• 제목/요약/키워드: Altitude training

검색결과 47건 처리시간 0.029초

야간산불진화 헬기 운영과 항공안전 (Night fire fighting helicopters operations and Aviation Safety)

  • 최연철
    • 한국항공운항학회지
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    • 제22권1호
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    • pp.145-151
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    • 2014
  • Not only in Korea, but also in other countries, most helicopter accidents occur at low altitude. Analysis on accidents data collected both in Korea and other countries has brought two conclusions. Firstly, helicopter operations during the night hours carries a high risk. Secondly, the most common cause of night hour operations is loss of control due to the flight illusion. As an operation relying on a night vision in particular has a very high accident hazard, accompanying instruments such as NVG are ought to be provided. Hence, a thorough preparation and inspection on missions for night forest fire extinguishing should be required and perfect guidelines/road maps and enough training programs for the operation should be provided before the engagement in missions.

A Review of Safety and Quality Issues in the Construction Industry

  • Ogwueleka, Amaka Chinweude
    • Journal of Construction Engineering and Project Management
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    • 제3권3호
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    • pp.42-48
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    • 2013
  • Construction industry is considered as the most hazardous industry due to its unique nature. Safety and quality management are essential to control hazards and improve success in project implementation. This paper focuses on evaluating the crucial factors influencing safety and quality management in construction projects. In order to achieve this, the qualitative and quantitative approaches were used for data collection. The findings of this study reveal the crucial safety factors as management commitment, safety awareness of top management practices/ procedures/ reviews, and errors in judgement or carelessness. Project supervision, employee involvement/ altitude, and expertise knowledge/ training were considered as the crucial quality factors influencing safety and quality management. The study shows that safety and quality issues cannot be overlooked therefore proper implementation is paramount to achieve project success.

남부지역 졸참나무의 임분 특성에 따른 물리·역학적 특성 (Physical and Mechanical Properties of Quercus serrata according to Stand Characteristics in Southern Region of Korea)

  • 원경록;홍남의;이광수;정수영;유병오;박용배;정성호;변희섭
    • Journal of the Korean Wood Science and Technology
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    • 제42권6호
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    • pp.659-665
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    • 2014
  • 목재의 조직, 물리, 역학적 특성은 토양조건과 기후변화 등의 환경적 인자에 의해서도 바뀌게 됨으로 남부 세 지역의 임분 특성이 목재의 재질특성에 미치는 영향과 지역별 조직, 물리, 역학적 특성 등을 비교 검토하였다. 경상도, 전라도, 제주도의 졸참나무임지에 대해 임분 특성과 목재특성을 평가 분석하였는데 이들 간에는 대부분 높은 상관관계가 나타났다. 남부지역의 졸참나무는 온대에서 난대로 기후가 변화하는 난대 지역의 산림자원으로 본 목재재질특성 분석결과 유용한 산림자원으로 활용할 수 있을 것으로 생각된다.

Application of Statistical and Machine Learning Techniques for Habitat Potential Mapping of Siberian Roe Deer in South Korea

  • Lee, Saro;Rezaie, Fatemeh
    • Proceedings of the National Institute of Ecology of the Republic of Korea
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    • 제2권1호
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    • pp.1-14
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    • 2021
  • The study has been carried out with an objective to prepare Siberian roe deer habitat potential maps in South Korea based on three geographic information system-based models including frequency ratio (FR) as a bivariate statistical approach as well as convolutional neural network (CNN) and long short-term memory (LSTM) as machine learning algorithms. According to field observations, 741 locations were reported as roe deer's habitat preferences. The dataset were divided with a proportion of 70:30 for constructing models and validation purposes. Through FR model, a total of 10 influential factors were opted for the modelling process, namely altitude, valley depth, slope height, topographic position index (TPI), topographic wetness index (TWI), normalized difference water index, drainage density, road density, radar intensity, and morphological feature. The results of variable importance analysis determined that TPI, TWI, altitude and valley depth have higher impact on predicting. Furthermore, the area under the receiver operating characteristic (ROC) curve was applied to assess the prediction accuracies of three models. The results showed that all the models almost have similar performances, but LSTM model had relatively higher prediction ability in comparison to FR and CNN models with the accuracy of 76% and 73% during the training and validation process. The obtained map of LSTM model was categorized into five classes of potentiality including very low, low, moderate, high and very high with proportions of 19.70%, 19.81%, 19.31%, 19.86%, and 21.31%, respectively. The resultant potential maps may be valuable to monitor and preserve the Siberian roe deer habitats.

Support Vector Machine을 이용한 선에코 특성 분석 및 탐지 방법 (Analysis and Detection Method for Line-shaped Echoes using Support Vector Machine)

  • 이한수;김은경;김성신
    • 한국지능시스템학회논문지
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    • 제24권6호
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    • pp.665-670
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    • 2014
  • SVM은 학습 데이터를 두 개의 집단으로 분리시키는 최적의 초평면을 찾는 이진 분류기로서 우수한 성능 때문에 다양한 분야에서 귀납 추론, 이진 분류, 예측 등을 목적으로 사용되는 알고리즘이다. 또한 대표적인 블랙박스 모델 중 하나이기 때문에 학습 후 생성되는 SVM의 해석에 대한 연구도 활발히 진행되고 있다. 본 논문에서는 SVM 알고리즘을 이용하여 기상 레이더의 데이터 내에 비교적 높은 빈도로 발생하여 기상 예보의 정확도를 감소시키는 비강수에코 중 하나인 선에코를 자동으로 탐지하는 방법에 대한 연구를 수행하였다. 학습 데이터로는 평균 반사도, 크기, 발생 형태, 중심 고도 등과 같은 특성을 활용하였는데, 이는 기상 레이더 데이터에 저장된 다양한 데이터 중 반사도 값을 선택한 후 클러스터링 기법을 통해 추출한 것이다. 이와 같이 학습된 SVM 분류기를 실제 사례를 바탕으로 하여 검증하였으며, Decision Tree 알고리즘을 적용하여 생성한 분류기의 해석을 수행하였다.

Application of neural network for airship take-off and landing system by buoyancy change

  • Chang, Yong-Jin;Woo, Gui-Aee;Kim, Jong-Kwon;Cho, Kyeum-Rae
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2003년도 ICCAS
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    • pp.333-336
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    • 2003
  • For long time, the takeoff and landing control of airship was worked by human handling. With the development of the autonomous control system, the exact controls during the takeoff and landing were required and lots of methods and algorithms were suggested. This paper presents the result of airship take-off and landing by buoyancy control using air ballonet volume change and performance control of pitch angle for stable flight within the desired altitude. For the complexity of airship's dynamics, firstly, simple PID controller was applied. Due to the various atmospheric conditions, this controller didn’t give satisfactory results. Therefore, new control method was designed to reduce rapidly the error between designed trajectory and actual trajectory by learning algorithm using an artificial neural network. Generally, ANN has various weaknesses such as large training time, selection of neuron and hidden layer numbers required to deal with complex problem. To overcome these drawbacks, in this paper, the RBFN (radial basis function network) controller developed.

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GIS-based Landslide Susceptibility Mapping of Bhotang, Nepal using Frequency Ratio and Statistical Index Methods

  • Acharya, Tri Dev;Yang, In Tae;Lee, Dong Ha
    • 한국측량학회지
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    • 제35권5호
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    • pp.357-364
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    • 2017
  • The purpose of the study is to develop and validate landslide susceptibility map of Bhotang village development committee, Nepal using FR (Frequency Ration) and SI (Statistical Index) methods. For the purpose, firstly, a landslide inventory map was constructed based on mainly high resolution satellite images available in Google Earth Pro, and rest fieldwork as verification. Secondly, ten conditioning factors of landslide occurrence, namely: altitude, slope, aspect, mean topographic wetness index, landcover, normalized difference vegetation index, dominant soil, distance to river, distance to lineaments and rainfall, were derived and used for the development of landslide susceptibility map in GIS (Geographic Information System) environment. The landslide inventory of total 116 landslides was divided randomly such that 70% were used for training and remaining 30% for validating result by receiver operating characteristics curve analysis. The area under the curve were found to be greater than 0.7 indicating an acceptable susceptibility maps obtained using FR and SI methods in GIS for hilly region of Nepal.

Launch and Early Orbit Phase Simulations by using the KOMPSAT Simulator

  • Lee, Sanguk;Park, Wan-Sik;Lee, Byoung-sun;Lee, Ho-Jin;Park, Hanjun
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1999년도 제14차 학술회의논문집
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    • pp.33-36
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    • 1999
  • The KOMPSAT, which is scheduled to be launched by Taurus launch vehicle in late November of 1999, will be in a sun-synchronous orbit with an altitude of 685km, eccentricity of 0.001, inclination of 98deg and local time of ascending node of 10:50 a.m. Electronics and Telecommunications Research Institute and Daewoo Heavy Industry had jointly developed a KOMPSAT Simulator as a component of the KOMPSAT Mission Control Element. The MCE had been delivered to Korea Aerospace Research Institute for the KOMPSAT ground operation. It is being used for training of KOMPSAT ground station personnel. Each of satellite subsystems and space environment were mathematically modeled in the simulator. To verify the overall function of KOMPSAT simulator, a Launch and Early Orbit Phase(LEOP) operation simulations have been performed. The simulator had been verified through various tests such as functional level test, subsystem test, interface test, system test, and acceptance test. In this paper, simulation results for LEOP operations to verify flight software adapted into simulator, satellite subsystem models and environment models are presented.

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수치지형정보를 애용한 지형의 3차원 표현 software 개발 (Development of the Three Dimensional Landform Display Software Using the Digital Terrain Model)

  • 이규석
    • 한국조경학회지
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    • 제17권3호
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    • pp.1-8
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    • 1990
  • The digital terrain model (DTM) or digital elevation model (DEM) is commonly used in representing the continuous variation of relief over space. One of the most frequent applications is to display the three dimensional view of the landform concerned. In this paper, the altitude matrices-regular grid cell format of the elevation in Mt. Kyeryong National Park were used in developing the three dimensional view software for the first time in Korea. It required the removal of hidden lines or surfaces. To do this, it was necessary to identify those surfaces and line segments that are visible and those that are invisible. Then, only the visible portions of the landform were displayed. The assumption that line segments are used to approximate contour surfaces by polygons was used in developing the three dimensional orthographic view. In order to remove hidden lines, the visibility test and masking algorithms were used. The software was developed in the engineering workstation, SUN 3/280 at the Institute of Space Science and Astronomy using 'C' in UNIX operating system. The software developed in this paper can be used in various fields. Some of them are as follows : (1) Landscape design and planning for identifying viewshed area(line of sight maps) (2) For planning the route selection and the facility location (3) Flight simulation for pilot training (4) Other landscape planning or civil engineering purposes

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항공기 비정상 자세 사고의 TEM 분류 및 UPRT 향상에 관한 연구 (Analysis of Aircraft Upset through TEM and Improvement of UPRT)

  • 최진국;전승준
    • 한국콘텐츠학회논문지
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    • 제19권11호
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    • pp.365-374
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    • 2019
  • 항공운항사고율은 항공기 비정상 자세(Upset)로 인한 조종능력상실(LOC-­I: Loss of Control in Flight)이 가장 높아 ICAO(International Civil Aviation Organization: 국제민간항공기구)는 TEM(Threat and Error Management)을 활용하여 비정상자세 예방 및 회복훈련(UPRT: Upset Prevention & Recovery Training)을 하도록 권고하였다. 그러나 전 세계적으로 항공기 비정상 자세에 관한 TEM 요인 연구가 많이 도출되지 않은 관계로 항공사들이 실질적인 TEM 훈련에 참고할 자료가 많지 않은 실정이다. 본 연구의 목적은 UPRT의 소개와 항공기 비정상 자세로 인한 대표적 사고 3건을 ICAO에서 권고하는 TEM으로 분류하여 핵심요소인 위협과 에러, 불안전항공기 상태의 공통요인을 도출하여 살펴보는 것이다. 본 논문에서 대표적인 비정상자세 사고를 TEM을 활용하여 분류한 결과 공통위협으로는 야간비행/IFR, 자동화 놀람, 부적절한 훈련과 미숙련 부기장 편조로 나타났다. 공통 에러로는 부적절한 엔진 추력, 절차적용오류, 조종, 속도이탈 및 고도 이탈, 의사소통실패, 항공기 이상자세, 복창실패, 크로스 체크 실패 등으로 나타났으며, 불안전항공기 상태로는 부적절한 자동화 모드, 저속이탈, 수직 이탈, 부정확한 엔진 추력 등으로 실속하여 추락한 것으로 나타났다. 또한 공통요인으로부터 개선방향을 도출하여 본 연구는 시작단계에 있는 TEM활용 Upset 향상 방안을 제시하고자 한다.