• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.49 no.1
• /
• pp.63-73
• /
• 2021

This paper presents a algorithm for automatic target recognition robust to the influence of the flame in order to track the target by EOTS(Electro-Optical Targeting System) equipped on UAV(Unmanned Aerial Vehicle) when there is aerial target or marine target with flame at the same time. The proposed method converts infrared images of targets and flames into a gradient vector field, and applies each gradient magnitude to a polynomial curve fitting technique to extract polynomial coefficients, and learns them in a shallow neural network model to automatically recognize targets and flames. The performance of the proposed technique was confirmed by utilizing the various infrared image database of the target and flame. Using this algorithm, it can be applied to areas where collision avoidance, forest fire detection, automatic detection and recognition of targets in the air and sea during automatic flight of unmanned aircraft.

• The Korean Journal of Air & Space Law and Policy
• /
• v.35 no.1
• /
• pp.103-125
• /
• 2020

This paper reviews the EU Case, Claudia Wegener v. Royal Air Maroc SA [2018] ECLI:EU:C:2018:361, Case C-537/17. It analyzes some issues as to Wegener case by examining EU Regulations and practical point of views. Article 3(1)(a) of Regulation (EC) No 261/2004 of the European Parliament and of the Council of 11 February 2004 establishing common rules on compensation and assistance to passengers in the event of denied boarding and of cancellation or long delay of flights, entitled scope, provides: "this Regulation shall apply: (a) to passengers departing from an airport located in the territory of a Member State to which the Treaty applies; (b) to passengers departing from an airport located in a third country to an airport situated in the territory of a Member State to which the Treaty applies, unless they received benefits or compensation and were given assistance in that third country, if the operating air carrier of the flight concerned is a Community carrier." ECJ held that must be interpreted as meaning that Regulation (EC) No 261/2004 applies to a passenger transport effected under a single booking and comprising, between its departure from an airport situated in the territory of a Member State and its arrival at an airport situated in the territory of a third State, a scheduled stopover outside the European Union with a change of aircraft. According to the Court, it is apparent from the regulation and case-law that when, as in the present case, two (or more) flights are booked as a single unit, those flights constitute a whole for the purposes of the right to compensation for passengers. Those flights must therefore be considered as one and the same connecting flight.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.50 no.7
• /
• pp.445-454
• /
• 2022

Ice accretion on the aircraft components, such as wings, fuselage, and empennage, can occur when the aircraft encounters a cloud zone with high humidity and low temperature. The prevention of ice accretion is important because it causes a decrease in the aerodynamic performance and flight stability, thus leading to fatal safety problems. In this study, a shape design optimization of a multi-element airfoil is performed to minimize the amount of ice accretion on the high-lift device including leading-edge slat, main element, and trailing-edge flap. The design optimization framework proposed in this paper consists of four major parts: air flow, droplet impingement and ice accretion simulations and gradient-free optimization algorithm. Reynolds-averaged Navier-Stokes (RANS) simulation is used to predict the aerodynamic performance and flow field around the multi-element airfoil at the angle of attack 8°. Droplet impingement and ice accretion simulations are conducted using the multi-physics computational analysis tool. The objective function is to minimize the total mass of ice accretion and the design variables are the deflection angle, gap, and overhang of the flap and slat. Kriging surrogate model is used to construct the response surface, providing rapid approximations of time-consuming function evaluation, and genetic algorithm is employed to find the optimal solution. As a result of optimization, the total mass of ice accretion on the optimized multielement airfoil is reduced by about 8% compared to the baseline configuration.

• Aerospace Engineering and Technology
• /
• v.2 no.2
• /
• pp.179-185
• /
• 2003

In this study, considerations for establishing RVSM airspace and requirements for RVSM operating aircraft are verified. The purpose of RVSM is to reduce vertical separation minimum for aircraft which operate between FL290~FL410 inclusive in regional airspace, and to increase airspace capacity by providing additional flight levels. To introduce RVSM, it is necessary to estimate quantatively airborne collision risk due to the reduction in vertical separation minimum. Aircraft operating through RVSM airspace is required to verify that height keeping performance is above specific standards.

• Proceedings of KOSOMES biannual meeting
• /
• 2005.11a
• /
• pp.85-90
• /
• 2005

이 연구에서는 대형위그선 개발에 따른 운항요원의 양성 방향에 관한 기초 연구를 수행하였다. 국제해사기구(IMO)는 2002년 12월 제76차 해사안전위원회에서 기존의 선박과 동일한 위그선의 충돌 회피규정 등 안전운항에 관한 잠정적인 가이드라인을 제정하였고, 지난 2005년 5월에는 위그선 운항요원의 운항지식, 운항기술 및 교육훈련 사항 등에 대한 가이드라인을 제시하였다. 위그선은 선박과 항공기의 복합형태인 새로운 운송수단임을 고려한 양성 교육과정 준비가 필요하다. 우리나라는 세계 최고의 조선 인프라와 기술력을 확보하여 대형위그선 건조는 기술적으로 실현가능할 뿐만 아니라 차세대 해상 수송혁신을 주도할 수 있다고 한다. 또한 최근 적재량 100톤급 대형위그선 실용화 사업이 해양수산부를 중심으로 순조롭게 추진되고 있다. 따라서 양 해양대학은 대형위그선 개발 시점에 맞춰 운항요원 양성을 통한 신규분야에 대한 블루오션 창출이라는 목표를 갖고 종합적인 연구와 체계적인 준비가 절실히 요구된다.

• Journal of the Korea Institute of Military Science and Technology
• /
• v.4 no.2
• /
• pp.249-255
• /
• 2001

무인자율항체는 자동차, 선박, 잠수함과 같이 인간에 의해 직접 조종되는 유인항체에 인간의 역할을 대신할 수 있는 지능시스템을 배치하여 전체적 혹은 부분적으로 무인화한 이동체를 말한다. 무인자율항체에서 사용되는 소프트웨어는 인식, 사고, 행위와 같은 인간의 지적능력을 내포한 인공지능시스템이어야 한다. 자율무인잠수정, 자율운항선박과 같은 저속무인자율항체는 무인항공기나 무인차량과 같이 빠른 판단과 제어가 요구되는 지능제어시스템과는 다른 특성을 가진다. 저속무인자율항체에서 가장 주목되는 특성은 주위 환경 변화속도와 운항속도에 따른 긴박감의 차이이다. 고속자율항체에서는 제어시스템의 처리속도에, 저속자율항체에서는 제어시스템의 신뢰성에 비중을 둔다. 본 연구에서는 이와 같은 저속무인자율항체의 특성과 기능별 독립성 보장, 반응형 및 인식형 인공지능 기법의 융화 극대화에 촛점을 맞춘 RVC(Reactive Layer - Virtual World - Considerative Layer) 지능시스템 모델을 소개한다.

• Computational Structural Engineering
• /
• v.1 no.2
• /
• pp.26-33
• /
• 1988

유한요소해석프로그램들의 적용대상이 최근들어 다(多) 자유도의 비선형문제로 확대됨에 따라 컴퓨터의 계산속도가 특히 중요한 제한조건으로 대두되기 시작하였으며 금속성형해석, 자동차 등의 충돌해석(자유도가 2만-6만), 토질 및 콘크리트 등의 점소성해석과 더불어 항공기, 터빈 등의 열응력해석 및 동적해석 등에 있어서는 막대한 계산시간으로 인하여 해석의 효율성에 대한 문제가 제기되고 있다. 따라서 슈퍼컴퓨터를 포함하여 고속연산기능을 가진 병렬처리컴퓨터를 이용하여 유한요소해석을 수행하여야 할 필요성이 증가하고 있다. 88년 9월중에 한국과학기술원 시스템공학센터에 현존하는 슈퍼컴퓨터중 최상위 성능을 가진 CRAY2S가 설치됨에 따라 국내에도 슈퍼컴퓨터시대가 열리게 되었으며 따라서 본 고에서는 CRAY2S의 시스템개요 및 응용소프트웨어에 대하여 소개하고 슈퍼컴퓨터를 이용한 유한요소해석에 관하여 간략히 기술하고저 한다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
• /
• 2014.10a
• /
• pp.21-22
• /
• 2014

VDR은 IMO의 협약에 따라 요구되는 모든 선박의 데이터를 기록하는 장비이다. 2002년 7월 1일 이후 건조되는여객선과 3,000톤 이상의 여객선을 제외한 모든 선박을 VDR를 탑재하여야 한다. 이것은 항공기의 블랙박스와 같이 사고조사를 가능하게 한다. 이 논문에서는 VDR을 이용한 선박의 거동 특성에 대하여 실선 M/S WS 선박을 대상으로 실시하기로 한다. 이 선박은 2014년 1월 여천에 있는 GS 칼텍스 터미널 부두와 충돌하여 상당량의 기름을 유출시킨 바 있다. 이 논문에서는 어느 쪽 타각을 더 많이 사용하였는지를 알기 위하기 위하여 타각면적을 도입하였다 그 외에 평균 선수방위, 평균속력, 평균 rpm 등을 사용하였다. 이 결과 이 선박은 우현타각을 많이 사용하는 것으로 나타났고 이것은 이 선박이 좌선회하는 경향이 있음을 확인할 수 있다.

• Transactions of the Korean Society of Pressure Vessels and Piping
• /
• v.18 no.2
• /
• pp.50-53
• /
• 2022

To investigate the validity of the finite element analysis program to assess structural integrity of a spent nuclear fuel transport cask subjected to extreme impact loads, structural integrity of the cask for the case of an aircraft engine collision is evaluated using three FE analysis programs: Autodyn, Speed and ABAQUS explicit version. As a result of all analyses, it is confirmed that no penetration occurred in the cask wall. Even though the different programs are used, it is identified that there are insignificant differences in the FE analysis variables such as von Mises effective stress and equivalent plastic strain among the programs.

• Journal of Advanced Navigation Technology
• /
• v.27 no.6
• /
• pp.710-715
• /
• 2023

Urbanization brings many challenges such as traffic, housing, and environment. To solve these problems, researchers are working on new transportation systems like urban air mobility (UAM). UAM aircraft should fly safely without burdening the existing air traffic system in the early stage of low-density operation. The airspace should also be managed and operated efficiently. Therefore it is important to make urban air traffic predictable by using corridors and collecting data on low-density operations in the early stage. For this purpose various simulations are needed before operation to create scenarios that estimate potential collisions between UAM aircraft and to evaluate the risks of aircraft spacing, loss of separation (LoS), and near mid air collision (NMAC). This paper focuses on identifying the requirements and considerations for setting separation standards for urban air traffic based on the results of studies.