• 제목/요약/키워드: Air and Missile Defense

검색결과 91건 처리시간 0.027초

유전자 알고리즘을 이용한 한국형 미사일 방어체계 최적 배치에 관한 연구 (A Study on the Optimal Allocation of Korea Air and Missile Defense System using a Genetic Algorithm)

  • 윤승환;김수환
    • 한국군사과학기술학회지
    • /
    • 제18권6호
    • /
    • pp.797-807
    • /
    • 2015
  • The low-altitude PAC-2 Patriot missile system is the backbone of ROK air defense for intercepting enemy aircraft. Currently there is no missile interceptor which can defend against the relatively high velocity ballistic missile from North Korea which may carry nuclear, biological or chemical warheads. For ballistic missile defense, Korea's air defense systems are being evaluated. In attempting to intercept ballistic missiles at high altitude the most effective means is through a multi-layered missile defense system. The missile defense problem has been studied considering a single interception system or any additional capability. In this study, we seek to establish a mathematical model that's available for multi-layered missile defense and minimize total interception fail probability and proposes a solution based on genetic algorithms. We perform computational tests to evaluate the relative speed and solution of our GA algorithm in comparison with the commercial optimization tool GAMS.

3-D Optimal Evasion of Air-to-Surface Missiles against Proportionally Navigated Defense Missiles

  • Cho, Sung-Bong;Ryoo, Chang-Kyung;Tahk, Min-Jea
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2003년도 ICCAS
    • /
    • pp.514-518
    • /
    • 2003
  • In this paper, we investigate three dimensional optimal evasive maneuver patterns for air-to-surface attack missiles against proportionally navigated anti-air defense missiles. Interception error of the defense missile can be generated by evasive maneuver of the attack missile during the time of flight for which the defense missile intercepts the attack missile. Time varying weighted sum of the inverse of these interception errors forms a performance index to be minimized. Direct parameter optimization technique using CFSQP is adopted to get the attack missile's optimal evasive maneuver patterns according to parameter changes of both the attack missile and the defense missile such as maneuver limit and time constant of autopilot approximated by the 1st order lag system. The overall shape of resultant optimal evasive maneuver to enhance the survivability of air-to-surface missiles against proportionally navigated anti-air missiles is a kind of deformed barrel roll.

  • PDF

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
    • /
    • 제18권3호
    • /
    • pp.260-266
    • /
    • 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.

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

  • 김재권;설현주
    • 산업경영시스템학회지
    • /
    • 제39권1호
    • /
    • pp.98-104
    • /
    • 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.

복합-휴리스틱 알고리즘을 이용한 지대공 유도무기(SAM) 최적배치 방안 : 탄도미사일 방어를 중심으로 (The Optimal Allocation Model for SAM Using Multi-Heuristic Algorithm : Focused on Theater Ballistic Missile Defense)

  • 이재영;곽기훈
    • 산업공학
    • /
    • 제21권3호
    • /
    • pp.262-273
    • /
    • 2008
  • In Korean peninsular, Air Defense with SAM(Surface-to-Air Missile) is very important, because of threatening by North Korea's theater ballistic missiles installed with nuclear or biochemistry. 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 Multi-heuristic algorithm which can handle both factors simultaneously for solving allocation problem of the batteries and missile assignment problem in each battery. To solve allocation problem, genetic algorithm is used to decide location of the batteries. To solve missile assignment problem, a heuristic algorithm is applied to determine the number of SAM for each target. If the proposed model is applied to allocation of SAM, it will improve the effectiveness of missile defense operations.

미 해군의 이지스 탄도미사일 방어 (The U.S. Navy Aegis Ballistic Missile Defense)

  • 박태용
    • 한국정보통신학회:학술대회논문집
    • /
    • 한국정보통신학회 2015년도 춘계학술대회
    • /
    • pp.359-362
    • /
    • 2015
  • 미국은 러시아, 중국, 북한 등 주변국으로부터 탄도미사일의 위협이 증가함에 따라 미사일 방어체계를 구축하고 있다. 미국의 탄도미사일 방어체계는 미사일방어국(MDA, Missile Defense Agency)을 중심으로 통합 대공 및 미사일 방어(IAMD, Integrated Air and Missile Defense) 개념으로 이루어지며, 해군은 탄도미사일을 해상에서 탐지, 추적 및 요격하는 임무를 담당하고 있다. 본 논문에서는 미 해군의 이지스 탄도미사일 방어(Aegis Ballistic Missile Defense)의 개념과 구축 현황 및 계획을 조사하여 기술하였다.

  • PDF

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
    • /
    • 제34권4호
    • /
    • pp.43-56
    • /
    • 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.

함대공 방어체계 복합자산 운용개념 연구 (A Study on Operation Concept of Naval Surface to Air Defense System with Complex Assets)

  • 김태구;나웅재;양서연;박여진;심동혁;류다빈;윤나혜;박인철;김래은
    • 산업경영시스템학회지
    • /
    • 제46권4호
    • /
    • pp.190-198
    • /
    • 2023
  • The purpose of this study was to propose an operational concept for a ship in a fleet equipped with an interceptor missile system, a naval surface to air defense system, and to develop a simulation program that reflects it. The results of the defense activities of other ships in the fleet can be reflected by receiving information about the status of the enemy missiles. The allocation of defensive assets is based on the survival probability of the ship, not on the destruction of enemy attacks, which can be obtained as the product of the expected survival probability for each enemy missile. In addition, the concept of predicted survivability was introduced to assess the loss of future defense opportunities that would result from assigning a new command. A simulation program was also developed as a tool for realizing the proposed concept of operations, which generated cases.

대함유도탄 요격 확률을 고려한 함정 대공방어유도탄의 최적 운용 연구 (A Study on Optimal Operation against Anti-Air Missiles with Consideration of Anti-Surface Missile Kill Probability)

  • 박현우;이한민
    • 한국군사과학기술학회지
    • /
    • 제22권6호
    • /
    • pp.815-823
    • /
    • 2019
  • A naval surface-to-air missile is an effective countermeasure against increasing threats of anti-ship missiles. Optimal operation is imperative for high survivability due to limited defense resources of a warship. This paper addresses a problem of optimal engagement to maximize the overall probability of intercept under Shoot-Look-Shoot tactics. The problem is formulated and analyzed with consideration of a realistic single-shoot probability model. The analysis shows that a global solution is achieved for some engagement scenarios. A numerical algorithm to optimize the overall probability of intercept is suggested. An illustrative example is provided to verify our results.

A Comparison of Guided Missile Simulations Between EADSIM and SADM in Composite Combat Mission Planning Simulation Environments

  • Kim, Jingyu
    • 한국멀티미디어학회논문지
    • /
    • 제23권8호
    • /
    • pp.1066-1074
    • /
    • 2020
  • High Level Architecture/Run-Time Infrastructure (HLA/RTI) is used to connect individual simulators on networks in order to interoperate heterogeneous simulators. In defense domain, Ship Air Defense Model (SADM) and Extended Air Defense Simulation (EADSIM) are two of most advanced simulation tools. To interoperate these SADM and EADSIM, this paper attempts to use HLA/RTI that helps to support a Composite Combat Mission Planning Simulation Environment (CCMPSE). The CCMPSE allows us to analyze a group of simulations for comprehensive and accurate experiments. For the first time, this paper analyzes guided missile simulations in EADSIM and SADM by comparing related simulation models in their parameters and considerations. It presents characteristics of these models in view of guided missile simulation perspectives. For the contributions of this paper, it provides insights to select guided missiles between SADM and EADSIM on the CCMPSE according to specific simulation purposes.