• 한국항공운항학회:학술대회논문집
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• 2015.11a
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• pp.144-147
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• 2015

외부이물질에 의한 손상(FOD)으로 인해 항공기 및 엔진 등의 원상복구를 위한 비용손실 뿐만 아니라 항공기 안전운항에 큰 위협요인으로 부각되고 있다. 그러나 우리나라 FOD와 관련 된 연구 실태는 엔진부품, 타이어, 기체 및 조류충돌에 의한 사건사고에 대한 통계분석 등이 주를 이루고 있으며, 잠재적으로 FOD를 유발할 수 있는 항공기를 정비하고 취급하는 정비사 및 지상 조업직원 등의 인적요인을 고려한 연구는 전무한 실정이다. 이에 본 연구에서는 FOD의 정의와 발생 원인들을 살펴보고, 항공정비사를 비롯한 지상 조업직원들의 인적요인에 의한 FOD 유발가능성 등을 연구하여 FOD방지를 위한 개선 방안을 제시하고자 한다.

• 한국항공운항학회:학술대회논문집
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• 2015.11a
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• pp.83-87
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• 2015

미국 국방부에서 군사용으로 사용되던 수 GHz 대역의 초 광대역 주파수 스펙트럼을 미국연방통신위원회(FCC)에서 민간에 개방하면서 여러 활용 기술이 개발 되고 있다. 소비전력이 적고, 고속통신 및 방해 전파에 강하다는 특성을 갖고 있으며 또한 작은 위치 검출 오차로 정밀도가 높으나 거리가 길어지면 급속도록 떨어지는 속도로 인하여 근거리 통신으로 활용 검토 되고 있다. 따라서 공항 및 항공기내 지역에서 초 광대역 주파수 특성을 활용하여 적용 가능한 항공기 익단충돌방지시스템, 항공기와 고속 데이터 전송, 항공기 내의 무선 백본 시스템 활용 및 공항 지역의 이동체 위치 정보 관리 등 다양한 항공 서비스 업무에 적용 가능함을 알 수 있었다.

• 한국항공운항학회:학술대회논문집
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• 2005.11a
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• pp.146-150
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• 2005

• Proceedings of the Korean Radioactive Waste Society Conference
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• 2009.11a
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• pp.461-462
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• 2009

• Journal of Aerospace System Engineering
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• v.15 no.5
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• pp.106-112
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• 2021

In this study, we performed a design and structural analysis of a blade-shaped antenna installation on the rear fuselage of a rotary wing aircraft operated by the military. When the structure is damaged while the aircraft is in operation, it is separated from the aircraft main structure and may collide with the rotor or blades to cause the aircraft to crash. Therefore, structural safety for the modified structure must be secured. The design requirement for the newly installed modified part were established, and the load condition was constructed by applying the load that may occur in the aircraft after the modification. Structure safety for the modified structure was secured by performing structure analysis. To analysis stress and deformation of aircraft structure, we developed finite element model and verified it by using hand calculation method. We confirmed the safety of the modified structure through the final structural integrity analysis.

• Journal of Advanced Navigation Technology
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• v.26 no.2
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• pp.47-53
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• 2022

With the recent development of defense technology, various aircraft armaments/equipments are being developed. Among them, cruise guided weapons(missile) for launching aircraft can be installed on aircraft aftersecuring reliability and safety through varioustests. In order to avoid collision with aircraft, missile separated from aircraft must release restraint of wing at the specified time, control wing in the specified direction. In order to confirm this, a test system that can control MIL-STD-1760 according to safety separation procedure and verify release performance is required. test system needs a function to check circuit for release of restraints and a function to check driving performance by controlling MIL-STD-1760. In addition, test system should be simulate environment separated from aircraft. This paper presented a testsystemthat can verify circuit and driving performance mounted on missile according to the safety separation procedure, and it was confirmed that it was normally separated from aircraft through flight tests.

• Proceedings of the Korean Society of Computer Information Conference
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• 2012.01a
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• pp.49-50
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• 2012

본 논문에서는 다수의 소형 무인 항공기(UAV) 그룹이 이동 중 장애물을 만났을 때 장애물과의 충돌을 방지하는 효율적인 장애물 회피 정책을 제안한다. 이 정책은 무선 에드혹(moblie ad hoc) 네트워크를 기반으로 단순히 UAV 간의 충돌 회피 뿐만이 아니라 UAV 그룹이 이동하는 도중 장애물을 발견 하였을 경우 장애물을 효율적으로 회피하는 방법과 연결성이 손실되는 경우에 대처하는 방안도 고려하였다. 제안하는 정책은 UAV가 장애물을 포착 하였을 때 현재 이동 속도를 유지한 채 장애물을 기준으로 UAV 그룹을 2개의 그룹으로 분리하여 장애물을 회피 한 후 일정한 지점에서 모여 다시 각 UAV간의 연결성을 유지한 채 목표물을 향해 이동하는 정책을 제안한다.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.17 no.4
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• pp.85-93
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• 2009

Bird strike is big issue in aviation. Because a bird strike causes not only an aircraft damage but also a fatality, aviation societies are gearing up to prevent a bird strike. However, the accidents is not going down yet. Annal average of bird strikes in Korea is 1.15 accidents per ten thousand of flight, which is lower than the other country, for example 1.84 accidents in France and 2.38 accidents in Switzerland, 1.15 accidents. In the U.S.A, there are 89,727 accidents for the 19 year(1990-2008). Also flight delay is total 637,692 hours. The cost is total 350,258 billion dollar and 18,435 billion dollar per year. In related with those data's, this research is about the current and legal status of the bird strike. Also it will be useful to establish aviation safety policy and manage the bird strike.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.1
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• pp.81-88
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• 2020

Flight data recorder is a equipment that records data required for investigation of aircraft accidents and should be developed in compliance with the ED-112A standard. Unlike general data storage device, flight data recorder must be able to recover data after an aircraft accident, requiring a housing and a memory board to protect data in extreme environments. To attain this performance, we designed a housing that can withstand the test by analyzing the physical environment of the impact, shear/tensile, penetration resistance and static crush test of the crash survival test and minimized the size and weight compared to the existing one in consideration of the installation of the aircraft in this paper. Insulation material and thermal block material were applied to endure high and low temperature fire so that the internal temperature does not rise above 150℃ even in 260℃, 10 hour environment. In addition, the memory board is designed to minimize the size and we devise a hoping programming method to prevent continuous data loss of more than 16 seconds. Through this, Crash protected memory module that satisfies ED-112A was completed.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.50 no.11
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• pp.763-770
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• 2022

In an environment where multiple drones are operated, collisions can occur when path points overlap, and collision avoidance in preparation for this is essential. When multiple drones perform multiple tasks, it is not appropriate to use a method to generate a collision-avoiding path in the path planning phase because the path of the drone is complex and there are too many collision prediction points. In this paper, we generate a path through a commonly used path generation algorithm and propose a collision avoidance method using speed profile optimization from that path segment. The safe distance between drones was considered at the expected point of collision between paths of drones, and it was designed to assign a speed profile to the path segment. The optimization problem was defined by setting the distance between drones as variables in the flight time equation. We constructed the constraints through linearize and convexification, and compared the computation time of SQP and convex optimization method in multiple drone operating environments. Finally, we confirmed whether the results of performing convex optimization in the 20 drone operating environments were suitable for the multiple drone operating system proposed in this study.