• Title/Summary/Keyword: 비행 절차

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Quantitative Safety Assessment and Effectiveness Analysis for Duplication of ATS Routes (복선 항공로에 대한 정량적 안전평가 및 효과에 관한 분석)

  • Se-eun Park;Sun-min Park;Hui-yang Kim
    • Journal of Advanced Navigation Technology
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    • v.28 no.4
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    • pp.480-489
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    • 2024
  • The Ministry of Land, Infrastructure and Transport duplicated a section of ATS Route Y579 connecting Jeju and Busan in 2022 to enhance aviation safety and operational efficiency. Before duplication, an offset procedure was applied to separate aircraft flying in opposite direction by deviating them to the right of their intended flight paths. However, on December 1, 2022, this offset procedure was abolished and replaced with two parallel route, Y571(towards Busan) and Y572(towards Jeju), to improve safety and efficiency. The duplication of ATS Routes has significant implications in various aspects. This study analyzes the safety of the newly established ATS Routes and compares their safety with the previously applied offset procedure to evaluate the effectiveness of the duplication. Additionally, it presents the significance from the perspective of airspace operation. A safety assessment has conducted using a modified version of the Reich CRM (collision risk model). The analysis results confirms that the level of safety improves after the duplication and that there were benefits in terms of airspace utilization.

The Obligation of Return Unjust Enrichment or Compensation for the Use of Flight Safety Zone -Seoul High Court Judgment 2018Na2034474, decided on 2018. 10. 11.- (비행안전구역의 사용에 대한 부당이득반환·손실 보상 의무의 존부 -서울고등법원 2018. 10. 11. 선고 2018나2034474 판결-)

  • Kwon, Chang-Young;Park, Soo-Jin
    • The Korean Journal of Air & Space Law and Policy
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    • v.35 no.1
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    • pp.63-101
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    • 2020
  • 'Flight safety zone' means a zone that the Minister of National Defense designates under Articles 4 and 6 of the Protection of Military Bases and Installations Act (hereinafter 'PMBIA') for the safety of flight during takeoff and landing of military aircrafts. The purpose of flight safety zone is to contribute to the national security by providing necessary measures for the protection of military bases and installations and smooth conduct of military operations. In this case, when the state set and used the flight safety zone, the landowner claimed restitution of unjust enrichment against the country. This article is an analysis based on the existing legal theory regarding the legitimacy of plaintiff's claim, and the summary of the discussion is as follows. A person who without any legal ground derives a benefit from the property or services of another and thereby causes loss to the latter shall be bound to return such benefit (Article 741 of the Civil Act). Since the subject matter is an infringing profit, the defendant must prove that he has a legitimate right to retain the profit. The State reserves the right to use over the land designated as a flight safety zone in accordance with legitimate procedures established by the PMBIA for the safe takeoff and landing of military aircrafts. Therefore, it cannot be said that the State gained an unjust enrichment equivalent to the rent over the land without legal cause. Expropriation, use or restriction of private property from public necessity and compensation therefor shall be governed by Act: provided, that in such a case, just compensation shall be paid (Article 23 (1) of the Constitution of The Republic of KOREA). Since there is not any provision in the PMBIA for loss compensation for the case where a flight safety zone is set over land as in this case, next question would be whether or not it is unconstitutional. Even if it is designated as a flight safety zone and the use and profits of the land are limited, the justification of the purpose of the flight safety zone system, the appropriateness of the means, the minimization of infringement, and the balance of legal interests are still recognized; thus just not having any loss compensation clause does not make the act unconstitutional. In conclusion, plaintiff's claim for loss compensation based on the 'Act on Acquisition of and Compensation for land, etc. for Public Works Projects', which has no provision for loss compensation due to public limits, is unjust.

A Study on the Altitude Restrictions of Obstructions outside Airport Obstacle Limitation Surfaces of Korea (한국의 비행장 장애물 제한구역 밖의 장애물이 항공안전에 미치는 영향에 관한 연구)

  • Yang, Han-Mo;Kim, Byung-Jong;Kim, Do-Hyun
    • Journal of Korean Society of Transportation
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    • v.23 no.6 s.84
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    • pp.41-53
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    • 2005
  • The effective utilization of an airport is considerably influenced by natural features and man-made structures inside and outside its boundary. These obstacles affect the airspace available for approaches and departures and the weather minima which dictates the necessary weather conditions for aircraft to be allowed to take-off or land. Certain areas of the airspace near airports must be regarded as the integral parts of the airport system. The availability of the required airspace is as important as are the runway and their associated strips to the safe and efficient use of the airport. For these reasons, ICAO and the member states have established the standards regarding the obstacle limitation surfaces and regulated the construction of the man-made structures in and beyond the surfaces. Existing objects that extend above a obstacle limitation surfaces should as for as practicable be removed except when, in the opinion of the appropriate authority, an objects is shielded an existing immovable objects, or after aeronautical study it is determined that the object would not adversely affect the safety or significantly affect the regularity of operations of airplanes. However, Korea's aviation law does not specified the outer horizontal surface in the obstacle limitation surfaces, while ICAO and most member states do. The absence of the outer horizontal surface regulation has created legal disputes between regulating agencies and private parties. The case study in this paper found that a skyscraper planned beyond Korea's obstacle limitation surfaces does affect the flight safety and the efficient use of an airport. Therefore, in areas beyond the obstacle limitation surfaces. those objects which extend to a height of 150m or more above ground elevation should be regarded as obstacle, unless a special aeronautical study indicates that they do not constitute a hazard to airplanes. We proposed low alternative regulatory schemes for resolving the issues raised in this paper, and we recommended to adopt ICAO's standards and recommended practices.

A Study on Takeoff Decision Speed Improvement of Air Transport Airplane (운송용항공기의 이륙단념속도 개선에 관한 연구)

  • Noh, Kun-Doo;Choi, Youn-Chul;Yoo, Kwang-Eui
    • Journal of Korean Society of Transportation
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    • v.23 no.4 s.82
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    • pp.7-16
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    • 2005
  • Rejected Takeoff Accidents are not common. but if occurred, it leads to big disaster From the year of 1959, when Jet Transport service opened, to the year of 2000, Rejected Takeoff accidents/incidents occurred total of 94 cases. All cases led to overrun, and major cause is to initiate stopping maneuvers over $V_1$, takeoff decision speed, according to National Transport Safety Board of America. Similar results are represented in Aviation Safety Reporting System of National Aeronautics and Space Administration. So I believe that it is worth studying if Airplane Flight Manual, which is the reference Performance criteria, is appropriate to operations of line pilots. The definition of $V_1$ has been revised a couple of times and Rejected Takeoff Certification Standards for Transport Airplanes was changed in 1998. It shows that up to now there are some portions unreasonable. This study focused on gathering the pilot's tendency for current Rejected Takeoff Procedures of K airlines and analyze the factors they concern. I chose B777 airplane and actually measured the recognition and reaction time of the rejected takeoff transitions through Simulators. And compared the results with the data of flight test and Airplane Flight Manual.

The effect of notification disposition in the current juvenile justice system from the perspective of institutionalized children's welfare (시설보호아동의 복지 관점에서 본 소년법상 통고제도)

  • Lee, Hyung-Seob;Jung, Sun-wook
    • Journal of the Korean Society of Child Welfare
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    • no.56
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    • pp.69-99
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    • 2016
  • Taking the perspective of children's welfare, this study aimed at critically analyzing the system of notification disposition which institutionalized children have experienced. Notification disposition is a juvenile justice process that, when a child (10 th 18 years old ) has been delinquent or is at risk for delinquency, is initiated without investigation or prosecution procedures by direct notification to a judge from the caregivers, school principals, chief probation officers, or directors of child care institutions. The data used in the analysis included case records of probation offices, and court sentencing documents of juvenile protective dispositions. Results showed that notification cases were initiated by directors of child shelters/care institutions. The most common reasons of notification were theft, runaway, physical violence, drinking, and smoking. Furthermore, there were more controversial reasons, such as "bad influence on another institutionalized children", "showing no remorse", "no sense of guilt"and "challenge of rearing in institutions" Based on the results, we discussed three problematic aspects of the direct notification system by directors of childcare institutions : (1) too much reliance on the judicature judgment of juvenile court; (2) less stability of the judicial status of notified children, and (3) inadequacies of the notifying eligibility for directors of child care institutions.

The Study on Development on LUAV Software based on DO-178 (DO-178 기반 무인비행장치 소프트웨어 개발 방안에 대한 고찰)

  • Ji-hun Kwon;Dong-min Lee;Kyung-min Park;Ye-won Na;Ye-ju Kim;Gi-moung Lee;Jong-whoa Na
    • Journal of Advanced Navigation Technology
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    • v.27 no.4
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    • pp.382-390
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    • 2023
  • The Korea market for LUAV (Light Unmanned Aerial Vehicle) weighing less than 150 kg is growing rapidly. As a result, the market for manufacturing and operating LUAV is expanding, and domestic development of parts and finished products is actively taking place. However, the flight control system and onboard software, which are key components of domestic LUAV, are largely dependent on overseas products due to the excessive cost and period required for development. This paper presented a domestic software development and certification procedure using DO-178C, a guideline for aircraft software development, and the Model-based Development method, and conducted a survey of those involved in the development, manufacturing, and certification of LUAV and analyzed the results. In addition, a case study was conducted to apply the software development plan to the helicopter FCC (Flight Control Computer).

A Study on Optimal Airspace Design for Continuous Climb Operation (연속상승운항을 위한 최적 공역 설계에 관한 연구)

  • Kim, Eun-Young;Hong, Sung-Kwon;Lee, Keum-Jin
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.23 no.2
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    • pp.15-20
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    • 2015
  • This paper introduces a new airspace design method for continuous climb operation (CCO). The optimization problem is formulated as Mixed-Integer Linear Program (MILP) to maximize the upper limits of altitude on the waypoints to facilitate continuous climb for aircraft. In the proposed method, the interactions with other flight procedures are considered as well as various aircraft flight performances. The proposed method is applied to one of the departure procedures of Incheon International Airport (ICN) to demonstrate its performances.

Development & Operation of Integrated Technical Information System (통합기술정보시스템(ITIS)의 개발 및 운용)

  • Chung, Joon-Young;Lee, Joon-Woo;Kim, Cheon-Young;Lee, Sang-Bum
    • Proceedings of the Korea Information Processing Society Conference
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    • 2003.05b
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    • pp.859-862
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    • 2003
  • 지금까지의 기술자료관리는 수작업의 비효율성과 복잡한 절차로 인해 업무의 시간 손실을 발생시켜 왔다. 대용량 저장장치, 그래픽 디스플레이 및 네트워킹 같은 정보기술 진보는 효과적인 전자문서 처리를 가능하게 했다. 본 논문에서 기술하고자하는 XKO-1의 통합기술 정보시스템 모델은 방대한 문서 데이터베이스를 개발하고 XKO-1 항공기의 도면, 기술문서 및 비행시험 자료의 관리와 처리를 지원하기 위한 기술을 보여주기 위한 것이다. 또한 ITIS 프로그램은 워크플로우를 이용한 문서저장기능과 스캐너를 사용해서 문서를 디지탈화, 전자화, 색인화 및 압축화하여 데이터베이스에 저장할 뿐만 아니라, 프로세스에 따라 검색 및 분배된다.

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A Study on the Control Law Design and Analysis Process (비행제어법칙 설계 및 해석 절차에 관한 연구)

  • Hwang Byung-moon;Cho In-jae;Kim Chong-sup
    • Journal of Institute of Control, Robotics and Systems
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    • v.11 no.11
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    • pp.913-919
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    • 2005
  • An advanced method of Relaxed Static Stability (RSS) is utilized for improving the aerodynamic performance of modem version supersonic jet fighter aircraft. The flight control system utilizes RSS criteria in both longitudinal and lateral-directional axes to achieve performance enhancements and improve stability. Standard CLDA (Control Law Design and Analysis) process is provided that reduce the development period of the flight control system. In addition, if this process is employed in developing flight control laws, it reduces the trial and error development and verification of control laws. This paper details the design process of developing a flight control law for the RSS aircraft, utilizing military specifications, linear and nonlinea, analysis using XMATH and ATLAS(Aircraft, Tim Linear and Simulation), handling quality tests using the HQS (Handling Quality Simulator), and real flight test results to verify aircraft dynamic flight responses.

Flight Control System Design and Verification Process (비행제어시스템 설계 및 검증 절차)

  • Kim, Chong-Sup
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.8
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    • pp.824-836
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    • 2008
  • Relaxed static stability(RSS) concept has been applied to improve aerodynamic performance of modern version supersonic jet fighter aircraft. Therefore, flight control systems are necessary to stabilize an unstable aircraft, and provides adequate handling qualities and achieve performance enhancements. Standard FCSDVP (Flight Control System Design and Verification Process) is provided to reduce development period of the flight control system. In addition, if this process is employed in developing flight control system, it reduces the trial and error for development and verification of flight control system. This paper addresses the flight control system design and verification process for the RSS aircraft utilizing design goal based on military specifications, linear and nonlinear system design and verification based on universal software, handling quality test based on HILS(Hardware In-the-Loop Simulator) environment, and ground and flight test results to verify aircraft dynamic flight responses.