• 한국항행학회논문지
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• 제24권6호
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• pp.515-520
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• 2020

오늘날 항공기 항행에 있어서 자동조종장치와 FMS (flight management system)의 발전은 조종사들의 작업량감소와 항행 안전유지에 그 성과가 크다고 할 수 있다. 특히 공항의 교통량이 많거나 표준계기 출발 절차 (SID; standard instrument departure)가 복잡한 항행의 경우에 자동조종장치와 FMS 장비의 효과는 더욱 크다. 하지만 일부 공항의 특정한 출발 절차에서 FMS의 오류로 인한 uncommanded turn 이벤트가 발생하여, 항공기가 항로의 중심선에서 벗어나는 경우가 있다. 대부분의 출발 절차가 RNAV(area navigation) 운영이 요구됨으로, 조종사의 상황인식과 수정 조작이 항로 편차(deviation)를 최소화하여, RNAV의 안전을 유지하는 유일한 방법이다. 이와 관련하여 uncommanded turn 이벤트의 국내외 발생 현황을 기종별, 공항별, 비행 단계별로 조사하고 항공사의 uncommanded turn 이벤트 경감방안 분석을 통해 해당 이벤트의 더욱 근본적인 재발 방지대책 마련의 필요성 및 시사점을 도출하고자 한다.

• 항공우주기술
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• 제4권1호
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• pp.247-259
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• 2005

자연대기 전기의 항공기에 대한 상호 작용은 비행안전 상에 많은 문제를 초래하고 있다. 상용 항공기는 년간 1회 이상의 낙뢰를 맞는 것으로 보고되고 있으며 낙뢰는 항공기의 운항안전에 큰 위협이 되고 있다. 낙뢰 유도 전압은 항공기 전기․전자장비의 기능 장애 또는 손상을 가져다 주는 데 이것을 낙뢰의 간접영향이라 한다. 이러한 항공기의 낙뢰 간접영향으로부터 항공전자장비를 보호하기 위해서는 항공기에 대한 낙뢰의 영향과 항공기 내부 시스템을 분석하고 해당 부품에 대한 위협 내용에 대한 보호 설계를 통해 달성한다.

• 산업공학
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• 제25권4호
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• pp.472-479
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• 2012

Before an aircraft is delivered to customers, manufacturers have to verify required reliability for the aircraft. In usual, reliability of electronic equipments in military aircraft are predicted based on MIL-HDBK-217. But the specification has not been revised since 1995. Some alternatives including SR-332 and 217PLUS are suggested in this study. The processes and methods specified in MIL-HDBK-217 are compared with those of SR-332. Additionally, the predicted reliability of aircraft electronic equipment between usage data and field data are investigated using MIL-HDBK-217. The results show that predicted reliability of MIL-HDBK-217 is more conservative (underestimated) than that of usage data and field data.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 추계학술발표대회 논문집
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• pp.215-218
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• 2005

In this research, design scheme of fiber Bragg grating(FBG) sensor system for aircraft application is suggested from the results and the know-how from the fon11er researches on structural health monitoring techniques using fiber optic sensors. Design factors to be taken into consideration were derived for both sensor parts including connection and system parts. For the stability of FBG sensor system, design requirements of temperature, vibration, humidity, electromagnetic interference were presented from U. S. military standards. The direction of software programming which increases stability and perfon11ance of the aircraft with the FBG sensor system was also examined.

• 항공우주시스템공학회지
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• 제12권2호
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• pp.59-65
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• 2018

항공기 구성품인 착륙장치 핸들은 항공기 이 착륙 시 착륙장치 작동을 위한 핵심적인 장비이다. 착륙장치 핸들의 개발을 위한 진동시험 중 착륙장치 핸들 내부의 브라켓 파손 현상이 발생하였다. 따라서 본 논문에서는 착륙장치 핸들 개발 시 수행한 진동시험 절차와 진동시험 중 발생한 결함사항에 대한 원인 분석, 설계 개선사항 그리고 검증 결과를 함께 기술하였다.

• 한국항해항만학회지
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• 제44권2호
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• pp.65-72
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• 2020

Mankind has been using ships for more than 5,000 years and has developed a range of related technologies. However, despite such a long history, compared to aircraft with a history of approximately one century, the pace of progress has been markedly slow. Even though technological progress of ships or the installation of various navigation equipment have been achieved, seaborne collisions have occurred quite frequently. This study analyzed the TCAS( Traffic Collision Avoidance System) that has contributed to the prevention of collisions with other transport methods including aircraft to suggest a collision avoidance system that can be deployed for ships. To apply the technologies applied to aircraft that move in 3D to ships that move in 2D, the difference in the operational environment between the two modes was analyzed to identify elements that need to be applied to ships. The suggested display of data on the collision prevention system is one that manipulates the augmented reality display device used in automobiles that over the past few years has undergone rapid development. Based on the presentation of technological elements that need to be considered when adopting the SCAS or the Seaborne Collision Avoidance System as suggested in this study, the authors hope to contribute to the prevention of collisions.

• 한국군사과학기술학회지
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• 제16권1호
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• pp.74-80
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• 2013

In this paper, we have proposed a vapor cycle refrigeration system as a cooling system to provide cooling air to the aircraft external reconnaissance stores. In the proposed vapor cycle system, receiver which prevents refrigerant from subcooling was eliminated and thermal expansion valve was replaced with electronic expansion valve. The vapor cycle refrigeration system is aimed to provide cooling air to the reconnaissance stores which is added to the aircraft in the form of external store. The wide temperature range of ambient air from the flight conditions can decrease the cooling performance and can make the refrigeration system unstable in low ambient temperature. Performance characteristics of the vapor cycle refrigeration system has been experimented under air conditions which is derived from the flight envelope. From the experiments, the vapor cycle refrigeration system has been proved to provide enough cooling air to the reconnaissance equipment and to be stable under all the flight conditions.

• International Journal of Aerospace System Engineering
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• 제5권2호
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• pp.1-7
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• 2018

This study examines the history of Korean aviation industry and presents the investment strategy based on the evidence and the 4th industrial revolution. Looking at the evolution of the Korean aviation industry and its technological development will be a great help to support industrial and technological innovation in the future. The modern aviation industry is divided into stages of development, focusing on maintenance of equipment introduced in advanced countries, localization through license assembly, production of products based on technology, and international joint development. The development of aeronautics technology has been progressing towards a general improvement of economic efficiency, aircraft safety efficiency through environmental-friendliness, unmanned operation, and downsizing. The Korea Aerospace Research Institute has secured key technologies through development of several aircrafts such as Experimental Aircraft Kachi, EXPO Unmanned Airship, Twin-engine Composite Aircraft, Canard Aircraft, Multi-Purpose Stratosphere unmanned-airship, Medium Aerostats, Smart UAV, Surion, EAV-2H, KC-100, and OPV. The development strategy is discussed at the level of the evidence-based investment strategy that is currently being discussed, and so the investment priorities in aircraft is high. Current drone usage and development direction are not only producing parts using 3D printer, but also autonomous flight, communication (IoT, 5G), information processing (big data, machine learning). Therefore, the aviation industry is expected to lead the fourth industrial revolution.

• Journal of Positioning, Navigation, and Timing
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• 제10권2호
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• pp.113-120
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• 2021

The Distance Measuring Equipment (DME) is a ground-based aircraft navigation system and is considered as an infrastructure that ensures resilient aircraft navigation capability during the event of a Global Navigation Satellite System (GNSS) outage. The main problem of DME as a GNSS back up is a poor positioning accuracy that often reaches over 100 m. In this paper, a novel approach of applying deep reinforcement learning to a DME pulse design is introduced to improve the DME distance measuring accuracy. This method is designed to develop multipath-resistant DME pulses that comply with current DME specifications. In the research, a Markov Decision Process (MDP) for DME pulse design is set using pulse shape requirements and a timing error. Based on the designed MDP, we created an Environment called PulseEnv, which allows the agent representing a DME pulse shape to explore continuous space using the Soft Actor Critical (SAC) reinforcement learning algorithm.

• 한국항공우주학회지
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• 제41권5호
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• pp.391-403
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• 2013

전기 추진 프로펠러 항공기는 기존의 제트엔진으로부터 나오는 유해한 배기가스로 인한 환경적 우려와 국가 에너지 안보 차원에서 새로운 관심을 받고 있다. 그러나 전통적인 항공기 사이징 방법들은 여러 종류의 에너지원과 동력 시스템을 사용하는 전기 추진 항공기에 바로 적용될 수 없다. 본 연구에서는 일반화된 동력기반 사이징 기법에 기초한 전기 추진 항공기 사이징의 실제 예를 제시하였다. 여기서 일반 항공기는 프로펠러, 고온초전도모터, 수소가 연료로 사용되는 연료전지, 동력 조절 장치로 구성되는 전기 추진시스템에 의해 구동된다. 기술 향상의 영향을 평가하기 위해 전기 구성품들의 두 가지 다른 기술 구성을 가정하여 항공기 사이징을 수행하였고, 전형적인 형태의 기준 항공기와 사이징 결과를 비교하였다.