• 제목/요약/키워드: Attack Helicopter

검색결과 25건 처리시간 0.024초

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.

A Study on the Tank-Attack Helicopter Duel

  • 최석철
    • 한국국방경영분석학회지
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    • 제23권1호
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    • pp.25-46
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    • 1997
  • In this paper, we consider a tow-person zero-sum game in which an attack helicopter with a missile wishes to destroy a tank. The tank has much small-caliber ammunition for protection itself from the attack helicopter. And the attack helicopter possesses a missile for attacking the tank. We develop models for the behavior of the attack helicopter, in terms of missile launch time, and of the tank, in terms of ammunition firing rate, in several situations. In particular, we examine the Weiss-Gillman model.

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QFD를 이용한 미래 공격헬기의 핵심기능 도출 (Derivation of Critical Functions of the Future Attack Helicopter Using QFD)

  • 이재원;권용수;고남경
    • 한국군사과학기술학회지
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    • 제16권3호
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    • pp.348-357
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    • 2013
  • This work describes an approach that contributes to derive from mission to critical functions of the attack helicopter under future battle space environment. An existing mission of the attack helicopter is limited to the only shooter oriented functions. In the future environment, mission and its functions of the helicopter might be much expanded. The functions should be derived by the top down approach based on systems engineering approach. In this point of view, this work describes network based future battle environment. From this environment, the missions of the attack helicopter are identified and optimized functions are derived through sequential procedures like from missions to tasks, tasks to activities, and activities to functions. The selected activities are obtained from the tasks using QFD. The weighting scores of the QFD are calculated by the AHP computational procedure. Finally the critical functions are presented through the similar procedure.

시뮬레이션 및 AHP기법을 이용한 공격헬기 전투효과 분석 (The Combat Effectiveness Analysis of Attack Helicopter Using Simulation and AHP)

  • 이재문;정치영;이재영
    • 한국시뮬레이션학회논문지
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    • 제19권3호
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    • pp.63-70
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    • 2010
  • 본 연구의 목적은 미래 한국 육군이 운영할 공격헬기의 전투효과를 산출하는 방법론을 제시하는 것이다. 본 연구에서 적용한 전투 효과 산출방법은 첫째, 육군항공분야의 작전계획과 전투발전 분야별 요소인 DOTMLPF 분석에 활용되는 분석용 워게임 모델인 육군항공분석모델을 사용하였으며, 둘째, 전문가 의견을 기반으로 한 AHP기법을 사용하였다. 이 때, 시뮬레이션 및 AHP 기법 적용시 공격헬기의 전투효과를 가장 잘 반영할 수 있는 대 기갑작전을 고려하였다. 연구결과, 공격헬기의 기종별 전투효과를 산출할 수 있었으며, 이러한 전투효과도는 신규 무기체계 획득시 기종선정이나 수량결정과 같은 의사결정시 의사결정자가 합리적으로 의사결정을 할 수 있게 하는 데 유용할 것으로 판단된다.

헬리콥터 로터 블레이드의 자려소음 예측 (Self-Noise Prediction from Helicopter Rotor Blade)

  • 김효영;유기완
    • 항공우주시스템공학회지
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    • 제1권1호
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    • pp.73-78
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    • 2007
  • Self-noise from the rotor blade of the UH-1H Helicopter is obtained numerically by using the Brooks' empirical noise model. All of the five noise sources are compared with each other in frequency domain. From the calculated results the bluntness noise reveals dominant noise sources at small angel of attack, whereas the separation noise shows main noise term with gradually increasing angel of attack. From the results of two different tip Mach numbers with the change of angel of attack, the OASPLs at M = 0.8 show about 15dB larger than those at M = 0.4.

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헬기 운용환경을 고려한 가상 사격 통제 시스템 개발 (The Development of Virtual Fire Control System Considering Operational Environment of Helicopter)

  • 김우식;이동호;장인동;박한준
    • 한국군사과학기술학회지
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    • 제17권4호
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    • pp.448-455
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    • 2014
  • Virtual Fire Control System(VFCS) in attack helicopter is developed. VFCS is comprised of multifunction display, store management computer, mission computer, target acquisition and designation system, mission planning system, weapon simulator and flight simulator. Weapon engagement process under the operational environment of helicopter was considered by using the VFCS. We considered hellfire missile, tow missile, unguided rocket and turret gun. The results of this study will be utilized efficiently on integrated fire control system SIL(System Integration Lab.) in attack helicopter.

Performance Comparison of Two Airfoil Rotor Designs for an Agricultural Unmanned Helicopter

  • Koo, Young-Mo
    • Journal of Biosystems Engineering
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    • 제37권1호
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    • pp.1-10
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    • 2012
  • Purpose: The most important element of an agricultural helicopter is the rotor blade realizing lift force. In order to improve the performance of the rotor blades, two types (KA152313 and KB203611) of airfoils were designed and compared. Methods: The nose shape of the KB203611 airfoil was 'drooped' and 'sharp' compared to the leading edge of the KA152313 airfoil. The performance of the experimental airfoils was simulated using CFD-ACE program, and lifts were measured in situ using the 'AgroHeli-4G', a prototype helicopter. Results: Simulated lifts of the blade with the KA152313 airfoil showed proper values for a wide range of angles of attack between $14^{\circ}{\sim}18^{\circ}$, while the simulated lift of the KB203611 blade exhibited maximum values near $13^{\circ}{\sim}14^{\circ}$. In the lift measurements, the range of operable angles of attack was a collective pitch angle at the grip (GP) of $12^{\circ}{\sim}18^{\circ}$ for the KA152313 blade. On the other hand, the range of angles of attack for the KB203611 blade was a GP of $12^{\circ}{\sim}14^{\circ}$. Conclusions: The blade of KA152313 performed well over a wide range of AoAs and the blade of KB203611 performed better at low AoAs. In this study, a variative airfoil blade, gradually emerging from grip to tip using the two different airfoils, was suggested.

헬기에 의한 산불공중진화 효과 및 안전성 인식 연구 (A Study on the Recognition of Effectiveness and Safety of the Helicopter Aerial Fire Attack)

  • 배택훈;이시영
    • 한국화재소방학회논문지
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    • 제26권2호
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    • pp.97-104
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    • 2012
  • 본 연구에서는 산불이 발생하면 대형화 위험성이 증대하여 항공기 특히, 헬기의 산불진화 활용성이 점차 증가되고 있는 관점에서, 산불진화 과정 중 헬기에 의한 공중진화기술과 안전성 향상은 효율적인 산불진화의 성공요인으로서 매우 중요하다. 따라서 우리나라 산불전문기관인 산림청 산림항공본부의 조종사들에 대하여 산불현장에서 실제 경험한 내용을 토대로 설문조사를 실시하여 효율적인 공중진화기술 및 안전성 향상 방안을 제시하였다.

헬기에 의한 산불공중간접진화 방법에 관한 연구 (Study of Indirect Attack Method of Aerial Fire Firefighting by Helicopter on Forest Fire)

  • 배택훈;최연철
    • 한국항공운항학회지
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    • 제24권3호
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    • pp.55-61
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    • 2016
  • Among the method of aerial fire firefighting, the indirect attack is efficiency way to protect main facilities and it is the aerial fire line construction. According to this study is suggested the fire line construction strategy of indirect attack by helicopter suitable Korea forest fire on theory consideration of indirect attack and experience in practical scene. This study defined that main key points of the fire line construction are accuracy, large quantity, and quickness. Main protection facilities are devided as caution area, warning area, danger area and concern area. Also, it suggested stage-by-stsge from 1 step to 3 step for the aerial fire firefighting correspondence strategy and the fire line construction model. I regard that this study's indirect attack method of the aerial fire firefighting of the fire line construction may be understand about indirect attack tactics and application of indirect attack which is assistance to raise of capability of the aerial fire firefighting with effectiveness and efficiency.

산불진화 헬기의 효율적인 운영방안 연구 (Study on Efficient Operation on Aerial Fire Fighting Helicopter in Forest Fire)

  • 배택훈;이시영
    • 한국화재소방학회논문지
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    • 제29권1호
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    • pp.45-52
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    • 2015
  • 본 연구에서는 우리나라 산불현장에서 운영되는 산림청, 소방, 민간헬기의 특성과 배치현황을 분석하였다. 헬기 배치를 통합적으로 살펴보면 충북, 전남이 타 지역에 비하여 산불발생 건수가 다소 많으나 헬기배치의 공백으로 인한 초동진화에 취약하다. 경기도는 산불발생이 비교적 적은데 비하여 헬기가 많이 배치되어 강원도와 비교할 때 불균형적인 배치가 되어있다. 결론적으로 산불조심기간에 일부지역의 편중배치를 일부분 조정하여 지역별로 공백이 있는 취약한 지역에 헬기 배치와 민간헬기를 국비로 임차하여 운영하는 방안의 검토가 필요하다. 더불어 대전, 충북, 전남, 제주 등은 임차예산을 확보한 헬기 배치가 필요하며 특히, 대전은 소방헬기 기지 개설도 필요할 것으로 사료된다.