• 제목/요약/키워드: Missile Allocation Problem

검색결과 12건 처리시간 0.024초

격추확률 최대화를 위한 미사일 최적배치 문제 (An Optimal Missile Allocation Problem for Maximizing Kill Probability)

  • 정치영;이재영;이상헌
    • 경영과학
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    • 제27권1호
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    • pp.75-90
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    • 2010
  • In this paper, we proposed new solution procedure of the air defense missile allocation problem. In order to find the optimal location of missile, we formulated a simple mathematical model maximizing the kill probability of enemy air threat including aircraft and missile. To find the Kill probability, we developed a new procedure using actual experimental data in the mathematical model. Actual experimental data mean real characteristic factor, which was acquired when the missile had been developed through missile fire experiment. The result of this study can offer practical solution for missile allocation and the methodology in this study can be used to the decision making for the optimal military facility allocation.

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
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    • 제21권3호
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    • pp.262-273
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    • 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.

요격미사일 배치문제에 대한 하이브리드 유전알고리듬 적용방법 연구 (An Application of a Hybrid Genetic Algorithm on Missile Interceptor Allocation Problem)

  • 한현진
    • 한국국방경영분석학회지
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    • 제35권3호
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    • pp.47-59
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    • 2009
  • A hybrid Genetic Algorithm is applied to military resource allocation problem. Since military uses many resources in order to maximize its ability, optimization technique has been widely used for analysing resource allocation problem. However, most of the military resource allocation problems are too complicate to solve through the traditional operations research solution tools. Recent innovation in computer technology from the academy makes it possible to apply heuristic approach such as Genetic Algorithm(GA), Simulated Annealing(SA) and Tabu Search(TS) to combinatorial problems which were not addressed by previous operations research tools. In this study, a hybrid Genetic Algorithm which reinforces GA by applying local search algorithm is introduced in order to address military optimization problem. The computational result of hybrid Genetic Algorithm on Missile Interceptor Allocation problem demonstrates its efficiency by comparing its result with that of a simple Genetic Algorithm.

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.

단거리 지대공 미사일의 최적배치에 관한 연구 (A Study on Optimal Allocation of Short Surface-to-Air Missile)

  • 이영해;남상억
    • 한국국방경영분석학회지
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    • 제26권1호
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    • pp.34-46
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    • 2000
  • The object of this study is to construct a model for an optimal allocation of short surface to air missile defending our targets most efficiently from hostile aircraft´s attack. For the purpose of this, we analyze and establish facility allocation concept of existing models, apply set covering theory appropriate to problem´s properties, present the process of calculating the probability of target being protected, apply Sherali-Kim´s branching variable selection strategy, and then construct the model. As constructed model apply the reducing problem with application, we confirm that we can apply the large scale, real problem.

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탄도미사일 방어무기체계 배치모형 연구 (Optimal Allocation Model for Ballistic Missile Defense System by Simulated Annealing Algorithm)

  • 이상헌
    • 한국경영과학회:학술대회논문집
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    • 한국경영과학회/대한산업공학회 2005년도 춘계공동학술대회 발표논문
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    • pp.1020-1025
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    • 2005
  • The set covering(SC) problem has many practical application of modeling not only real world problems in civilian but also in military. In this paper we study optimal allocation model for maximizing utility of consolidating old fashioned and new air defense weapon system like Patriot missile and develop the new computational algorithm for the SC problem by using simulated annealing(SA) algorithm. This study examines three different methods: 1) simulated annealing(SA); 2) accelerated simulated annealing(ASA); and 3) selection by effectiveness degree(SED) with SA. The SED is adopted as an enhanced SA algorithm that the neighboring solutions could be generated only in possible optimal feasible region at the PERTURB function. Furthermore, we perform various experiments for both a reduced and an extended scale sized situations depending on the number of customers(protective objective), service(air defense), facilities(air defense artillery), threat, candidate locations, and azimuth angles of Patriot missile. Our experiment shows that the SED obtains the best results than others.

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미사일 방어를 위한 KDX 최적배치모형 연구 (Optimal Allocation Model of KDX for Missile Defense)

  • 이상헌;정인철
    • 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.

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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
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    • 제18권6호
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    • pp.797-807
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    • 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.

혼합정수계획법을 이용한 요격미사일의 할당 및 교전 일정계획에 관한 연구 (A Study on the Allocation and Engagement Scheduling of Air Defense Missiles by Using Mixed Integer Programming)

  • 이대력;양재환
    • 경영과학
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    • 제32권4호
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    • pp.109-133
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    • 2015
  • This paper considers the allocation and engagement scheduling of air defense missiles by using MIP (mixed integer programming). Specifically, it focuses on developing a realistic MIP model for a real battle situation where multiple enemy missiles are headed toward valuable defended assets and there exist multiple air defense missiles to counteract the threats. In addition to the conventional objective such as the minimization of surviving target value, the maximization of total intercept altitude is introduced as a new objective. The intercept altitude of incoming missiles is important in order to minimize damages from debris of the intercepted missiles and moreover it can be critical if the enemy warhead contains an atomic or chemical bomb. The concept of so called the time window is used to model the engagement situation and a continuous time is assumed for flying times of the both missiles. Lastly, the model is extended to simulate the situation where the guidance radar, which guides a defense missile to its target, has the maximum guidance capacity. The initial mathematical model developed contains several non-linear constraints and a non-linear objective function. Hence, the linearization of those terms is performed before it is solved by a commercially available software. Then to thoroughly examine the MIP model, the model is empirically evaluated with several test problems. Specifically, the models with different objective functions are compared and several battle scenarios are generated to evaluate performance of the models including the extended one. The results indicate that the new model consistently presents better and more realistic results than the compared models.

효율적인 유전 알고리즘을 활용한 요격미사일 할당 및 교전 일정계획의 최적화 (An Efficient Genetic Algorithm for the Allocation and Engagement Scheduling of Interceptor Missiles)

  • 이대력;양재환
    • 산업경영시스템학회지
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    • 제39권2호
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    • pp.88-102
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    • 2016
  • This paper considers the allocation and engagement scheduling problem of interceptor missiles, and the problem was formulated by using MIP (mixed integer programming) in the previous research. The objective of the model is the maximization of total intercept altitude instead of the more conventional objective such as the minimization of surviving target value. The concept of the time window was used to model the engagement situation and a continuous time is assumed for flying times of the both missiles. The MIP formulation of the problem is very complex due to the complexity of the real problem itself. Hence, the finding of an efficient optimal solution procedure seems to be difficult. In this paper, an efficient genetic algorithm is developed by improving a general genetic algorithm. The improvement is achieved by carefully analyzing the structure of the formulation. Specifically, the new algorithm includes an enhanced repair process and a crossover operation which utilizes the idea of the PSO (particle swarm optimization). Then, the algorithm is throughly tested on 50 randomly generated engagement scenarios, and its performance is compared with that of a commercial package and a more general genetic algorithm, respectively. The results indicate that the new algorithm consistently performs better than a general genetic algorithm. Also, the new algorithm generates much better results than those by the commercial package on several test cases when the execution time of the commercial package is limited to 8,000 seconds, which is about two hours and 13 minutes. Moreover, it obtains a solution within 0.13~33.34 seconds depending on the size of scenarios.