• Proceedings of the Korean Society of Disaster Information Conference
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• 2023.11a
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• pp.43-44
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• 2023

항공기 사고시에 탑승객의 생존성을 제고하기 위한 방법으로 충돌/충격 전, 충격방지자세 Brace Position를 취하도록 하는 것이 전 세계 항공사의 공통적인 안전 매뉴얼이다. 해당 매뉴얼은 1980년대 미국 NTSB에서 항공기 사고를 조사하면서 생존 특성을 연구한 이후 처음 정형화 되었고 이후 현재까지 일반적으로 적용되고 있다. 그러나 허드슨강의 기적으로 불리는 2009년 1월 15일 US Airways 1549편의 비상착수 사고에서 항공기의 큰 구조적인 손상이 없었음에도 불구하고 탑승객 일부가 중상을 입는 결과를 초래하여 이를 계기로 기존의 충격방지자세 적절성을 재검토하여 개선하는 움직임이 있었다. 이에 관련 연구자료를 분석하여 국내 적용 방안을 살피고 또한 추가적인 개선방안을 제시하고자 한다.

• The Journal of the Korea institute of electronic communication sciences
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• v.11 no.1
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• pp.119-124
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• 2016

In this paper, we studied on MAC(Media Access Control) protocol for UAVs application. According to the number of UAVs, ground control station should control properly increased UAVs. So, we applied CSMA/CA that used in current civil aircraft to UAV communications and verified the applicability through comparison of throughput and delays of data with various message sizes, In the results, we confirmed applicability for UAVs MAC protocol.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.25 no.4
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• pp.83-90
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• 2017

Unmanned Aerial Vehicles(UAVs) require collision avoidance capabilities equivalent to the capabilities of manned aircraft to enter the airspace of manned aircraft. In the case of Visual Flight Rules of manned aircraft, collision avoidance is performed by 'See-and-Avoid' of pilots. To obtain those capabilities of UAVs named as 'Sense-and-Avoid', sensor-system-based intruder tracking and collision avoidance methods are required. In this study, a multi-sensor-based tracking, data fusion, and collision avoidance algorithm is designed by using a model-based design tool MATLAB/SIMULINK, and validations of the designed model and code using numerical simulations and processor-in-the-loop simulations are performed.

• Journal of Advanced Navigation Technology
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• v.16 no.1
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• pp.122-130
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• 2012

Airborne separation assurance is a key requirement for Free Flight. This paper is to propose autonomous flight algorithm, such as extended authority of delegation, efficiency of airspace issue to deal with the empirical solution for free flight, and to measure flight efficiency and conflict detection and resolution (CD&R) by utilizing flight performance data under the two circumstances of scenario with the modeling of proposed algorithm and potential field algorithm. The results show that the autonomous flight algorithm is superior to the potential field algorithm under the circumstances of free flight airspace in terms of algorithm performance, CD&R, and flight efficiency.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.14 no.4
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• pp.87-93
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• 2006

The black-tailed gull chicks, Larus crassirostris, recognize various adult voice signal base on the simple patterns. We investigated behavior change in black-tailed gull chicks through physical manipulation of mew call. They were playback in four situations differing in physical character: 1) frequency manipulation only, 2) duration manipulation only, 3) call intensity(dB) manipulation only, and 4) call interval manipulation only. We observed occurrence of different response of the chicks, which were categorized into two behaviors(hidden and return behavior). The manipulated frequency, duration, and intensity were directly correlated. The chicks exposed to only manipulated call interval(0.5, 1sec) made significantly more hidden and return behavior. Adult black-tailed gull only increased flight time on manipulated call interval. The results suggest that black-tailed gulls use short call interval for alarm signal. The analysis of alarm signal provides an important on basic study of bird strike.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.10
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• pp.1032-1037
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• 2008

The fuel tank systems of fixed wing and rotary wing aircrafts require the self-sealing and crash-worthiness for their survivability. For these requirements, the flexible composite fuel tank is generally used. In this study, the performance of the flexible composite fuel tank is investigated. The FE simulation includes the drop test of a fuel tank using MSC.DYTRAN. MSC.DYTRAN can provide the fluid-structure modeling of these test from Euler and Lagrange grids. Using MSC.DYTRAN, the finite element modeling of the test cube of the flexible fuel tank and its FE simulation are performed for various environments. The simulation results can show if the test cube satisfies the performance requirements of the fuel tank.

• Journal of Aerospace System Engineering
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• v.12 no.5
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• pp.24-31
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• 2018

The objectives of this study is to carry out Bird strike analysis and tests of a blade antenna of aircraft. FEMs (Finite Element Models) were created for the analysis, while dummy and real antennas were used for the bird strike tests. In the analysis, birds were modeled with SPH (Smooth Particle Hydrodynamics) method, and the behaviors of the bird, antenna, and joint structure between antenna and aircraft fuselage were simulated with the FSI (Fluid-Structure Interaction) method. After the bird strike test was performed, the results of the analysis and test showed that they had a positive relationship. The damage of antenna and bolted joint was checked, and the structural integrity of the airframe was proved.

• Aerospace Industry
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• v.69
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• pp.48-51
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• 1999

이미 10여년 전의 일이지만 공항 관제사와 조종사간의 의사소통에 문제가 있어 항공기 충돌사고를 야기한 일이 있었다. 대서양 한가운데 있는 스페인령 카나리아군도는 7개 섬으로 되어 있는데 그중 주섬인 그랑 카나리아 섬에는 라스팔마스라는 어업기지와 휴양지가 있다.

• Computational Structural Engineering
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• v.25 no.3
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• pp.32-42
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• 2012

• Proceedings of the Korean Nuclear Society Conference
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• 2003.05a
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• pp.400-400
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• 2003