• 한국항공우주학회지
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• 제32권5호
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• pp.1-9
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• 2004

수직이착륙과 고속수평비행이 기능한 스마트 무인기 개발의 일환으로 초기개념설계용 성능예측 프로그램을 작성하였다. 스마트 무인기가 요구하는 설계조건을 기반으로 각 임무 단계 수행과정에서의 연료소모중량을 반복계산하여 전체 중량을 예측하고, 동시에 무인기의 주요형상변수, 추진성능, 수직이착륙성능, 수평비행성능 등의 계산을 통해 성능예측 및 설계요구조건 만족여부 판단, 경향성 분석을 수행할 수 있다. 동 프로그램은 수직이착륙 무인항공기 비행체의 초기개념설계단계에서 비행체의 경향성 분석, 비행성능 예측 및 설계 요구조건 검증 등을 손쉽고 간편하게 수행 할 수 있는 도구도서 사용할 수 있다.

• 한국운동역학회지
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• 제17권3호
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• pp.133-145
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• 2007

The purpose of this paper was to compare of difference between energy walking and normal walking. Subjects were selected 8 male undergraduates. The kinematic variables of a pelvis and a thorax were analysed at the take off and contact with 3d cinematography. In addition to the variables, the phase plot angle was calculated in order to definite characteristics in the phase space. The pelvic angle and angular velocity showed significant differences in the flexion/extension between two walking patterns. The pelvic angle and angular velocity were increasing when walking speed was increasing and magnitude of the variables of energy walking was larger than corresponding values for normal walking. On the other hand, the thoracic angle demonstrated significant differences in the flexion/extension and rotation between two walking patterns. The angles of energy walking were smaller in the flexion/extension and were larger in the rotation than the angle of normal walking. The kinematic characteristics of energy walking were also showed clearly significant differences in the range of motion and the relative angle of the trunk. The angle of phase plot only showed demonstrated a significant difference in the rotation at contact between the two walking patterns.

• 한국정밀공학회지
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• 제22권5호
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• pp.113-120
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• 2005

Because of the turbulent markets and the increasing demand on product quality, the application of new technology to practice is increasingly important. In case of automotive industries, they take interest in laser welding to solve these problems because laser welding has many advantages such as good accessibility, welding quality, fast welding speed and so on. To apply this technology to welding of car body, the data of laser welding are collected through lots of the experiment according to the material, geometry and layer number of welding points. Based on the experiment results and the information of product, i.e. the car side panel, the clustering of stitches for laser welding was carried out and the optimal equipments are selected through the comparison between the requirements of welding and the potential of equipments. Using these results, laser welding cell for the car side panel are configured with the concept of the digital manufacturing, which ensures maximum planning security with visualization and simulation. Finally, the optimal laser welding cell is chosen by the evaluation of alternative cells with assessment criteria.

• 한국항공운항학회지
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• 제29권4호
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• pp.96-104
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• 2021

Technological advances have recently led to the development of Urban Air Mobility (UAM) which is a small airplane being able to take off and land vertically. It is emerging as an alternative to transportation services in the city in the future because of the advantage of providing speed and congestion problem in cities like taxis. This research aim to study the user's acceptance of UAM. Based on the survey conducted abroad, the analysis was carried out based on th Technology Acceptance Model (TAM), by Davis et al. (1989). According to the data analysis results of 292 people, Technology, Reliability and Price effect perceived usefulness, which in turn effects Behavioral intention. UAM cannot be operated independently by a single company. It consists of partnerships with vehicles, transport platforms, batteries and other related company. To improve acceptance of UAM, it is required that collaboration between companies and support from government. And while UAM is being developed, research on acceptance from user's point of view should continue.

• 한국항공운항학회지
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• 제32권1호
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• pp.79-90
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• 2024

UAM is emerging due to the deepening population concentration in the metropolitan area and the problem of congested ground transportation in urban areas. Accordingly, along with research on eVTOL aircraft for UAM services, interest in vertiport, the interest in vertiports, the infrastructure that allows eVTOLs to take off and land, is also increasing. However, behind the concentration of population in the metropolitan area, aphenomenon of local extinction is occurring in conjunction with the aging population. AAM, which moves quickly through 3D space, can be an effective SOC facility in times of local extinction crisis. In this paper, we introduce a design plan from the perspective of a complex transper center for a regional hub-level vertiport that can connect with local high-speed rail and utilize local airports in compliance with the vertiport design guidelines issued by FAA(Federal Aviation Administration) and EASA(European union Aviation Safety Agency). We would like to present Vertiport's future operation plan.

• 디지털융복합연구
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• 제13권8호
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• pp.495-502
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• 2015

본 연구는 빙상 선수를 대상으로 외발점프 훈련 시 하지관절 운동역학 변인의 차이를 분석함으로써 무릎테이핑의 효과를 알아보고자 하였다. 연구결과 다음과 같은 결론을 얻었다. 점프높이는 테이핑 후 높은 것으로 나타났지만 테이핑에 따른 차이는 없는 것으로 나타났다. 상승 시 좌 우, 전 후 최대충격력은 테이핑 후 감소되는 것으로 나타났고, 수직 최대충격력은 테이핑 후 증가된 것으로 나타났다. 착지에서 테이핑 후의 좌우 최대충격력은 감소되었으나 전 후, 수직 최대 충격력은 증가된 것으로 나타났다. 상승과 하강 시 테이핑 후 충격량의 감소가 크게 나타났다. 상승 시 테이핑 후 무릎관절의 신전, 외번모멘트에서 감소가 나타났다. 착지에서 테이핑 후 무릎관절의 굴곡모멘트는 감소했지만 내번모멘트는 테이핑 후 증가된 것으로 나타났다. 무릎테이핑이 선수들의 부상예방과 운동수행능력에 도움을 줄 수 있을 것으로 판단되며 스포츠의학과의 융복합연구가 필요할 것으로 판단된다.

• 한국항공우주학회지
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• 제38권10호
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• pp.973-978
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• 2010

본 논문에서는 유격을 고려한 항공기 전방 착륙 장치의 쉬미 현상을 연구하였다. 쉬미는 항공기의 이착륙 시 랜딩기어가 주행도중 측방향과 조향방향으로 진동에 놓이는 현상이다. 이 현상은 스트럿의 낮은 강성, 랜딩기어 내부의 마찰과 유격, 휠의 불균형이나 마모된 부품 등으로 인해 발생하며, 항공기의 안정성을 저하시킨다. 유격은 비선형 요소이기 때문에 기술 함수로 선형화 하여 주파수 영역에서 안정성해석을 수행하였고, 4차 Runge - Kutta를 이용하여 시간영역에서 안정성해석을 수행하였다. 본 연구에서는 수치적인 해석법을 통해 쉬미현상의 선형 동특성과 비선형 동특성을 조사하였다. 유격을 고려한 비선형 수치 해석결과, 선형 임계속도보다 낮은 속도에서 제한주기진동이 발생하는 등, 유격으로 인해 쉬미 안정성이 저감되는 결과를 관찰하였다.

• Journal of Biosystems Engineering
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• 제43권2호
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• pp.83-93
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• 2018

Purpose: This study derived the consumed power and load characteristics of a tillage operation performed in an upland field located in Seomyeon, Chuncheon, Rep. Korea, where potatoes and cabbages were cultivated in two crops. Methods: A plow and rotavator were mounted on a tractor with 23.7 kW of rated power to perform the tillage operation. The work conditions were determined, considering the actual working speed of the tillage operation performed by the local farmers. The power consumption of the rear axle, engine, and power take-off (PTO), PTO torque, and tractive force were measured under each work condition. The consumed power and load characteristics were analyzed using their average values. Results: The rotary-tillage operation consumed more engine power than the plow operation for the same tractor-transmission gear condition. The PTO in the rotary-tillage operation and the rear axle in the plow operation consumed the most power. The power consumption of the engine and the PTO for the rotary-tillage operation tended to increase as the transmission gears of the tractor and the PTO became higher. In contrast, the rear-axle power consumption was insignificant. In addition, the PTO torque tended to rise as the tilling pitch increased. For the plow operation, the drawbar power and the rear axle power accounted for 68-90% of the engine power. The engine and rear axle power, drawbar power, and tractive force tended to rise as the working speed increased. Conclusions: The power consumption and load characteristics differed for the plow and rotary-tillage operations. They may also differ depending on the soil conditions. Therefore, the power consumption and load characteristics in various work environments and regions should be analyzed, and reflected in the design of tractors and working implements. The results derived from this study can be used as a reference for such designs.

• 한국운동역학회지
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• 제19권1호
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• pp.87-98
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• 2009

본 연구는 남자고등학생 숙련자와 비 숙련자의 던지기 동작을 역학적으로 비교 분석하기 위해 3차원 영상분석 및 지면반력분석을 수행하였다. 연구 결과 숙련자는 공 던지기 동작의 총 소요 시간이 비숙련자보다 짧게 나타났으며, 숙련자는 (1) 왼발 착지 시 신체중심의 수평속도 (2) 전 구간에서 전완 분절의 수평속도 (3) 착지 시 손 분절의 수평속도가 비숙련자보다 빠르게 나타난 반면, 비숙련자는 (1) 착지이후에 신체중심의 수평속도 (2) 왼발이 지면에 닿는 시점에서 손 분절의 수평속도가 숙련자보다 빠르게 나타났다. 전후경각도에서 숙련자는 전 구간에서 후경자세를 취하는 것으로 나타났으나, 비 숙련자는 릴리즈 전까지는 후경자세를 취하다 릴리즈 순간에서는 전경자세를 취한 형태에서 릴리즈를 하는 것으로 나타났다. 또한 숙련자는 공 던지기 동작에서 (1) 어깨각도 (2) 이지 후 오른발의 착지에서 팔꿈치 각도 (3) 최대수직지면반력 (4) 오른발의 착지 시 최대전후지면반력이 비숙련자보다 크게 나타났다. 이와 같은 결과에서 숙련자는 비숙련자보다 안정된 자세로 신체의 중심을 후방에 위치시키는 후경자세를 유지하고 신체의 중심이동을 부드럽게 전환하는 효과적인 던지기 동작이 이루어짐을 알 수 있다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.513-520
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• 2004

A steady-state/transient performance simulation model was newly developed for the propulsion system of the CRW (Canard Rotor Wing) type UAV (Unmanned Aerial Vehicle) during flight mode transition. The CRW type UAV has a new concept RPV (Remotely Piloted Vehicle) which can fly at two flight modes such as the take-off/landing and low speed forward flight mode using the rotary wing driven by engine bypass exhaust gas and the high speed forward flight mode using the stopped wing and main engine thrust. The propulsion system of the CRW type UAV consists of the main engine system and the duct system. The flight vehicle may generally select a proper type and specific engine with acceptable thrust level to meet the flight mission in the propulsion system design phase. In this study, a turbojet engine with one spool was selected by decision of the vehicle system designer, and the duct system is composed of main duct, rotor duct, master valve, rotor tip-jet nozzles, and variable area main nozzle. In order to establish the safe flight mode transition region of the propulsion system, steady-state and transient performance simulation should be needed. Using this simulation model, the optimal fuel flow schedules were obtained to keep the proper surge margin and the turbine inlet temperature limitation through steady-state and transient performance estimation. Furthermore, these analysis results will be used to the control optimization of the propulsion system, later. In the transient performance model, ICV (Inter-Component Volume) model was used. The performance analysis using the developed models was performed at various flight conditions and fuel flow schedules, and these results could set the safe flight mode transition region to satisfy the turbine inlet temperature overshoot limitation as well as the compressor surge margin. Because the engine performance simulation results without the duct system were well agreed with the engine manufacturer's data and the analysis results using a commercial program, it was confirmed that the validity of the proposed performance model was verified. However, the propulsion system performance model including the duct system will be compared with experimental measuring data, later.