• Title/Summary/Keyword: 근접 교전

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Design of an Autonomous Air Combat Guidance Law using a Virtual Pursuit Point for UCAV (무인전투기를 위한 가상 추적점 기반 자율 공중 교전 유도 법칙 설계)

  • You, Dong-Il;Shim, Hyunchul
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.3
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    • pp.199-212
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    • 2014
  • This paper describes an autonomous air combat guidance law using a Virtual Pursuit Point (VPP) in one-on-one close engagement for Unmanned Combat Aerial Vehicle (UCAV). The VPPs that consist of virtual lag and lead points are introduced to carry out tactical combat maneuvers. The VPPs are generated based on fighter's aerodynamic performance and Basic Fighter Maneuver (BFM)'s turn circle, total energy and weapon characteristics. The UCAV determines a single VPP and executes pursuit maneuvers based on a smoothing function which evaluates probabilities of the pursuit types for switching maneuvers with given combat states. The proposed law is demonstrated by high-fidelity real-time combat simulation using commercial fighter model and X-Plane simulator.

Optimal Weapon-Target Assignment Algorithm for Closed-In Weapon Systems Considering Variable Burst Time (가변 연속사격 시간을 고려한 근접 방어 시스템의 최적 무장 할당 알고리듬)

  • Kim, Bosoek;Lee, Chang-Hun;Tahk, Min-Jea;Kim, Da-Sol;Kim, Sang-Hyun;Lee, Hyun-Seok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.5
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    • pp.365-372
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    • 2021
  • This paper deals with an optimal Weapon-Target Assignment (WTA) algorithm for Closed-In Weapon Systems (CIWS), considering variable burst time. In this study, the WTA problem for CIWS is formulated based on Mixed Integer Linear Programming (MILP). Unlike the previous study assuming that the burst time is fixed regardless of the engagement range, the proposed method utilizes the variable burst time based on the kill probability according to the engagement range. Thus, the proposed method can reflect a more realistic engagement situation and reduce the reaction time of CIWS against targets, compared to the existing method. In this paper, we first reformulate the existing MILP-based WTA problem to accommodate the variable burst Time. The proposed method is then validated through numerical simulations with the help of a commercial optimization tool.

A Position of a Anti-Air Weapon System for Fighting Ship's Self-Defence Effectiveness Enhancement (대공방어무기체계의 교전 효과도 향상을 위한 함상 배치 위치 분석)

  • Hwang, Soo-Jin
    • Journal of the Korea Institute of Military Science and Technology
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    • v.9 no.3
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    • pp.41-47
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    • 2006
  • Naval combat system is total management system integrating a ship and several weapon system functions. For the mission of a ship, naval combat system manages features and constraints of each weapon system. Proper treats of each weapon system's conditions guarantee effective performances of naval combat system. In this paper, the relationship of anti-air weapon system's on board position and self-defence effectiveness against anti-surface missiles is studied

The Study on Consistency of Simulation Logic about Close Combat Damage Assessment among Constructive Models : Based on Combined Arms Integrated Interoperability System (워게임모델간 근접전투 피해평가 모의논리 일치에 관한 연구 : 제병협동통합연동체계를 중심으로)

  • Moon, Ho-Seok;Kim, Hyung-Se;Hwang, Myung-Sang;Bae, Hyun-Wung;Lee, Dong-Keun
    • Journal of the military operations research society of Korea
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    • v.37 no.1
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    • pp.87-97
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    • 2011
  • In this paper, we propose a new close combat expert system to overcome the difference of combat damage assessments between combat units belong to their own model in Combined Arms Integrated Interoperability System(CAIIS) which will be deployed in the early future. When it happens to engage in a battle among combat units belong to their own model in CAIIS, the result of damage assessment is different severely. This is related to CAIIS's confidence and need to be overcome. We propose the expert system for close combat damage assessment with a decision tree. Simulation results show that the proposed expert system is valid well. Because the proposed expert system is made not as an independent system but as an inner module type of CAIIS, CAIIS will be simpler system than we expect. And we will hope to reduce the cost of CAIIS.

A Study on Securing Ship Survivability focused on a Cost and Effectiveness Analysis for Air Defense Performance (대공방어성능에 대한 비용효과분석을 중심으로 한 함정생존성 확보방안 연구)

  • Choi, Sung-Lin;Park, Dong-Ki
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.15 no.5
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    • pp.2579-2586
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    • 2014
  • It is crucial to set up early the required performance of surface ship for preventing the risk factors such as an excess of performance, cost and period in development stage. In this study, MOP and MOE are proposed to establish the method for deriving alternatives, MOP represents the defensive effect for anti ship missiles and MOE is the ratio of cost and performance. The 16 engagement scenarios which selectively install RF decoy, RF jammer, CIWS and anti air missile are suggested. The simulation results by using NORAM tool operated by ROK Navy show that the ship survivability is 0.605~0.975 and MOP is 0.301~0.887. The analyzed results represent the operating scenario with RF decoy, RF jammer and short range anti air missile is the best cost and effectiveness measure.

Defense Strategy against Multiple Anti-Ship Missiles using Anti-Air Missiles (다수 대함유도탄에 대한 함정의 대공방어유도탄 운용기법 연구)

  • Kim, Do-Wan;Yun, Joong-Sup;Ryoo, Chang-Kyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.4
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    • pp.354-361
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    • 2011
  • In this paper, an efficient defense strategy of single naval ship using short range anti-air missiles against the threat of multiple anti-ship missiles is suggested. The defense logic is based on the estimated future trajectory of anti-ship missiles by using current radar information. The logic is designed to maximize the range of interception of anti-ship missiles so that the chance of interception can be increased although the prior tries turn out to be fail. Basically, the decision making for the allocation of a defense missile is achieved by comparing the total kill probability and the estimated intercepting point. Performance of the proposed logic is investigated by nonlinear planar numerical simulations.