The air bridge that connects an airplane with air terminal is important facilities that help people get in and out an airplane safely and conveniently. As the number of people who takes airplane has been increasing, an unexpected accident or a disorder on an air bridge can lead to the loss of passenger's lives or a great damage of airplane. This paper suggests a method to secure the safety of an air bridge.

본 논문은 8절점 고체요소를 이용하여 항공기 충돌에 의한 원전 격납건물의 동적 거동을 분석하고 그 결과를 기술하였다. 콘크리트의 재료적 특성을 표현하기 위하여 Drucker-Prager항복기준을 바탕으로 항복면과 파괴면을 형성하였다. 이때 항복면과 파괴면은 콘크리트의 소성변형이 누적되면 가변하는 것으로 가정하였다. 철근의 재료특성은 변형도에 의존적인 탄성/점소성모델을 이용하여 표현하였다. 표준고체요소의 성능저하를 방지하기 위하여 Hughes가 제시한 B bar법을 바탕으로 변형도-변위관계 행렬을 형성하였다. 동적 시간이력해석을 수행하기 위하여 안정적인 수렴성을 가지는 암시적인 Newmark법을 도입하였다. 마지막으로 시간이력해석을 통하여 콘크리트 균열변형도의 수준과 충돌하는 항공기의 종류에 따른 격납건물의 동적거동변화를 조사하고 이를 정량적으로 기술하였다.

본 연구의 목적은 항공기용 터어보팬 엔진의 재료선정을 위한 데이타 베이스를 구축하는 것이다. 터어보팬 엔진은 고성능이면서도 연료소모율이 적어 경제적인 운용이 가능하므로 최근 여러 용도로 사용되고 있는 엔진이다. 현재 서로 다른 특성을 가진 수백종의 초내열재료들이 개발되어 있는데, 한 엔진설계자가 어떤 엔진요소에 사용할 재료를 선택한다는 것은 매우 어려운 작업이다. 따라서 수 많은 재료에 대한 정보를 관리할 수 있는 데이타 베이스가 절실히 요구되고 있으나, 국내에서는 아직 이 방면의 기초연구가 이루어져 있지 않은 실정이다. 본 연구에서는 재료공학적 관점에서 초내열재료의 대표적 성질로서 고온강도, 내식성, 내산화성, 항복강도, 열팽창계수, 융정등을 고려해서 후보재료를 선정할 수 있도록 하였다. 이외에도 성 형성이나 제조단가등도 고려해야할 변수가 된다. 본 연구에 의해 사용자의 편의를 고려한 전산프로그램이 개발되었으며, 이를 이용하여 새로운 재료정보의 입력, 요구 재료선정 및 선정결과의 출력등이 가능하다. 끝으로 선정된 재료에 대한 성능검토도 실시하였다.

In this study, we improved the water-based condensation particle counter in Atmospheric Research Aircraft NARA and investigated the condensation particle number concentration over the Korean peninsula. Pump and set point information were changed to improve the instrument used by aircraft for observation. Ground-based observational result showed that the error between two instruments, which are water-based condensation particle counter and butanol-based condensation particle counter, was 4.7%. Aerial observational result revealed that the number concentration before improvement indicate large variation with unstable condition, whereas the number concentration after improvement indicate a reasonable variation. After improvement, the number concentration was 706±499 particle/㎤ in the West Sea and 257±80 particle/㎤ in Gangwon-do, and these are similar to the concentration range reported in previous studies. Notably, this is the first attempt to use aerial observation with water-based condensation particle counter to investigate condensation particle number concentration.

This study explored measures to reduce noise applicable to Gimhae international airport centering on densely packed housing areas. Especially, as for measures to relieve noise damage on the densely packed housing areas in Gimhae-si, the noise reduction effect is expected to be doubled if the west runway (36L/18R) is used as the preferred runway for the 36 direction takeoff, as well as if the flight bypasses the densely packed housing areas by means of sophisticated navigation using the area navigation (RNAV) procedure based on performance-based navigation (PBN). Takeoff toward the south connects the flight path to the South Sea which has comparatively low noise impact, relieving noise damage on the densely packed housing areas (apartment complexes in Naeoe-dong of Gimhae-si, etc.) near the northern end of the runway. The operation of the runway displaced threshold is currently being implemented on the west runway (36L/18R) of Gimhae international airport. It has been found that swing landing in spring and summer when the wind blows from the south has a noise reduction effect on the noise sensitive areas at the side and end of the west runway (Gangdong-dong and Jukdong-dong of Gangseo-gu and Buram-dong of Gimhae-si, etc.).

The purpose of this study is to investigate systematic and comprehensive explanation about safety behavior by applying integrated model of Theory of Planned Behavior (TPB) and Social Cognitive Theory (SCT). By showing the interrelationship of effects of factors affecting safety behavior in a single model, comprehensive understanding regarding safety behavior will be possible. Research design, data, and methodology: This study try to integrate the two theory, TPB and SCT, to introduce background factors, such as safety culture, affecting cognitive factors of subjective norm, safety attitude, perceived behavioral control, safety consciousness, which are again affecting behavior intention of the TPB. We composed 73 questionnaire to analyse the relationship among factors affecting safety behavior. The questionnaire were distributed to stewards and stewardesses of KAL, ASIANA, and LCCs. 422 were collected and used for analysis. Factor analysis, regression analysis, and control effect analysis were conducted using SPSS windows version 2.0. Results: The safety culture, safety atmosphere, and safety education/training were turned out to affect subjective norm, safety attitude, perceived behavioral control, safety consciousness. And the cognitive factors also showed to affect safety intention significantly. The results that safety intention affects safety behavior was found. Also there are control effect of cost consciousness and punishment while safety intention affects safety behavior. Conclusions: Safety is the virtue that should be given first priority to in our daily life. To secure safety, everyone in an organization should have high level of safety intention and conduct safety behavior. The study results provide systematic and comprehensive understandings on the relationship among factors affecting cabin crews’ safety behavior. The results will help design safety related regulations, education/training, and support employees to engage in safety behavior related activities.

This paper presents the current status of development of assessment program for shock/Fire damage caused by aircraft impacts for NPP(nuclear power plants). According to international and domestic regulations, the design of nuclear power plants have to take into account the potential effects of the impact of a large commercial aircraft. In this study, we set up the practical application procedure to assess the shock/fire damage due to aircraft impacts for NPP in accordance with NEI(Nuclear Energy Institute)07-13 rule set and are developing the aircraft impact assessment program to reduce the effort and improve the accuracy.

The purpose of this study is to analyze the accuracy of cultivated crop database in agricultural farm business using UAV(Unmanned Aerial Vehicle) and field survey over Daesso-myeon, Umsung-gun, Chungbuk. When comparing with agricultural farm business and cadastral maps, Daeso-myeon crop field shows 29.8%(2,030 parcels out of 6,822 parcels) is either mismatched or missing. It covers almost 19.3%(3.4km2 of 17.6km2) of total farmland. In order to solve these problems, it is necessary to prepare a multifaceted plan including cadastral map. Comparative analysis of the cultivated crop registered in the agricultural farm business and the field survey agreed only in 3,622 parcels in total 6,822 parcels whereas 3200 parcels disagree. Among these disagreed parcels 2,030(29.8%) have been confirmed as unregistered farm business entity. Accuracy of cultivated crop registered in agricultural farm business agreed in 75.6% cases. Especially the paddy field registration is more accurate that other crops. These discrepancies can lead to false payment in agricultural farm business. For exploration and analysis of regional resources, UAV images can be used together with farm business management database and cadastral map to get a clearer grasp over on-site resources and conditions.

본 연구는 무인항공기를 활용한 원격탐사적 기법을 통해 고해상도 정사영상과 수치표고모델기 반 3차원 지표모델을 구축하여, 광해복구사업의 중간단계 모니터링에 활용하고 그 효율성을 고찰하였 다. 무인항공기를 통한 원격탐사로 3.8 cm의 공간해상도를 갖는 수치표고모델 및 정사영상을 구축하 였으며, 광해복구사업의 중간과정을 모니터링하였다. 또한 고해상도 영상을 통해 사물 및 지형적 구분 이 용이함을 확인하였다. 구축된 수치표고모델을 기반으로 3차원 모델을 구축하였고 토양복구사업의 면적 및 체적 등의 공간정보를 추출하였다. 그 결과 사업 결과모델 형성을 위한 추가적인 토양 적치 총량은 268,672 m3이며 약 71만 톤의 양에 해당하는 것을 확인하였다. 이는 무인항공기의 광해복구사 업 모니터링의 효율성을 증명하는 것으로 추후 보다 많은 활용도를 보일 것으로 사료된다.

Flight of an autonomous unmanned aerial vehicle (UAV) generally consists of four steps; take-off, ascent, descent, and finally landing. Among them, autonomous landing is a challenging task due to high risks and reliability problem. In case the landing site where the UAV is supposed to land is moving or oscillating, the situation becomes more unpredictable and it is far more difficult than landing on a stationary site. For these reasons, the accurate and precise control is required for an autonomous landing system of a UAV on top of a moving vehicle which is rolling or oscillating while moving. In this paper, a vision-only based landing algorithm using dynamic gimbal control is proposed. The conventional camera systems which are applied to the previous studies are fixed as downward facing or forward facing. The main disadvantage of these system is a narrow field of view (FOV). By controlling the gimbal to track the target dynamically, this problem can be ameliorated. Furthermore, the system helps the UAV follow the target faster than using only a fixed camera. With the artificial tag on a landing pad, the relative position and orientation of the UAV are acquired, and those estimated poses are used for gimbal control and UAV control for safe and stable landing on a moving vehicle. The outdoor experimental results show that this vision-based algorithm performs fairly well and can be applied to real situations.

Tried to photographing of aerial Image using unmanned aerial vehicle for applied to safety inspection on a large area or inaccessible. In result, 3D Spatial Information data were acquired, understand the overall terrain and coastline to based on data, compared to traditional aerial images and analyzed. Finally, identified the regions to requiring continuous monitoring by assessment of a disaster risk. We hoping to help build to continues data for identified the changing shape over time.

Emissions from aircraft have impacts on the air pollution of airport and the surrounding area. There are methods of emissions calculated as Tier 1, Tier2, Tier 3A and Tier 3B. Thus, this study investigated emissions from aircraft at the Gimhae International Airport using EDMS(Emissions & Dispersion Modeling System) program. Results of estimation from aviation emissions, Tier 3B considering all parts which can occur at the airport has the largest amount emissions. In order to understand the relation between aviation emissions and distribution of ozone concentration over airport area, numerical evaluation were carried out. Although the difference of surface ozone distribution between numerical assessment with and without aviation emissions was little, effects of air pollution at airport area from aviation emissions of NOx and VOCs.

The Global Positioning System (GPS) is widely used to aid the navigation of aerial vehicles. However, the GPS cannot be used indoors, so alternative navigation methods are needed to be developed for micro aerial vehicles (MAVs) flying in GPS-denied environments. In this paper, a real-time three-dimensional (3-D) indoor navigation system and closed-loop control of a quad-rotor aerial vehicle equipped with an inertial measurement unit (IMU) and a low-cost light detection and ranging (LIDAR) is presented. In order to estimate the pose of the vehicle equipped with the two-dimensional LIDAR, an octree-based grid map and Monte-Carlo Localization (MCL) are adopted. The navigation results using the MCL are then evaluated by making a comparison with a motion capture system. Finally, the results are used for closed-loop control in order to validate its positioning accuracy during procedures for stable hovering and waypoint-following.

In this study, sensitivity analysis to investigate the effect on analytical results of the aircraft impact analysis parameter for the nuclear power plant was carried out. Verification of the analytical model and method using the test results was performed. The eroding parameter of the Winfrith concrete material model in LS-Dyna and modelling method of the SC wall structure were studied. Finally, these results are to be used for the development of the structural safety evaluation procedure for the aircraft impact on the nuclear power plant.

According to NEI 07-13 R8, in aircraft impact analysis for new plant design, global structural damage of the target structure can be evaluated analytically using one of the following methods of evaluation: 1) Force time-history analysis method. 2) Missile-target interaction analysis method. It depends on the availability of data on the dynamic characteristics and the intended level of detail of analysis. The purpose of this study is to evaluate the effect on the analytical results of the aircraft impact analysis method. Several impact analyses using various method were performed for the simplified external SC wall of the APR+ nuclear power plant structure.

This study is carried out to propose an empirical equation which can promptly predict the aircraft noise level at a specific point (a receptor) near Jeju international airport by using the information of the flight path data. For this purpose, Analyses of multiple linear regression with the slant distances (SD) calculated from the gate analyses of the flight path data, aircraft noise certification levels with unit of EPNL(effective perceived noise level) and noise levels measured at receptors are performed by SPSS package. From these regression analyses for approach and departure of aircraft, we can propose empirical equations which is statistically significant. The noise levels predicted by these empirical equations are highly correlated the measured data.

최근 마무리된 4대강 살리기 사업 등의 여파로 하천 내 수리·수문현상의 많은 변화가 예상되고 있다. 하천지형정보는 하천관리를 위해 요구되는 다양한 하천 정보의 기초가 되며 하천 내 수리·수문현상을 이해하고 예측하는데 필수적인 자료이다. 기존의 하천지형정보 취득 기술은 많은 인력과 시간이 소요되는 노동집약적 기술에 머무르고 있어 광범위한 지역에 걸쳐 대규모로 진행된 하천 사업의 영향을 계측하고 관리하기에는 한계가 있다. 본 연구에서는 저수부 하상 측정에는 ADCP 센서를 장착한 무선조종 하천조사보트 (R2V2)를 이용하여 3차원 저수부 하상지형자료를 취득하였으며, 고수부 지형자료 취득에는 사진측량 장비를 장착한 무인항공기 (UAV)를 이용하였다. R2V2는 ADCP 센서와 RTK-GPS 모듈을 장착하여 실시간으로 하천 전단면에 대한 유속, 유량, 하상 등에 대한 자료를 측정할 수 있고, RTK-GPS를 이용하여 정밀한 위치측정이 가능한 장비이며, UAV는 저고도에서 촬영한 고해상도 항공사진과 자세보정장치 및 GPS를 이용하여 지형의 정밀한 고도와 평면좌표 측정이 가능한 장비이다. 서로 상이한 측정방법을 사용하는 두 측정 장비의 평면좌표와 고도측정의 기준을 일치시키기 위해 4대강 살리기 사업에서 설치한 측량기준점을 이용하여 정밀한 GPS 보정을 실시하고 보정된 GPS를 이용하여 측정 시점의 수위 측량을 실시하였다. 측정된 고수부 및 저수부의 지형정보와 3차원 지형정보 표출 소프트웨어를 이용하여 3차원 하천지형을 구성하였다. 구성된 3차원 하천지형으로 기존의 하천측량 방법으로는 구현할 수 없었던 단절부 없이 고수부와 저수부가 연결된 하천 종·횡단 정보를 추출할 수 있었으며 이는 하천을 유지·관리하고 시설물 등을 계획하는데 유용한 정보로 활용될 수 있을 것으로 판단된다. 본 연구에서 제시하고 있는 하천지형자료 취득 방법은 기존 하천 측정 방법에 비해 시간적, 경제적 효율성이 높아 하천재해 발생 시 긴급한 정보취득이 용이하며, 하천정보 취득이 주기를 짧게하여 신뢰도 높은 자료 제공이 가능해질 수 있을 것으로 판단된다.