats in order to contribute to the survival of a warship and the success of missions. The short-range air defense missile system is applied to a various combat systems. In this paper, we have proposed the interface design between the short-range air defense missile and dissimilar combat systems. To employ the short-range air defense missile at dissimilar combat systems, each system is driven by independent processor, and the tasks which are performed by each system are assigned. The information created by them is exchanged through the interface, and the flow of messages is designed.

이지스함의 탄도미사일 방어를 위한 운용개념 도출 (Derivation of Operational Concept for the BMD of the Aegis Ship)

  • 이경행;백병선
    • 항공우주시스템공학회지
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    • 제10권3호
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    • pp.44-51
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    • 2016
  • This paper describes the operational concept of the Aegis ship's missile defense. Recently, North Korea conducted a fourth nuclear-weapon test that involved the launch of a long-range missile and the underwater launch of an SLBM. The ground-based BMD (Ballistic Missile Defense) system is very limited for the SLBM of a miniaturized nuclear warhead; therefore, it is necessary to build a reliable sea-based missile-defense system. The ROK Navy has, however, only utilized the Aegis ship that is designed with a search-and-tracking sensor but is without a ballistic-missile interception capability. Given this information, this work focuses on the operational concept of the Aegis BMD by comparing the BMD capabilities of the ROK with those of the U.S.

자산기반 무기할당 문제의 선형 근사 모형 (A Linear Approximation Model for an Asset-based Weapon Target Assignment Problem)

  • 장준건;김경택;최봉완;서재준
    • 산업경영시스템학회지
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    • 제38권3호
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    • pp.108-116
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    • 2015
  • A missile defense system is composed of radars detecting incoming missiles aiming at defense assets, command control units making the decisions on weapon target assignment, and artillery batteries firing of defensive weapons to the incoming missiles. Although, the technology behind the development of radars and weapons is very important, effective assignment of the weapons against missile threats is much more crucial. When incoming missile targets toward valuable assets in the defense area are detected, the asset-based weapon target assignment model addresses the issue of weapon assignment to these missiles so as to maximize the total value of surviving assets threatened by them. In this paper, we present a model for an asset-based weapon assignment problem with shoot-look-shoot engagement policy and fixed set-up time between each anti-missile launch from each defense unit. Then, we show detailed linear approximation process for nonlinear portions of the model and propose final linear approximation model. After that, the proposed model is applied to several ballistic missile defense scenarios. In each defense scenario, the number of incoming missiles, the speed and the position of each missile, the number of defense artillery battery, the number of anti-missile in each artillery battery, single shot kill probability of each weapon to each target, value of assets, the air defense coverage are given. After running lpSolveAPI package of R language with the given data in each scenario in a personal computer, we summarize its weapon target assignment results specified with launch order time for each artillery battery. We also show computer processing time to get the result for each scenario.

극초음속 미사일 대응을 위한 방어체계에 관한 연구 (A Study on the Defense System of the Hypersonic Missile Systems)

  • 이경행
    • 항공우주시스템공학회지
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    • 제16권5호
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    • pp.43-48
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    • 2022
  • 최근 러시아가 우크라이나에 발사한 킨잘 미사일은 실전에서 최초로 사용된 극초음속 순항미사일 마하 5이상의 빠른 속력으로 비행한다. 빠른 속력은 강력한 파괴력으로 이어지며, 방어체계의 요격가능시간을 극단적으로 단축시킨다. 따라서 극초음속 미사일은 다층화된 방어체계가 구축된 미국조차도 요격에 어려움을 인정하고 있는 게임체인저가 될 수 있다. 미국, 러시아, 중국 및 북한 등 군사강국 들은 공격무기인 극초음속 미사일 개발에 집중하고 있으나 방어체계 능력은 부족한 실정이다. 이러한 관점에서 본 논문은 주요국의 극초음속 미사일 개발현황과 방어체계 능력을 식별하고 이를 기반으로 우리 군의 대응방안을 모색하고자 한다.

복합 휴리스틱 알고리즘을 이용한 지대공 유도무기 최적배치 모형 : 항공기 방어를 중심으로 (The Optimal Allocation Model for SAM Using Multi-Heuristic Algorithm : Focused on Aircraft Defense)

  • 곽기훈;이재영;정치영
    • 한국경영과학회지
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    • 제34권4호
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    • pp.43-56
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    • 2009
  • In korean peninsular, aircraft defense with SAM (Surface-to-Air Missile) is very important because of short range of combat space in depth. Effective and successful defense operation largely depends on two factors, SAM's location and the number of SAM for each target based on missile's availability in each SAM's location. However, most previous papers have handled only the former. In this paper, we developed Set covering model which can handle both factors simultaneously and Multi-heuristic algorithm for solving allocation problem of the batteries and missile assignment problem in each battery. Genetic algorithm is used to decide optimal location of the batteries. To determine the number of SAM, a heuristic algorithm is applied for solving missile assignment problem. If the proposed model is applied to allocation of SAM, it will improve the effectiveness of air defense operations.

완성 유도탄 탑재장비의 소프트웨어 업그레이드를 위한 MIL-STD-1553B 기반 간접적 데이터 전송 기술 (An Indirect Data Transfer Technique based on MIL-STD-1553B for the Software Upgrade of Embedded Equipments on a Missile Assembly with Booster)

  • 김기표;유해성;이헌철;윤석재;안기현;우덕영
    • 한국군사과학기술학회지
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    • 제19권1호
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    • pp.43-49
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    • 2016
  • This paper addresses the problem of the software update or upgrade of embedded equipments on a missile assembly with booster. Because the embedded equipments are assembled delicately and closely one another with various communication and power cables, they should be very carefully disassembled to directly upgrade the software of a certain embedded equipment. This may cause not only the costs for disassembly and reassembly but also additional tests to verify the completeness of the reassembled missile as a missile assembly with booster. This paper presents an indirect data transfer technique based on MIL-STD-1553B through Guidance Control Unit to easily upgrade the software of other equipments without any additional costs caused by disassembly and reassembly. The presented technique was successfully applied to the software upgrade of various equipments on real missile assembly with booster.