• Title/Summary/Keyword: Armed Configuration

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Airframe Durability Certification for Export Basic Trainer (수출형 기본 훈련기에 대한 기체구조물 내구성 입증)

  • Park, Taegyu;Park, Jeongkyu;Moon, Changoh
    • Journal of Aerospace System Engineering
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    • v.9 no.2
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    • pp.19-24
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    • 2015
  • Export basic trainer was designed to add armed configuration required by customer. Design configuration of main wing was changed to satisfy changed internal load caused by armed configuration. It was verified that design changed main wing airframe of export basic trainer satisfy the requirement through the structural detail analysis, structural ground test and flight test. This paper presents the durability test procensure and test result for the main wing of export basic trainer.

Mission Task & Workload Analysis of Armed Helicopter (무장헬기 임무절차 수립 및 임무하중 분석 연구)

  • Park, Hyojin;Lee, Jinwoo;Lee, Minwoo;Park, Sang C.;Kwon, Yongjin;Lee, Jonghoon
    • Journal of the Korea Society for Simulation
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    • v.21 no.4
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    • pp.25-33
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    • 2012
  • Armed helicopter is an integral part of armed forces, which conducts vital missions, such as anti-armor attack, close air support, escorting air assault operations, and reconnaissance. A typical cockpit arrangement of armed helicopters has been a tandem configuration. This is to reduce the frontal area, which in turn increases the forward speed as well as reduces the chance of being hit by enemy fires. However, many armed helicopters in the world are now being developed as a side-by-side configuration. Such configuration is quite different from the conventional cockpit arrangement in light of the crew communications and situational awareness. Therefore, the main objective of this study is to find the optimized combination of mission tasks among pilots in a side-by-side configuration cockpit by measuring the workload using the NASA Task Load Index method. The experimental results indicate that the workload of crew members differ as disparate tasks are being performed.

A Study for Optimization of Armed Flight Test Ammunition Requirement for the Development of Attack Helicopter (공격헬기 개발을 위한 무장 비행시험 탄약발수 최적화 연구)

  • Lee, Myeong-Seok;Hur, Jang-Wook
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.8
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    • pp.147-153
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    • 2020
  • Developments in aircraft require safety verification through flight testing for many hours with prototype design and production. The test evaluation step of performing flight tests was an important process that determines the success in the development of the system. In particular, safety development through flight tests in the armed flight test is important for the development of attack helicopters. In the development of attack helicopters, the evaluation period and cost related to the armed flight test are closely related to the required ammunition requirement. Therefore, this paper presents the amount of ammunition required for the military flight test between attack helicopter developments through an analysis of the AH-1 helicopter in a similar case and ADS-44-HDBK of military specification. The AH-1 can be used to calculate the ammunition demand by considering the exclusion of redundant firing tests and configuration differences. In the case of the machine gun-equipped configuration, approximately 10,500R was required, and approximately 324R was required in the case of a rocket-mounted configuration. In addition, if the armed integrated bench is used properly, it is expected to promote efficiently the flight test in the armed flight by identifying the possible risk factors with armed flight tests and excluding them.

Stabilization Performance Test Technique for LAH Turret Driving System (소형무장헬기 회전형 포탑시스템의 안정화추적 성능 시험기법)

  • Nam, Byounguk;Lee, Hojung;Jo, Sihun;Cho, Sunghun
    • Journal of the Korea Institute of Military Science and Technology
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    • v.17 no.6
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    • pp.786-792
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    • 2014
  • In this paper, we propose a novel method which can be applied to test and verify the stabilization-tracking performance of Gun/Turret Driving System(GTDS) for Light Armed Helicopter(LAH). In real system, GTDS is connected to TADS/SMC and drived to aim at the target with 20mm gun. But each equipment is separately developed during exploratory development stage, so GTDS cannot be tested under real system state. We suggest new configuration of test system for evaluating the stabilization-tacking performance, in which TADS and SMC are replaced by vision acquisition unit and processing unit, respectively.

Scheduling Start-up Transient Periods of Dual Armed Cluster Tools (양팔 클러스터장비의 초기 전이 기간 스케줄링)

  • Hong, Kyeung-Hyo;Kim, Ja-Hee
    • Journal of the Korea Society for Simulation
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    • v.24 no.3
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    • pp.17-26
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    • 2015
  • A cluster tool used in many kinds of semiconductor processes for improving the performance and the quality of wafers has a simple configuration, but its schedule is not easy because of its parallel processing module, a lack of intermediate buffers, and time constraints. While there have been many studies on its schedule, most of them have focused on full cycles in which identical work cycles are repeated under constant task times. In this research, we suggest strategies of start-up transient scheduling which satisfies time constraints and converges into a desirable steady schedule for full work cycle. The proposed schedules are expected robust under the stationary stochastic task times. Finally, we show that the strategies make schedules enters the desirable steady schedule and robust using the simulation.

A Study on the Influence of Helicopter Main Rotor Inflow Model upon Launched Rocket Trajectory and Safe Launch Envelope (헬리콥터 유입류 모델에 따른 발사된 로켓의 비행궤적 영향성 및 안전발사 기동영역 해석 연구)

  • Yang, Chang Deok;Jung, Dong Woo
    • Journal of Aerospace System Engineering
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    • v.13 no.3
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    • pp.70-77
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    • 2019
  • This study presents the numerical investigation of the trajectory of rocket launched from a helicopter. The nonlinear mathematical model of armed configuration of UH-60 helicopter was developed while Hydra 70 unguided rocket was modeled to simulate the rocket behavior. The effects of various inflow models on the launched rocket trajectory are obtained. Similarly, rocket launch simulation was performed to determine the unsafe flight maneuver condition where the rocket trajectory is critically close to the helicopter main rotor tip path plane.

Multi Function Console display configuration and HCI design to improve Naval Combat System operability

  • Park, Dae-Young;Jung, Dong-Han;Yang, Moon-Seok
    • Journal of the Korea Society of Computer and Information
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    • v.24 no.12
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    • pp.75-84
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    • 2019
  • The Naval Combat System has several equipment needed to operate the system, such as radar equipment, underwater sensor equipment, guns and missile control and armed control equipment, and a multi function console is configured to control it. The multi function console is equipped with HCI(Human Computer Interaction)-based software for displaying the status information of equipment and controlling equipment, and the operator uses the installed software to operate the Naval Combat System. However, when operating a Naval Combat System for a long time, there are problems such as physical discomfort caused by the structure of the multi function console display and increase in fatigue of the person who operates various and complicated user interface configuration. These issues are important factors in reducing Naval Combat System operability. In order to solve these issues, in this paper, based on a questionnaire survey conducted for Naval Combat System development personnel, multi function console screen design to reduce physical discomfort and HCI design to reduce fatigue and increase intuition are proposed. The proposed design is expected to provide convenience to future Naval Combat System operators and improve operation over existing Naval Combat System.

Evaluation method for interoperability of weapon systems applying natural language processing techniques (자연어처리 기법을 적용한 무기체계의 상호운용성 평가방법)

  • Yong-Gyun Kim;Dong-Hyen Lee
    • Journal of The Korean Institute of Defense Technology
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    • v.5 no.3
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    • pp.8-17
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    • 2023
  • The current weapon system is operated as a complex weapon system with various standards and protocols applied, so there is a risk of failure in smooth information exchange during combined and joint operations on the battlefield. The interoperability of weapon systems to carry out precise strikes on key targets through rapid situational judgment between weapon systems is a key element in the conduct of war. Since the Korean military went into service, there has been a need to change the configuration and improve performance of a large number of software and hardware, but there is no verification system for the impact on interoperability, and there are no related test tools and facilities. In addition, during combined and joint training, errors frequently occur during use after arbitrarily changing the detailed operation method and software of the weapon/power support system. Therefore, periodic verification of interoperability between weapon systems is necessary. To solve this problem, rather than having people schedule an evaluation period and conduct the evaluation once, AI should continuously evaluate the interoperability between weapons and power support systems 24 hours a day to advance warfighting capabilities. To solve these problems, To this end, preliminary research was conducted to improve defense interoperability capabilities by applying natural language processing techniques (①Word2Vec model, ②FastText model, ③Swivel model) (using published algorithms and source code). Based on the results of this experiment, we would like to present a methodology (automated evaluation of interoperability requirements evaluation / level measurement through natural language processing model) to implement an automated defense interoperability evaluation tool without relying on humans.

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