• Title/Summary/Keyword: 비행안전성

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우리나라의 공역관리 개선방안

  • 박근혜
    • Proceedings of the KOR-KST Conference
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    • 1998.10b
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    • pp.453-453
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    • 1998
  • 우리나라가 관할하는 공역의 넓이는 약 40만$\textrm{km}^2$로 주한미군이 1952년부터, 국방부가 1958년부터 관리해 오다가 1995년에 건설교통부가 공역관리 업무를 인수하였다. 우리나라의 공역(대구 FIR)에는 비행금지구역, 비행제한구역, 위험구역, 경제구역, 훈련구역, 군작전구역 등 무려 114개의 특수목적 공역이 설정되어 있어 민항공기의 운항이 자유롭지 못하다. 또한 내륙을 중심으로 14개의 접근관제규역이 설정되어 있고 각기 관할구역에 대하여 배타적인 권리를 행사함으로써 신공항건설에 따라 운항이 필요한 소요공역 확보에도 애로가 많은 실정이다. 항로는 국내항로 5개, 국제항로 11개 등 모두 16개의 항로를 운영하고 있으나 대부분 한 개의 항로를 양방향으로 운영하고 있어 교통량 처리가 어려운 실정이고 항공교통량 전체의 75%가 수도권으로 집중되는 현상이 나타나 안전도 확보에도 지장을 주고 있다. 우리나라는 군사적 특수성 때문에 군의 작전비행 활동이 상당히 많으나 관제 및 비행절차에 관한 규정을 군과 민이 각각 달리 운영하고 있는 문제점들이 있다. 금번 세미나에서는 군의 작전활동을 유지하면서 민 항공의 안전성, 경제성 등을 확보하기 위하여 1)국제민간항공기가 제정한 공역등급화(ATS Air Space Spacification)방안, 2)접근관제구역의 조정개선 방안 3)특수공역의 합리적 운영방안, 4)항로의 적선화, 복수의 일방통행 항로 확보 및 국제연결 항로의 다양한 방안, 5)군민간의 관제규정의 일원화 방안 등을 제안하고자 한다.

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HILS Test for the Small Aircraft Autopilot (소형항공기용 Autopilot HILS 시험)

  • Lee, Jang-Ho;Kim, Eung-Tai;Seong, Ki-Jeong
    • Aerospace Engineering and Technology
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    • v.8 no.1
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    • pp.172-178
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    • 2009
  • Recently, autopilot is essential to reduce pilot's workload and increase flight safety. Avionics system of the small aircraft also has progressively adopted centralized multi-processor and multi-process computing architectures similar to the integrated modular avionics of B-777. It is increased more and more that importance of the flight control system. In this paper, the performance of the autopilot for the small aircraft has been verified with Hardware-In-the-Loop Simulation(HILS). Also, the autopilot algorithm that is operated in the Flight Control Computer(FCC) for the Fly by Wire(FBW) was verified with PILS and compared with the HILS results for the several commercial autopilots.

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The Effect of Flight Stress on Job Satisfaction and Safety Culture: Moderator Effect by Airlines and Rank (비행 스트레스가 직무 만족도와 안전문화에 미치는 영향 : 항공사 및 직급별 조절된 매개효과)

  • Byeong-Seon Yoo;Kangmin Ko
    • Journal of Advanced Navigation Technology
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    • v.28 no.1
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    • pp.44-50
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    • 2024
  • This study analyzed the effect of flight stress on job satisfaction and safety culture on 193 domestic civil airline pilots. As a result of the analysis, flight stress had a negative effect on job satisfaction, and pilots with low job satisfaction had a low awareness of safety culture. In particular, there was a difference in the effect of flight stress on job satisfaction and safety culture according to the airlines and rank of pilots. This suggests the necessity of developing customized stress management programs for each airline and pilot position. The study emphasizes the importance of managing pilots' stress and improving job satisfaction to reinforce the safety culture of the aviation industry. In addition, airlines should develop strategies to strengthen safety culture by reducing pilot stress and increasing job satisfaction. The result of this study is to be used as useful basic data for finding ways to manage pilots' stress and strengthen safety culture in the aviation industry.

Comparison Study on Take-Off and Landing Flight Test Using Ground Observation and DGPS Method (지상관측법 및 DGPS 기법을 활용한 이/착륙 성능 비행시험 비교)

  • Lee, Sang-Jong;Chang, Jae-Won;Jeon, Byoung-Ho;Seong, Kiej-Jeong;Yeom, Chan-Hong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.9
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    • pp.931-938
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    • 2009
  • The flight test is last means of compliance to satisfy airworthiness standards and important to evaluate the performance and safety of the developed aircraft. The flight test technologies are obtained from great numbers of experiences and know-hows and protected. In addition, flight test should be conducted efficiently since its various test conditions and items. Therefore, it is requisite to secure efficient flight test methods. This paper discusses the flight test methods for take-off and landing performance and two kinds of techniques are proposed. By performing real flight tests, they are compared with each other and analyzed through the flight analysis.

Flight Compatibility Certification of ALQ-X ECM Pod (ALQ-X ECM 포드 비행 적합성 인증)

  • Jun, Seung-Moon;Lim, Jae-Moon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.4
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    • pp.91-99
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    • 2005
  • Flight compatibility certification is performed to substantiate the compatibility between ALQ-X ECM pod and KF-16D/RF-4C aircraft. A certification plan for the ALQ-X flight compatibility is established. Similarity analysis, mass/inertia analysis, structural analysis/test, and ground vibration test/flutter analysis are made to support the safety of MIL-HDBK-1763 Test 250 (Captive compatibility flight profile). Aircraft flew along flight envelope boundary with representative ALQ-X configurations. Handling qualities are evaluated by comparing flight characteristics of the aircraft with and without ALQ-X. Structural integrity and endurance is evaluated using measured flight test data. Results of these flight tests showed that ALQ-X is compatible with KF-16D/RF-4C without altering the flight envelope which has originally been certified for ALQ-88 and ALQ-119 ECM pods. ALQ-X certification program made following technical achievements: Type III certification for foreign designed fighter, flutter analysis program development using GVT results, and utilization of MIL-STD-1553B data bus in flight test.

A Study of Model-Based Aircraft Safety Assessment (모델기반 항공기 안전성평가에 관한 연구)

  • Kim, Ju-young;Lee, Dong-Min;Lee, Byoung-Gil;Gil, Gi-Nam;Kim, Kyung-Nam;Na, Jong-Whoa
    • Journal of Aerospace System Engineering
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    • v.15 no.5
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    • pp.24-32
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    • 2021
  • Personal Air Vehicle (PAV), Cargo UAS (Cargo UAS), and existing manned and unmanned aircraft are key vehicles for urban air mobility (UAM), and should demonstrate compatibility for the design of aircraft systems. The safety assessment required by for certification to ensure safety and reliability should be systematically performed throughout the entire cycle from the beginning of the aircraft development process. However, with the increasing complexity of safety critical aviation systems and the application of state-of-the-art systems, conventional experience-based and procedural-based safety evaluation methods make ir difficult to objectively assess safety requirements and system safety. Therefore, Model-Based Safety Assessment (MBSA) using modeling and simulation techniques is actively being studied at domestic and foreign countries to address these problems. In this paper, we propose a Model-Based Safety Evaluation framework utilizing modeling and simulation-based integrated flight simulators. Our case studies on the Traffic Collision Availability System (TCAS) and Wheel Brake System (WBS) confirmed that they are practical for future safety assessments.

Compound Test를 활용한 위성비행소프트웨어의 검증

  • Sin, Hyeon-Gyu;Yang, Seung-Eun;Lee, Jae-Seung;Cheon, Lee-Jin
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.226.1-226.1
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    • 2012
  • 위성에 탑재되어 위성의 상태를 모니터링하며, 지상으로부터 명령을 받아 위성 본연의 임무 수행이 가능하게 하는 위성비행소프트웨어는 그 개발단계에서 다양한 검증활동이 이루어진다. 설계 검증 및 리뷰, 인스펙션을 거쳐 소스 코드로 구현된 후, 단위 시험을 통해 가장 낮은 수준의 검증을 거치게 된다. 이러한 단위 시험은 개별 함수에 대해 입력에 따른 해당 출력 및 동작 여부를 검사하게 된다. 단위 시험이 하나의 함수에 대한 시험 항목이라는 점은 검증대상의 스코프가 좁다는 장점이 있으나, 다른 모듈과 연동되었을 경우에 발생할 수 있는 다양한 경우를 고려하여 테스트 케이스를 작성해야 하는 어려움이 있다. 이러한 문제점을 해결하기 위하여 단위 시험과 함께, 연관된 함수가 이미 구현되어 있는 경우, Stubbing을 하기보다는 직접 해당 함수를 사용하며, 또한 동등한 수준의 개별 함수들을 주어진 시나리오에 따라 동작하는 Compound Test를 활용, 그 결과를 확인하는 방법을 도입하였다. 이를 이용하면 단위 시험에서는 검증하기 어려운 상황별 시나리오에 따른 검증 활동을 수행할 수 있고, 또한 전체 위성비행소프트웨어를 빌드할 필요없이 테스트의 대상이 되는 함수만을 이용, 나머지 부분은 기존의 방식을 그대로 적용할 수 있어, 위성비행소프트웨어의 안전성 및 신뢰성을 보다 향상시킬 수 있다.

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Synthetic Overview on the Dispute about Tiltrotor Technology and Flight Safety (틸트로터 비행체 개념에 대한 기술적 논란 및 비행안전성 논란 분석)

  • Ahn, Oh-Sung;Kim, Jai-Moo
    • Aerospace Engineering and Technology
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    • v.7 no.1
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    • pp.254-262
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    • 2008
  • Several decades have passed since tiltrotor technology became a hot issue of debates between aircraft majors, policy maker and mass-media. Although most of those subjects have been officially probed or answered in objective way, biased articles or argues related with the adequacy of this technology still prevail in the way of tilt-rotor development programs, which are totally irrelevant and out-dated. This paper aims to help understanding on those issues in technically balanced manner and the cases of flight test mishaps.

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시스템 안전의 항공기설계에의 응용

  • Jo, Geon-Hyeon
    • Defense and Technology
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    • no.5 s.147
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    • pp.55-63
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    • 1991
  • 시스템 안전에 대한 연구는 매년 증가하는 사고로부터 발생하는 엄청난 손실을 줄여보자는 필요하에 1960년경부터 미국의 군대에서 시작되었다. 시스템안전은 개발중인 시스템의 설계, 개발, 응용과 관련된 여러분야 즉 품질보증, 인간공학, 신뢰성, 정비성, 가치공학, 시험지원분야, 설계/생산공학, 산업안전, 시스템공학, 형상관리분야등과 상호 밀접하게 관련되어 있으므로 이분야에 대한 상호이해와 끊임없는 정보교환이 요청되고 있다. 항공기 개발프로그램의 경우 시스템 안전의 궁극적인 목표는 성공적인 초도비행이라고 할수 있다

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Effects of Job Stress and Hazard Factors on Pilot Safety Behavior (비행안전 위해(Hazard)요인이 조종사의 안전행동에 미치는 영향)

  • Dong-ryeol Lee;Hyeon-deok Kim
    • Journal of Advanced Navigation Technology
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    • v.28 no.1
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    • pp.87-94
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    • 2024
  • Despite the development of the aviation industry, aircraft accidents due to pilots' human errors continue to occur. The cause of aircraft accidents due to human errors is that they cannot remove hazard factors that hinder flight safety in advance, leading to accidents. This study examined how job stress, fatigue, and anxiety, which psychologically and physically affect flight safety among various hazard factors, affect pilots' safety behavior for flight crew and pilots of general aviation working in domestic airlines. In addition, an empirical analysis was conducted to confirm the mediating effect of safety culture between job stress and safety behavior. According to the results of the study, job stress not only directly affects the safety behavior of pilots, but also affects the safety culture of airlines such as safety atmosphere and reporting culture. The purpose of this study is to improve the performance of the safety management system through the correlation between the pilot's job stress and safety culture and safety behavior.