• 제목/요약/키워드: flight management system

검색결과 229건 처리시간 0.023초

항공기 비상조치 전문가 시스템 (An Expert System for Aircraft Emergency)

  • 김성인;정석윤
    • 한국국방경영분석학회지
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    • 제24권1호
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    • pp.88-97
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    • 1998
  • It is critical to determine the appropriate actions for safe landing of an aircraft in an emergency situation. An expert system can be very useful for this purpose. An expert system specifically for jet fighter $F-\bigcirc\bigcirc$ has been developed. Its knowledge base contains the standard procedures provided by various flight manuals and the expertise of human specialists such as pilots and emergency management personnels. Advising procedures are represented by an IF-THEN format in the developed rule-based expert system. Advises are provided in real time during the entire flight processes of ground, takeoff, inflight, and landing. The developed system would significantly increase the survivability of pilots and aircraft, while decreasing operational costs of emergency management personnels. By modifying the knowledge base, the developed system can also be applied to other types of aircrafts including civilian airlines.

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초경량비행장치의 민원처리시스템 운용 및 관리 효율성 개선을 위한 연구 (Study on Improvement in Operation and Management of Ultra-light flying device Civil Complaints Management System for Ultralight Aircraft)

  • 석금찬;장문수;류연승
    • 한국융합학회논문지
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    • 제11권1호
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    • pp.237-246
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    • 2020
  • 본 연구의 배경 및 문제는 초경량비행장치 산업의 발전으로 드론의 성능이 향상되고 운행 대수는 증가하는 반면에 비행 인·허가 과정은 개선되지 않아 민원이 증가하는 추세에 있다. 목적은 민원을 최소화하고 양개기관 요구조건에 맞게 시스템 운용 및 관리 전반에 대한 개선이다. 연구방법은 문헌연구 및 조사를 통하여 문제점을 도출하고 기관 및 전문가들의 포커스 그룹 인터뷰를 통해 검증하여 개선안을 제시하였다. 연구결과는 국토부 주관 하 항공안전법 내에 양개기관 임무·역할 및 시스템 운용·관리에 대한 반영, 비행 인·허가에 대한 명칭·절차·양식의 통합, 시스템 상에 홈페이지 바로가기 등 다수의 기능개선이다. 기대효과는 첫째, 관련법령에 양개기관의 임무와 역할을 명시함으로서 민원처리 협조가 원활해지며 둘째, 민원처리 프로세스를 통합함으로서 처리 기간단축으로 효율성이 향상되고 셋째, 대국민서비스 부가기능을 개선함으로서 민원 최소화가 기대된다. 향후 연구는 국방부 주관 하 항공촬영허가에 대한 제도적 기반마련, 국방개혁 2.0연계 관할부대 재편성, 현장 보안조치부대 여건보장 등 개선이 필요하다.

비행절차설계과정에서 적용 가능한 위험평가기준 연구 (A Study on the Risk Assessment Criteria to be applicable for Establishing Flight Procedure Design Process)

  • 김도현;김웅이;지민석
    • 한국항공운항학회지
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    • 제21권1호
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    • pp.51-56
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    • 2013
  • Risk assessment should be processed when physical circumstances of airspace such as establishment of new flight procedures or reconstruction of existing airspace are planned to change and one of the alternatives for the change have to be selected. This is an effort to find the best alternative which is able to maintain at or above the acceptable risk level. ICAO and its contracting states provide specialized guidance material for 'Safety Management System' relating to handing airspace matters. These manuals include a conceptual framework for managing safety as well as some of the systemic processes and criteria used to meet the objectives of a State's safety programme. This criteria must be established in compliance with the State's laws and regulations for air safety and for the fulfillment of the State's safety goals. This study is to carry out the risk assessment criteria through literature reviews relevant to the safety management, and to propose the results of criteria to be applicable for establishing flight procedure design process.

기동헬기 측면항법 알고리즘 구현 및 검증 (Implementation and Verification of Lateral Navigation Algorithm for Korean Utility Helicopter)

  • 김성우;고은경
    • 한국정보통신학회논문지
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    • 제22권2호
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    • pp.354-361
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    • 2018
  • 본 논문은 비행제어 비행체 관리 시스템 대신 한국형 기동헬기 임무컴퓨터의 비행운용 프로그램에서 구현한 측면 항법 알고리즘 설계 및 검증에 대하여 기술하였다. 구현된 측면항법 기능은 비행제어 시스템으로 롤 명령을 보내고 롤 명령 값은 임무컴퓨터의 제어 알고리즘에서 계산한다. 임무컴퓨터에서 제어 알고리즘 계산 시 항공기의 자세 및 위치에 대한 측정값을 이용한다. 이 입력 값들을 이용하여 임무컴퓨터에 탑재된 비행운용 프로그램은(선택한 비행계획 등)항법 요구를 롤 명령으로 자동조종으로 보낸다. 체계통합리그에서의 통합시험, 지상 및 비행시험을 통해 측면 항법 알고리즘을 검증하였다.

CPS환경에서 산불 정찰을 위한 무인기 비행경로 생성 도구 (UAV Path Creation Tool for Wildfire Reconnaissance in CPS Environment)

  • 정지원;배창희;최으뜸;이성진
    • 대한임베디드공학회논문지
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    • 제18권6호
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    • pp.327-333
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    • 2023
  • Existing studies on the UAV (Unmanned Aerial Vehicle)-based CPS (Cyber Physical System) environment lack forest fire monitoring and forest fire reconnaissance using real-world UAVs. So, it is necessary to monitor forest fires early through CPS based on real-world UAVs with high reliability and resource management efficiency. In this paper presents an MFG (Misstion File Generater) that automatically generates a flight path of an UAV for forest fire monitoring in a CPS environment. MFG generates flight paths based on a hiking trail with a high fire probability due to a true story of an entrant. We have confirmed that the flight path generated by MFG can be applied to the UAV. Also, we have verified that the UAV flies according to the flight path generated by MFG in simulation, with a negligible error rate.

소형 항공기의 전자식 디스플레이 설계시 고려사항 (Design Considerations of Electronic Display in Part 23 Airplanes)

  • 이백준;진영권
    • 항공우주시스템공학회지
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    • 제7권1호
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    • pp.26-31
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    • 2013
  • A glass cockpit is an aircraft cockpit that features electronic (digital) instrument displays, typically large LCD screens, rather than the traditional style of analog dials and gauges. While a traditional cockpit relies on numerous mechanical gauges to display information, a glass cockpit uses several displays driven by flight management systems, that can be adjusted to display flight information as needed. This study introduces design considerations of electronic display in KAS Part 23 airplanes.

공항용량 향상을 위한 위성항법기반 평행 접근 연구 (GNSS-based Parallel Approaches to Increase Airport Capacity)

  • 신권상;여송희;이형복
    • 한국항공운항학회지
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    • 제22권2호
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    • pp.53-59
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    • 2014
  • Simultaneous parallel approaches in all weather conditions should be applied to manage efficiently increasing volume of air traffic flow and solve the problem of delayed arrivals. But All of the airports which have closely-spaced parallel-runways in Korea don't meet the interval-standards for IFR parallel approaches. In that regard, more accurate and safer System should be applied for the Korean airports. GNSS was adopted as an international standard of the next-generation navigation system and many studies and master plans have been activated by stages in Korea. In this paper, the current state of the domestic airports will be analyzed focusing on the interval of parallel runways and future specification of both flight operation system and air-side management will be recommended.

항공안전법상 운항규정의 사법적 판단에 관한 고찰 (A Study on the Judicial Judgment of Flight Regulations under the Aviation Safety Act)

  • 김성미;안희복;여운진;황호원
    • 한국항공운항학회지
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    • 제31권3호
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    • pp.161-171
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    • 2023
  • The traditional safety management method starts with the misconception that similar accidents will recur if the inappropriate behavior of the person who caused the accident is investigated and punishment is not judged. However, in modern safety management, incidents or situations occur when negative conditions latent in the system are mutually influenced and triggered. The precedent for revoking the disposition of suspension of first officer A of Eastar Jet, which won a legal lawsuit against the administrative regulatory authority, is a representative example that will serve as an opportunity for the administrative regulatory authority to break away from the punishment-oriented safety management method of the past. On the other hand, airmans and air carriers also need to have a clear understanding of flight regulations, and when judicial judgment is required, predictable and effective legal effects can be obtained by preparing clear standards for flight regulations. In addition, administrative regulatory authorities expect a change from the punishment-oriented safety management policy of the past to a systematic safety management policy.

다대다 대응 위협평가 및 무기할당 알고리즘 연구: 탄도미사일 및 장사정포 위협을 중심으로 (A Study of Multi-to-Majority Response on Threat Assessment and Weapon Assignment Algorithm: by Adjusting Ballistic Missiles and Long-Range Artillery Threat)

  • 임준성;유병천;김주현;최봉완
    • 산업경영시스템학회지
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    • 제44권4호
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    • pp.43-52
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    • 2021
  • In weapon assignment studies to defend against threats such as ballistic missiles and long range artillery, threat assessment was partially lacking in analysis of various threat attributes, and considering the threat characteristics of warheads, which are difficult to judge in the early flight stages, it is very important to apply more reliable optimal solutions than approximate solution using LP model, Meta heuristics Genetic Algorithm, Tabu search and Particle swarm optimization etc. Our studies suggest Generic Rule based threat evaluation and weapon assignment algorithm in the basis of various attributes of threats. First job of studies analyzes information on Various attributes such as the type of target, Flight trajectory and flight time, range and intercept altitude of the intercept system, etc. Second job of studies propose Rule based threat evaluation and weapon assignment algorithm were applied to obtain a more reliable solution by reflection the importance of the interception system. It analyzes ballistic missiles and long-range artillery was assigned to multiple intercept system by real time threat assessment reflecting various threat information. The results of this study are provided reliable solution for Weapon Assignment problem as well as considered to be applicable to establishing a missile and long range artillery defense system.

236U accelerator mass spectrometry with a time-of-flight and energy detection system

  • Li Zheng;Hiroyuki Matsuzaki;Takeyasu Yamagata
    • Nuclear Engineering and Technology
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    • 제54권12호
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    • pp.4636-4643
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    • 2022
  • A time-of-flight and energy (TOF-E) detection system for the measurement of 236U accelerator mass spectrometry (AMS) has been developed to improve the 236U/238U sensitivity at Micro Analysis Laboratory, Tandem accelerator (MALT), The University of Tokyo. With observing TOF distribution of 235U, 236U and 238U, this TOF-E detection system has clearly separated 236U from the interference of 235U and 238U when measuring three kinds of uranium standards. In addition, we have developed a novel method combining kernel-based density estimation method and multi-Gaussian fitting method to estimate the 236U/238U sensitivity of the TOF-E detection system. Using this new estimation method, 3.4 × 10-12 of 236U/238U sensitivity and 1.9 ns of time resolution are obtained. 236U/238U sensitivity of TOF-E detection system has improved two orders of magnitude better than that of previous gas ionization chamber. Moreover, unknown species other than uranium isotopes were also observed in the measurement of a surface soil sample, which has demonstrated that TOF-E detection system has a higher sensitivity in particle identification. With its high sensibility in mass determination, this TOF-E detection system could also be used in other heavy isotope AMS.