• 한국운동역학회지
• /
• 제25권1호
• /
• pp.57-64
• /
• 2015

Purpose : The purpose of this study was to analyze setter toss motion kinematically according to toss types. Method : Dependent variables were elapsed time, vertical displacement of the body center, the projected speed of the ball, and differences of the joint angle to the target for four setters positioning. Result : There was no significant difference in the time but the ball contact time was shorter when the toss distance of P3 was longer. There was significant difference in the vertical displacement of COM (p<.05). The vertical displacement of COM showed that the vertical movement gradually decreased when the quick distance was longer. The vertical displacement of COM was difference (p<.05), also there was difference of the ball speed (p<.001) at the Release point(E4). There was significant difference in the knee joint angle at a certain moment among the Release(E4) and Landing point(E5)(p<.05). The hip joint was significant difference among the Apex(E2), Ball Touch(E3), Release(E4), and the Landing point(E5) on the surface(E2, E3, E4 p<.05; E5 p<.005). The shoulder angle was significant difference among the Ball Touch(E3), Release(E4) and the Landing point(E5) on the surface(E3, E4 p<.05; E5 p<.001). The elbow was significant difference in the Apex(E2) (p<.05). The wrist was significant difference in the Release(E4) (p<.05). Conclusion : If we find the clue to expect the direction of the setter's ball, we have to fine the clues in the Apex(E2) that hip join and elbow, Ball Touch(E3) that hip joint and shoulder joint, Release(E4) that wrist, elbow, hip joint, and knee joint.

• 한국항행학회논문지
• /
• 제16권2호
• /
• pp.179-189
• /
• 2012

본 논문은 측풍이 $40^{\circ}$일 때 이착륙 비행안정성의 예측을 위하여 활주로에 발생되는 유동현상과 받음각 변화량을 3차원 수치해석을 통하여 연구하였다. 3차원 수치해석결과 활주로 주변 시설물에서 발생된 후류로 인하여 활주로 상에서 발생되는 받음각 변화량의 최대 진폭은 $2^{\circ}$이고 그 지속 시간은 약 3초로 나타났으며 전체적으로 보면 불규칙적인 비주기적 성향으로 나타난다. 특히 건물의 배치와 형상이 활주로와 유도로에 발생되는 후류의 강도에 직접적인 영향을 미치고 시설물 사이를 통과한 빠른 흐름으로 인하여 더욱 강한 후류영역을 발생시켜 활주로 상에서 심각한 이착륙 불안정성을 발생시킬 것으로 예상된다.

• Composites Research
• /
• 제22권2호
• /
• pp.30-36
• /
• 2009

본 논문에서는 헬리콥터 착륙장치를 위한 복합재료 토크링크를 개발하기 위한 설계 기법을 제시하였다. 복합재 토크링크는 헬리콥터 착륙장치의 충격흡수부의 정렬을 위해 장착되는 장치로서 가벼우면서도 강성이 커서 외부하중에 대해 최소의 변형량을 가져야 한다. 또 가격적인 측면을 고려한 복합재 구조물 제조 공정(RTM: 수지충전공정)이 반영되어 대량생산이 가능한 구조 및 형태를 가져야 한다. 본 논문에서는 복합재 구조물 제조 공정과 동일한 공정으로 시편을 제작하여 설계에 필요한 기계적 특성을 얻었으며, 유한요소해석을 통하여 복합재 토크링크에 대한 최적 형상설계를 수행하였다. Lug 형태를 가지는 두꺼운 복합재료 구조물인 복합재료 토크링크의 설계를 위해서는 ABAQUS의 3D Layered Solid 요소로 구성된 유한요소모델을 활용하여 복합재료의 두께방향을 포함한 강도해석을 수행하였으며, Rigid-Deform 구속조건의 접촉문제를 고려한 비선형 정적 해석을 반복적으로 수행하여 주어진 정강도 요구조건을 만족시키는 복합재 토크링크를 설계하였다.

• 융합정보논문지
• /
• 제12권2호
• /
• pp.37-46
• /
• 2022

본 연구는 빅데이터와 키워드 네트워크 분석을 통해 공동선 증진을 위한 미래교육 방향을 탐색함으로써 미래교육의 방향성 제안에 대한 기초자료를 제공하는 것을 목적으로 한다. Textom에서 제공하는 빅데이터를 기반으로 '미래교육 + 공통선'이라는 키워드로 데이터를 수집한 후 키워드 네트워크 분석을 수행했다. 연구결과 '공익', '사회', 'KAIST 미래경고', '대책', '연구', '미래교육', '정치' 등이 공동선을 위한 미래교육의 사회적 인식에서 공통 키워드인 것으로 나타났다. 이번 연구결과는 공동선 증진을 위한 미래교육에 대한 사회적 인식이 인간, 물리적 환경, 사회적 대응, 학문적 관심, 교육정책, 교육계획 및 관련 변수와 밀접한 관련이 있음을 시사한다. 이와 같은 결과를 바탕으로 공동선 증진을 위한 미래교육의 방향성 제안을 위한 기초자료 마련에 의미 있는 시사점을 제시하였다.

• 제어로봇시스템학회논문지
• /
• 제11권8호
• /
• pp.726-732
• /
• 2005

This paper proposes an autolanding guidance and control algorithm with the lateral guidance law. This algorithm is basically formulated and designed in feedback linearization based on singular perturbation. Main features of this algorithm are two facts. One of those is that when a certain situation happens that airplane must realign to the runway suddenly assigned due to unexpected environment change around the landing site, the heading guidance in this algorithm is very valuable, and the other is the fact that the inner loop control of this algorithm is able to be designed directly based on the Handling Quality Requirements that most flight control systems must be satisfied with. To illustrate the potential of this algorithm, 6-DOF nonlinear simulation based on the nonlinear airplane model shown in Ref.[11] is carried out. The simulation results showed that the altitude response to the given landing trajectory is accurate, and the airplane heading alignment to the assigned runway from the lateral deviation is successful. It is noted that this algorithm is also applicable to unmanned aerial vehicle, which can be retrieved in autolanding technique, where the runway far retrieving the vehicle is in any direction for example at war field.

• 수산경영론집
• /
• 제50권3호
• /
• pp.17-29
• /
• 2019

This paper aims to find out the problems and improvement direction of quality control and hygiene management of fishery products in Korea. For this reason, we conducted a comparative analysis of quality control and hygiene management of fishing, landing and selling between Japan and Korea, taking mackerel as an example. Japan has established a systematic freshness management system from fishing to landing (production) areas and consumption areas. On the other hand, Korea is not fully lead-managed in the production area after fishing, and is distributed in a state where the quality of the product is deteriorated due to exposure to room temperature. Accordingly, a certain quality can not be secured at the final consumption stage, and sanitary problems occur. In order to improve the quality control and hygiene management of the fishery products, the following needs to be improved. First, we will improve the fishing level freshness management system. Second, we will improve the quality control and hygiene management of fish in the production area and wholesale stage. Third, we will promote the introduction of innovative sales and consignment sales systems at the production stage. Fourth, we will establish a consistent low temperature distribution system from the production area to the wholesale stage from a long-term perspective. Fifth, we will promote the development and education of manuals on fish quality and hygiene management.

• 한국항공운항학회지
• /
• 제31권1호
• /
• pp.11-17
• /
• 2023

In this study, the correlation analysis between total system error and environmental factor variables was performed to confirm the effect on the performance of the integrated navigation system by various environmental factors. To collect flight data of hybrid vertical take-off and landing UAVs, scenarios including various turning sections and straight sections such as left turn, right turn, turning rate, and path change angle were selected, and environmental data of wind direction, wind speed, temperature, air pressure, and humidity were collected in real time through weather station. As a result of the correlation analysis between the collected flight data and environmental data, it was concluded that the performance of the integrated navigation system by environmental factors within the collected data was not significant affected and was robust.

• 한국정보통신학회:학술대회논문집
• /
• 한국정보통신학회 2021년도 춘계학술대회
• /
• pp.502-504
• /
• 2021

UAV(Unmanned Aerial Vehicle)에 대한 활용영역은 시간이 갈수록 꾸준히 확대되고 있다. 특히 네 개 이상의 수평적인 프로펠러로 구성된 VTOL(Vertical Take-Off and Landing) 기능이 가능한 UAV는 시스템 안정성 및 비교적 단순한 항공역학적 설계 및 구조에 따라 다양한 플랫폼이 등장하고 있으며 비교적 저렴한 가격으로 응용제품들이 시중에 유통이 되고 있다. 대부분의 UAV는 GCS(Ground Control System, 지상시스템)를 통해 임무가 수행된다. 지상시스템은 주로 인터넷에 연결되어있기 때문에, 전자 지도 및 기타 최적의 비행조건(온도, 습도, 풍향 등)을 위한 환경정보를 또한 얻을 수 있다. 본 논문은 AIS(Auto Identification System)를 통해 얻은 정보를 기반으로 식별된 선박으로의 접근 및 감시(monitoring)하기 위한 UAV의 운영기법을 설계한다.

• 한국항공운항학회지
• /
• 제25권2호
• /
• pp.1-11
• /
• 2017

In this study, we surveyed the regulations of the Seaplane base and Sea Lane for the Light Sport Aircraft(LSA), and analyzed the water landing/takeoff roll distance of LSA in Korea. Based on the information, we presented the situation of the Sea Lane and the Sea Lane Protection Zone concept, to ensure the Rectangle type Sea Lane and the Omni direction type Sea Lane. We analyzed the availability elements of the safety of Sea Lane for LSA in Korea. A Rectangle type Sea Lane 350 meters long and 40 meters wide, the diameter 350 meters for the An Omni direction type Sea Lane.

• 한국항공운항학회지
• /
• 제20권2호
• /
• pp.18-25
• /
• 2012

The availability of the GPS signal has been expanded greatly in the field of society overall through the development and construction of the GNSS(Global Navigation Satellite System). Furthermore, in the military, aviation and field of space, the GPS signal is applied widely through the combination of INS consisting of gyroscope and accelerometer, IMU, AHRS with the addition of magnetic sensor. Particularly, the performance of these equipments or sensors is very important with GPS and PAR(Precision Approach Radar) in the flight control of the aircraft. This paper deals with MATLAB simulation and ROLSO(Reduced Order Luenberger State Observer) design to reduce the load of system and realize the stable lateral direction approach control in an appropriate time for reduction of the horizontal error which is importantly considered while an aircraft lands instead of the FOLSO(Full Order Luenberger State Observer) using all measurement values. Consequently, ROLSO is expected to be used for the aircraft's attitude control in the aircraft landing causing the burden to the pilots.