• 지능정보연구
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• 제11권2호
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• pp.47-57
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• 2005

본 논문에서는 험로를 주행하는 무인 자동차의 운동을 재현하는 차량 시뮬레이터의 운동큐를 생성함에 있어서 중요한 인자들을 결정할 때 충실한 재현을 위하여 필터를 적용하였다. 그러나 필터의 성능한계와 차량운동을 재현하는 워시아웃 알고리즘의 한계를 극복하기 위한 방안으로 퍼지논리를 이용한 필터의 설계를 하여 실차 실험에 적용하였고 향후의 연구방향을 제시하였다.

• Advances in aircraft and spacecraft science
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• 제3권3호
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• pp.243-257
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• 2016

The increase of air traffic volume has brought an increasing amount of issues related to carbon and NOx emissions and noise pollution. Aircraft manufacturers are concentrating their efforts to develop technologies to increase aircraft efficiency and consequently to reduce pollutant discharge and noise emission. Ultra High By-Pass Ratio engine concepts provide reduction of fuel consumption and noise emission thanks to a decrease of the jet velocity exhausting from the engine nozzles. In order to keep same thrust, mass flow and therefore section of fan/nacelle diameter should be increased to compensate velocity reduction. Such feature will lead to close-coupled architectures for engine installation under the wing. A strong jet-wing interaction resulting in a change of turbulent mixing in the aeroacoustic field as well as noise enhancement due to reflection phenomena are therefore expected. On the other hand, pressure fluctuations on the wing as well as on the fuselage represent the forcing loads, which stress panels causing vibrations. Some of these vibrations are re-emitted in the aeroacoustic field as vibration noise, some of them are transmitted in the cockpit as interior noise. In the present work, the interaction between a jet and wing or fuselage is reproduced by a flat surface tangential to an incompressible jet at different radial distances from the nozzle axis. The change in the aerodynamic field due to the presence of the rigid plate was studied by hot wire anemometric measurements, which provided a characterization of mean and fluctuating velocity fields in the jet plume. Pressure fluctuations acting on the flat plate were studied by cavity-mounted microphones which provided point-wise measurements in stream-wise and spanwise directions. Statistical description of velocity and wall pressure fields are determined in terms of Fourier-domain quantities. Scaling laws for pressure auto-spectra and coherence functions are also presented.

• 산업경영시스템학회지
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• 제41권4호
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• pp.42-49
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• 2018

Pilot Aptitude Research Equipment (PARE) is a simulator developed to measure or research pilot aptitude and train for student pilots. Design of an ergonomic PARE operation console is required to operate the equipment effectively. This study carried out five steps : (S1) operator questionnaire survey, (S2) anthropometric design formula development, (S3) usability evaluation, (S4) improvement design, and (S5) validation considering both Physical User Interface (PUI) and Graphic User Interface (GUI) of PARE operation console. The operator questionnaire surveyed needs for each PUI and GUI part of the console from two PARE actual operators. In terms of PUI, the anthropometric design formula was developed by using design variables, body dimensions, target population characteristics, and reference posture related to the PARE console. In terms of GUI, the usability evaluation was conducted by three usability testing experts with a 7-point scale (1 : very low, 4 : neutral, 7 : very high) on GUI of the PARE operation console by seven usability criteria. The improved PARE operation console was designed to reflect the optimal values of design variables calculated from design formula, the results from usability testing, and the operator's needs. The improvement effect was observed by 20 people who had experience with the PARE operation console. As a result of the validation, monitor visibility and cockpit visibility for the improved PUI design and visibility and efficiency for the improved GUI design were significantly increased by more than 90% respectively. The improved design of the PARE operation console in this study can contribute to enhance operation performance of the PARE.

• 융합정보논문지
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• 제9권5호
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• pp.27-33
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• 2019

완전자율주행(Auto Driving, AD) 실현을 위한 다양한 기술적, 사회적 접근이 진행되고 있으며, 동시에 통신 네트워크와 확장된 첨단운전자지원시스템을 포함하는 협력주행(Cooperative Driving, CD)에 대한 개발이 진행되고 있다. CD에서는 운전자와 시스템의 역할 분담과 주행 안정성 확보가 중요하기 때문에 운전자와 차량 간 효율적인 인터페이스 방안이 요구된다. 본 연구는 CD에서의 운전자와 시스템의 역할과 기능을 고려하여 운전자, 시스템 및 불확실성을 내재한 주행 환경을 포함하는 연구모델을 제안한다. 또한 주행 환경에 대한 분석과 연구모델을 이용하여 CD에서의 다양한 주행 상황에 대응해야하는 운전자와 차량 간의 효율적인 인터페이스 방안을 제시하였다. 본 연구를 통해서 제안된 연구모델과 인터페이스 방안은 CD 시스템 설계, 운전석 모듈 개발 및 인터페이스 디바이스 개발에 기여할 수 있을 것으로 기대된다.

• 한국의류산업학회지
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• 제22권6호
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• pp.844-852
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• 2020

This study is to understand the preferences of pilots, flight engineers and crew who work in the same aircraft but are exposed to different working environments and perform different mission operations in order to develop an ergonomic flight jacket. Based on a preliminary investigation, a survey of 107 pilots and 36 flight engineers and crew was conducted. The results are as follows; Pilots can control the temperature inside the cockpit, so they are less exposed to the cold when working, while flight engineers and crew are exposed to the cold more because they have many external tasks. The reason for the problem of the current flight jacket was a difference in ranking between two groups, but the highest ranking was poor dimensional suitability due to the habit of wearing layers of clothing. As a result of preferred design, there were significant differences between groups in the item of overall style. Pilots preferred a bomber jacket style(P:68.2%, E&C:44.4%), on the other hand, flight engineers and crew preferred a field jacket style(P:26.2%, E&C:55.6%)(p<.01). They preferred a stand collar(P:71.0%, E&C:86.1%), a fastener slider for a front fastening(P:62.6%, E&C:61.1%), fastener tape cuffs(P:54.2%, E&C:47.2%), a jacket with a softshell(P:86.9%, E&C:83.3%), fleece as softshell material(P:88.8%, E&C:69.4%), and fastener sliders as a attaching method(P:69.2%, E&C:61.1%). A hem fastening will be selected differently according to the overall style of outshell. Additionally, they preferred more than 5ea pockets(P:51.4%, E&C:44.4%), fastener sliders as pocket's fastenings(P:48.6%, E&C:61.1%), armpit ventilations(P:62.9%, E&C:58.5%). The results of above will be considered to design an ergonomic flight jacket.

• 한국항행학회논문지
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• 제27권4호
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• pp.323-329
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• 2023

본 연구는 헬리콥터 조종사 교육에 있어서 성공적인 비행훈련 성과에 영향을 미치는 요인을 살펴보고자 한다. 이를 위해 탐색적 요인분석을 이용하여 개인의 인지적 특성과 비인지적 특성을 추출하고, 계층적 회귀분석을 통해 이러한 특성(요인)들이 비행훈련 성과에 얼마나 영향을 미치는지 알아보았다. 그 결과 공간지각능력, 회복탄력성, 숙달목표지향적 학습태도 성향이 높을수록 비행 교육성과에 긍정적인 영향을 미치는 것으로 나타났다. 이는 조종사에게 특히 요구되는 공간지각능력의 중요성을 재확인할 수 있었고, 그리고 제한된 조종석 공간에서의 비행교관의 역할, 개인의 올바른 동기부여와 노력이 비행훈련 성과에 영향을 미친다는 것을 재확인시켜준다. 이러한 결과는 향후 헬기 조종사의 효과적인 비행교육에 유용한 지표가 될 것으로 기대한다.

• 한국항행학회논문지
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• 제27권6호
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• pp.724-732
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• 2023

민간 항공기에는 기장과 부기장이 반드시 탑승해야 한다. 일반적으로 기장은 항공기 운항 중 위난방지에 관한 역할과 책임을 이행하고, 부기장은 기장을 보좌하거나 조언하는 기능을 담당한다. 역사적으로 70%~80%의 항공기 사고가 조종사 인적요인에 의하여 발생함에 따라 전 세계적으로 CRM (crew resource management)이라는 운항관리기법을 도입하여 운영하고 있다. 한편 안전행동은 지식과 기술을 사용하여 위험으로부터 보호하려는 인간의 행동이며, 항공기 조종실에서 운항업무를 수행하는 기장과 부기장은 각각의 역할과 책임, 그리고 경험의 차이에 따라 안전행동의 수준 또한 다를 것으로 예상된다. 선행연구는 조종사의 안전행동이 기술적 능력에 영향을 받기보다 CRM skill과 같은 비기술적 요소에 영향을 받는다고 하였으며, 본 연구는 기장과 부기장의 CRM 역량 차이를 파악하고 그 차이가 안전행동과의 상관관계를 가지고 있는지를 검증하고자 수행되었다.

• 한국국방경영분석학회지
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• 제2권1호
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• pp.127-143
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• 1976

The purpose of this thesis is to study the optimal arrangement of aircraft instrument panels through the human factors approach. Human factors engineering is the process of effectively fitting the human component to the machine component in any man-machine system. The human factors. are especially important to an aircraft pilot who must constantly shift his attention between the instrument panel within the cockpit and the surrounding area of the aircraft. The preliminary part of this study is to find the general patterns of the Korean pilot's eye movements during their various flying maneuvers, and which instruments require the most attention while in flight. It is assumed that all pilots have a general pattern of eye movement when observing the aircraft instrument panel and that an optimum arrangement would be to minimize the eye travel distance between instruments. In this thesis the arrangements of instruments is taken to be the independent variable and the eye travel distance between instruments the dependent variable. la order to compile the information necessary for this study, sixty Korean Air Force pilots were interviewed and requested to complete information forms. These information forms listed various flying maneuvers and listed each instrument used on the instrument panel. The compilation of the information on these completed forms listed the instruments most frequently used by the pilots. The second part of this study was to determine the optimum instrument arrangement. It was necessary to study the various number of possible arrangements of instruments depending upon the number of instruments involved. Therefore, these instruments are grouped by two major functions, The flight instruments were subdivided into three groups, and the engineering instruments were subdivided into six groups. With this subdivision we arrive at the possible number of arrangements of 4,320. Through the simulation method, total eye travel distance for each of these 4,320 arrangements is calculated and the arrangement which appears to be of optimum distance between the most frequently used aircraft instruments is determined. The results of this study indicate that the optimum distance between instruments would be 33,028cm and that the corresponding distance of the instrument panel now being used is 34,288cm. Therefore, an increased efficiency of $3.8\%$ would be realized if the existing aircraft instrument panel were re-arranged according to layout proposed in this thesis.

• 대한인간공학회지
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• 제28권1호
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• pp.37-51
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• 2009

The nuclear power industry in the world has recognized the importance of integrating non-technical and team skills training with the technical training given to its control room operators to reduce human errors since the Three Mile Island and Chernobyl accidents. The Nuclear power plant (NPP) industry in Korea has been also making efforts to reduce the human errors which largely have contributed to 120 nuclear reactor trips from the year 2001 to 2006. The Crew Resource Management (CRM) training was one of the efforts to reduce the human errors in the nuclear power industry. The CRM was developed as a response to new insights into the causes of aircraft accidents which followed from the introduction of flight recorders and cockpit voice recorders into modern jet aircraft. The CRM first became widely used in the commercial airline industry, but military aviation, shipboard crews, medical and surgical teams, offshore oil crews, and other high-consequence, high-risk, time-critical industry teams soon followed. This study aims to develop a CRM training program that helps to improve plant performance by reducing the number of reactor trips caused by the operators' errors in Korean NPP. The program is; firstly, based on the work we conducted to develop a human factors training from the applications to the Nuclear Power Plant; secondly, based on a number of guidelines from the current practicable literature; thirdly, focused on team skills, such as leadership, situational awareness, teamwork, and communication, which have been widely known to be critical for improving the operational performance and reducing human errors in Korean NPPs; lastly, similar to the event-based training approach that many researchers have applied in other domains: aircraft, medical operations, railroads, and offshore oilrigs. We conducted an experiment to test effectiveness of the CRM training program in a condition of simulated control room also. We found that the program made the operators' attitudes and behaviors be improved positively from the experimental results. The more implications of the finding were discussed further in detail.

• 기술혁신연구
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• 제27권2호
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• pp.37-71
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• 2019

승용차의 아키텍처는 어떻게 진화해왔는가? 그간 승용차 아키텍처에 대한 논의는 통합형, 모듈형, 그리고 두 유형의 공존 등이 혼재되어 왔다. 이에 따라 본 연구에서는 글로벌 무역 자료를 활용하여 제품의 중층 구조를 반영한 모듈화의 진전 측정 지수를 개발하고, 이를 아키텍처 유형 프레임워크에 적용하여 승용차 아키텍처의 모듈화 진행을 종단적으로 분석하였다. 분석결과 승용차 아키텍처는 지난 2000년 이후 모듈화가 지속적으로 진행되었음을 확인하였으며, 동시에 모듈화 진행은 구성 모듈 별로 상이한 것으로 나타났다. 모듈 중에는 프론트-엔드, 운전석 및 시트 모듈의 모듈화 진행이 뚜렷함을 확인된 반면, 차체 도어 천장 모듈은 소비자 니즈 충족을 위한 외부 디자인 차별화 및 완성차와 모듈업체 간 상호 조율강화로 인해 모듈화가 더디게 진행됨을 관찰하였다. 또한 샤시, 엔진, 그리고 트랜스미션 모듈로 구성된 플랫폼은 모델 다양화, 생산 원가 절감, 신제품 개발 기간 단축을 위한 완성차 업계의 지속적인 노력에 따라 모듈화가 지속 진전됨을 확인하였다. 플랫폼 구성 모듈 중에서는 트랜스미션의 모듈화 진전이 가장 두드러진 반면 샤시와 엔진 모듈은 완성차 업체의 자체 혁신 노력으로 인해 비교적 통합형 아키텍처 경향이 강한 것으로 나타났다. 본 연구는 제품 아키텍처의 모듈화를 계량적으로 측정, 그 진행을 종단적으로 측정할 수 있는 접근법을 제시하는데 기여하였다. 또한 모듈 별 상이한 모듈화 진전에 대한 고찰을 통해 관련 연구의 분석 수준의 세분화 필요성을 제안하였다. 아울러 본 연구는 승용차 산업 전반에서 일어나고 있는 아키텍처 모듈화 진전 현상을 규명함으로써 완성차 업체 뿐 아니라 모듈 업체의 아키텍처 선택과 그에 따른 전략 수립의 가이드라인을 제시하였다. 본 연구가 다양한 제조업과 그 제품의 모듈화 진전을 규명하는데 활용되기를 기대한다.