• Title/Summary/Keyword: Airspace Design

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A Study on the Applications of Airspace Design Criterions Affecting on the Flight Safety (비행안전에 영향을 미치는 공역설계기준의 적용에 관한 연구)

  • 양한모;유광의
    • Journal of Korean Society of Transportation
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    • v.21 no.1
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    • pp.7-19
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    • 2003
  • The airspace has to be designed considering the flight safety and economic efficiency of aircraft operators. The International Civil Aviation Organization(ICAO) published standards and recommended practices for safe design of the airspace. Each contracting country must follow the ICAO standards in designing the airspace for the utilization of civil aviation. Normally each member establishes its own standards and national aviation law for the safe and efficient design of the airspace, regarding the ICAO standards. However, our government has not developed yet clear and detailed standards and regulation system for airspace design. This might lead to aviation accidents and disputes between operators of aviation system This study is to review the characteristics of ICAO standards and a legal problem related to application of international standards for airspace design. Specifically this research analyzed the case of airspace design and operation of a domestic airport. The results of analysis are as follow: (1) per the safety of civil aviation, it is very required to establish national regulation system to follow ICAO standards in designing airspace, (2) It is also necessary to establish separate procedure for civil aircraft in military air base, when the aerodrome is co-used by military and civil aircraft. If the same procedure for military aircraft is applied to civil aircraft, it is necessary to make clear what the design concept is, (3) and the differences from ICAO standards have to be publicly known.

Trajectory Based Air Traffic Analysis Software Design for Dynamic Airspace Configuration (동적 공역 형상관리를 위한 궤적기반 항공 교통량 분석 소프트웨어 설계)

  • Kim, Hyoun-Kyoung;Eun, Yeon-Ju;Oh, Eun-Mi
    • Aerospace Engineering and Technology
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    • v.12 no.1
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    • pp.173-181
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    • 2013
  • In this paper, the design result of the trajectory-based air traffic analysis software which is going to be used to assess air-traffic efficiency in case that some modification's made in dynamic airspace configuration, is described. The software has been developed to make statistical data about air-traffic in Incheon FIR based on the RPL, and to analyze the airway utilization and controller workload using the trajectory modeling data which are derived from the aircraft type, cruise speed, cruise altitude, and routes and fixes in the RPL. Since it batch-processes the long-term trajectory data with other inputs such as airspace, route information and so on, it has the advantage of quickly predicting the traffic variation when some change in airspace and route information is made.

On the Design of Extending Airspace for Improving Incheon International Airport Capacity (공역확장을 통한 인천국제공항 수용능력 향상에 관한 고찰)

  • Lee, Young-Jong
    • Journal of Advanced Navigation Technology
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    • v.19 no.2
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    • pp.103-107
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    • 2015
  • In this paper, we propose a secure alternative for improving airspace capacity of Incheon International Airport. Since the direction of simultaneous independent approaches to runway 15/16 radar-guided approach for ILS approach procedures for the need to provide control services, in view of the radar is the smallest possible no-fly zone airspace propose the demilitarized zone (P-518) adjustment. If possible simultaneous independent approaches to secure a temporary increase in the holding area due to traffic, the military training airspace gradually secured a total of 10 miles by 5 miles, some military training airspace in Osan Approach Control is proposed to include in Seoul Approach Control.

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.

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

  • Kim, Dohyun;Kim, W.Y.;Jie, M.S.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.1
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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.

Design of INM Input Generation Module for Aircraft Noise Analysis with Flight Procedures (비행 절차에 따른 항공기 소음 분석용 INM 입력 자료 생성 모듈 설계)

  • Choi, ChulHee;Eun, YeonJu;Jeon, DaeKeun;Jun, HyangSig
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2012.10a
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    • pp.178-182
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    • 2012
  • PEAT(Procedure/airspace Efficiency Assessment Tool) evaluates the efficiency of the flight procedures designed by Procedure and Airspace Design Program, such as fuel consumption fight time, flyability, noise footprint and etc. For noise footprint analysis among the efficiency metrics, the input generation module for INM(Integrated Noise Model) was designed in this research. The INM input files shall contain the information about aircraft types, noise model, airport and runway configuration, number of flights, flight routes, and also should be satisfied with the exact file formats for input data, since INM is not originally executable with file inputs. Therefore, it has been designed to convert the input data given in XML file to DBF. In this paper, the design result of the module which has functionalities to generate appropriate input file for INM, and to convert and save the analysis results from INM, is presented.

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A Study on UAM Traffic Management System Development Trends and Concept Design (UAM 교통관제시스템 개발 동향 및 설계 개념 연구)

  • Changhwan Heo;Kwangchun Kang;Heungkuen Yoon
    • Journal of Information Technology Applications and Management
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    • v.30 no.6
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    • pp.81-90
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    • 2023
  • In aviation, with the rapid transformation of the mobility industry, UAMs are emerging to operate green low-altitude airspace in urban environments. In order for UAM aircraft to fly safely transporting passengers and cargo in low-altitude urban airspace, a traffic control system that supports the safe operation of the aircraft is essential. In particular, traffic control systems that reflect the characteristics of the flight environment, such as operating at low altitude in urban environments for a short period of time, are required. In this study, we define the definition of UATM and its main services that perform traffic control for the safe operation of UAMs. In addition, we analyzed the development trends of UATM systems based on domestic and overseas cases. Based on these analyses, we present the results of the concept design of the UATM system. After analyzing UATM development cases, we found that there is no commercialized UATM system, but overseas development is focused on systems that can integrate ATM and UTM. And we identified key stakeholders and interface data, and performed UATM system architecture and functional design based on the identified data. Finally, as a necessary element for the future development of UATM systems, we propose the establishment and advancement of UAM traffic flow management systems, the establishment of integrated control systems, and the development of interface with aircraft operation systems in preparation for the unmanned UAM aircraft.

Establishment of Flight Inspection Evaluation Items and Optimal Design of SBAS Performance Test Measurement Equipment by Analyzing Evaluation Items and Essential Components of Korean SBAS (한국형 SBAS의 평가항목 및 필수 구성요소 분석을 통한 비행검사 평가항목 수립 및 SBAS 성능 시험 측정 장비 최적 설계 방안)

  • Kim, Young-Bin;Hong, Gyo-Young
    • Journal of Advanced Navigation Technology
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    • v.25 no.1
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    • pp.78-83
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    • 2021
  • Due to rapidly increasing air traffic congestion and airspace restrictions, the International Civil Aviation Organization (ICAO) is urging all aircraft to use SBAS by 2025, in order to implement Performance-based navigation to increase airspace capacity. In line with this, research and development of Korean-style SBAS, which reflects the characteristics of Korea's airspace environment, continues in Korea. Since there is no flight inspection procedure for performance testing and verification of SBAS in Korea yet, this paper analyzes FAA, ICAO Regulations, and laws enacted by the Ministry of Land, Infrastructure and Transport to derive essential evaluations and parameters of Korean SBAS, and presents the optimal design using RTK-DGPS as a position fixing system.

Autonomous flight Algorithm Design (자율형 운항 알고리즘 설계 연구)

  • Lee, Dae-Yong;Kang, Ja-Young
    • Journal of Advanced Navigation Technology
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    • v.16 no.1
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    • pp.122-130
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    • 2012
  • Airborne separation assurance is a key requirement for Free Flight. This paper is to propose autonomous flight algorithm, such as extended authority of delegation, efficiency of airspace issue to deal with the empirical solution for free flight, and to measure flight efficiency and conflict detection and resolution (CD&R) by utilizing flight performance data under the two circumstances of scenario with the modeling of proposed algorithm and potential field algorithm. The results show that the autonomous flight algorithm is superior to the potential field algorithm under the circumstances of free flight airspace in terms of algorithm performance, CD&R, and flight efficiency.