• 제목/요약/키워드: Battlefield Analysis

검색결과 109건 처리시간 0.027초

헬리콥터 블레이드 공력 소음 해석 기법 연구 (THE INVESTIGATION OF THE AERO-ACOUSTIC ANALYSIS METHODS FOR THE HELICOPTER BLADE)

  • 박남은;우철훈;이상기;이석준
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 학술대회
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    • pp.302-307
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    • 2008
  • The development technology for the helicopter is improved by the increasing of computing power and advanced test facilities. The increasing efficiency of fuel consuming by the developing of improved lift-to-drag rotor system is the major issue, the noise reduction for ecology(civil area) and increase of survivability to reduce noise detection(battlefield) also are important. This investigation shows the classification of helicopter external noise and requirements, the noise flight test methods, the numerical modeling method for aero-acoustic of rotor blade and the result of CAA(Computational Aero-Acoustic) for main rotor blade.

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헬리콥터 블레이드 공력 소음 해석 기법 연구 (THE INVESTIGATION OF THE AERO-ACOUSTIC ANALYSIS METHODS FOR THE HELICOPTER BLADE)

  • 박남은;우철훈;이상기;이석준
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년 추계학술대회논문집
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    • pp.302-307
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    • 2008
  • The development technology for the helicopter is improved by the increasing of computing power and advanced test facilities. The increasing efficiency of fuel consuming by the developing of improved lift-to-drag rotor system is the major issue, the noise reduction for ecology(civil area) and increase of survivability to reduce noise detection(battlefield) also are important. This investigation shows the classification of helicopter external noise and requirements, the noise flight test methods, the numerical modeling method for aero-acoustic of rotor blade and the result of CAA(Computational Aero-Acoustic) for main rotor blade.

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C4I Maintenance Priority Decision using Maintenance Metric

  • Kim, Kiwang;Kang, Dongsu
    • 한국컴퓨터정보학회논문지
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    • 제22권12호
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    • pp.145-153
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    • 2017
  • Systemic management is required at each phase of the C4I system life cycle to achieve information advantage in the battlefield through stable operation of the C4I system under the NCOE. In particular, the maintenance phase is the longest period of the C4I system life cycle, and it is easy to utilize and analyze data such as faults that occur during system operation. However, according to the previous research, the maintenance is evaluated as a phase in which the definition and management of comprehensive indicators are insufficient compared to other phase. In this paper, we propose the method of C4I Maintenance Priority decision using Maintenance metric. As a result of modifying the Naval Tactical C4I System's preventive maintenance cycle according to the priority, the total number of faults is reduced and the maintenance efficiency is improved.

ANN-based Evaluation Model of Combat Situation to predict the Progress of Simulated Combat Training

  • Yoon, Soungwoong;Lee, Sang-Hoon
    • 한국컴퓨터정보학회논문지
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    • 제22권7호
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    • pp.31-37
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    • 2017
  • There are lots of combined battlefield elements which complete the war. It looks problematic when collecting and analyzing these elements and then predicting the situation of war. Commander's experience and military power assessment have widely been used to come up with these problems, then simulated combat training program recently supplements the war-game models through recording real-time simulated combat data. Nevertheless, there are challenges to assess winning factors of combat. In this paper, we characterize the combat element (ce) by clustering simulated combat data, and then suggest multi-layered artificial neural network (ANN) model, which can comprehend non-linear, cross-connected effects among ces to assess mission completion degree (MCD). Through our ANN model, we have the chance of analyzing and predicting winning factors. Experimental results show that our ANN model can explain MCDs through networking ces which overperform multiple linear regression model. Moreover, sensitivity analysis of ces will be the basis of predicting combat situation.

시스템공학 도구를 이용한 KAFASAT 개념설계 (Conceptual Design of the KAFASAT Using System Engineering Tools)

  • 이기훈;김종범;정명진;엄윤종;조동현;권기범
    • 항공우주시스템공학회지
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    • 제8권1호
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    • pp.36-41
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    • 2014
  • KAFASAT is a CubeSat which has a high level mission of testing the possibility of establishing the LEO satellite constellation providing the role of communication nodes and quasi-realtime image recognition of battlefield in accordance with the aspect of future-war-environment. The high level mission is developed using the Pugh selection method, which is one of system engineering tools. In order to accomplish the high level mission objectives and deduce engineering level requirements, system engineering tools such as Analytic Hierarchy Process and Quality Function Deployment are used. The subsystem synthesis in the context of system engineering process is done using a developed integrated design environment. The paper also includes the conceptual design results of the KAFASAT, which can be used as a baseline for upcoming preliminary design.

시뮬레이션을 이용한 전투효과기반 공격헬기 소요 분석방안 (Combat Effectiveness Based Analysis Methodology for Optimal Requirement of Attack Helicopter Using Simulation)

  • 정치영;이재영
    • 한국군사과학기술학회지
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    • 제13권6호
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    • pp.1099-1105
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    • 2010
  • The purpose of this paper is to propose a methodology that can estimate optimal requirement of attack helicopter Korea army will be operating in future. For estimating optimal requirement, attack helicopter's operation concept, performance, battlefield environment and enemy threat are considered. We use a wargame model, AAsim(Army Aviation simulation), as a analytic simulation model which is used to analyze DOTMLPF and operation in army aviation field. In this paper, we conduct battle experiment for anti armored corps operation which reflects attack helicopter's combat effectiveness very well. As a result of simulation, the destructive rate for enemy armored corps per each attack helicopter can be calculated. In this paper, we propose optimal requirement of attack helicopter using that destructive rate for enemy armored corps.

AHP & 모수추정법을 이용한 차기 다련장로켓의 비용대 효과분석 (A Study on the Analysis of the Cost-Effectiveness for the New Generation Multiple Launcher Rocket System Using AHP & Parametric Estimating)

  • 조기홍
    • 한국군사과학기술학회지
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    • 제13권1호
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    • pp.84-90
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    • 2010
  • Korean army currently considers the development of the new generation MLRS(Multiple Launcher Rocket System) as a new alternative, which responses on the renovation of the artillery and future battlefield environment. This study suggests that it presents cost-effectiveness of MLRS based on the Analytic Hierarchy Process and Parametric Estimating(PRICE H). According to this study, the cost-effectiveness of new generation MLRS presented that alternative A is 2.30 times and alternative B is 1.70 times, which are better than currently operating M270A1. Therefore, The best acquisition is alternative A that launcher is carried on currently operating 10ton standard truck but final acquisition alternative should be politically decided to consider viability of operator, performance and the latest of equipment.

전쟁패러다임의 전환과 군사변혁 (Shift in Warfare Paradigm and Military Transformation)

  • 정춘일
    • 안보군사학연구
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    • 통권4호
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    • pp.381-418
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    • 2006
  • In present, advanced countries in the world are seen concentring on Military Transformation to create new military capability as there is a shift in Warfare Paradigm. Rapid development of technology enables military system, operational concept and organization innovated. As a result, Revolution in Military Affairs(RMA) that dramatically increased warfighting capability is pursued. Especially, advanced information technology constructs system of systems with abilities of battle visualization, information sharing in battlefield, long-range strike capability that are interoperable and combined. Corresponding to this, engagement methods and organizations are being progressively developed. The purpose of this thesis is overview of newly developing Warfare Paradigm and analysis of tendency of Military Transformation that advanced countries are pursuing preparation to this. Above all, specific aspects and contents of the Warfare Paradigm which emerged by information age were summarized. Subsequently, Military Transformation which provides the basic concepts and principles to the advanced countries in the world for the creation of new military capability was discussed. In conclusion, the tendency of Military Transformation by U.S.A, Japan, China, and Russia surround the Korean peninsular as the major power in military was carefully observed.

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전투창 화면 디스플레이를 중심으로 본 모바일 RPG 게임의 사용자 인터페이스의 특징과 인터페이스 만족도 평가 (Analysis of User Interface and Usability Evaluation for Mobile RPG Games based on Battlefield Display)

  • 김진수;이준형;송두헌
    • 한국정보통신학회:학술대회논문집
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    • 한국정보통신학회 2017년도 추계학술대회
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    • pp.433-436
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    • 2017
  • 조작해야 할 정보와 사물이 가장 많은 게임 장르인 RPG 장르에서 모바일 환경의 제약은 자연스럽게 사용자 인터페이스 패턴의 제약으로 연결된다. 다만 기기 환경도 스마트폰 디스플레이 화면이 예전보다 커지고 자동 전투 기능의 활용으로 조작의 대상과 적시성을 감소시키면서 최근에는 그 제약이 개선되었다는 평가가 있다. 이 논문에서 우리는 지난 3년간 연도별로 가장 많이 플레이 된 모바일 RPG 게임 5개씩을 골라 주요 구성 요소의 전투 창에서의 배치 패턴을 분석하고 그러한 패턴이 실제로 사용자들에게 어떻게 인식되고 있는지 조작 편의성을 중심으로 만족도 평가를 실시하였다. 4점 척도로 적극적 평가를 요구한 9개의 설문에서 이 장르 사용자들은 대체로 70% 이상의 만족도를 보이고 있었으며 일부 설문에서만 게임 간 차이가 발견되었다.

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The Design of Integrated Flying Vehicle Model for Engagement Analyses of Missiles

  • Ha, Sue Hyung
    • 한국멀티미디어학회논문지
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    • 제22권8호
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    • pp.930-939
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    • 2019
  • High-Level Architecture(HLA)/Run-Time Infrastructure(RTI) are standards for distributed simulation systems and offer a technology to interconnect them and form one single simulation system. In defense domain, M&S is the only way to prove effectiveness of weapon systems except for Live Fire Testing (LFT). This paper focuses on guided missile simulations in weapon systems for engagement analyses and proposes the integrated flying vehicle model that is based on HLA/RTI. There are a lot of missiles in real world; therefore, we should develop each missile models in M&S in order to apply battlefield scenarios. To deal with the difficulties, in this paper, firstly, I classify these missiles into three models: ballastic, cruise, and surface-to-air missile models, and then I design each missile model and integrates them into a single model. This paper also offers a case study with my integrated flying vehicle model. At the conclusion, this paper presents contributions of this paper.