• Title/Summary/Keyword: 항공관제 시스템

Search Result 124, Processing Time 0.028 seconds

A Study on the operation of Air Traffic Control System for a Korean Light Aircraft Carrier (한국형 경항공모함 항공관제장비 운영에 대한 연구)

  • Youn-chul Choi;Yong-tae Jung;Young-jin Cho;Do-hyun Kim;Won-hyuk Choi;Yoon-Su Park
    • Journal of Advanced Navigation Technology
    • /
    • v.27 no.2
    • /
    • pp.173-181
    • /
    • 2023
  • Aircraft carriers need to maintain an orderly flow of aircraft in order for military ships to conduct combat through aircraft. Maintaining aircraft flow is an important factor in strengthening ship and aviation safety. In order to maintain aircraft flow, it is essential to develop a state-of-the-art air control system that provides higher quality control information by simultaneously accommodating radar-based monitoring information and monitoring information based on CNS integrated technology. Based on this point, this study describes the function and operation method of specific control equipment for the operation of the Aviation Support System and Air Traffic Control System required to operate light aircraft carriers in Korea based on overseas cases.

Establishment of Test Environment for Surveillance Data Processor (항공관제용 감시자료처리시스템 시험 환경 구축)

  • Ko, Hyun;Jeon, Dae-Keun;Eun, Yeon-Ju;Yeom, Chan-Hong
    • Proceedings of the Korean Society of Computer Information Conference
    • /
    • 2010.07a
    • /
    • pp.91-94
    • /
    • 2010
  • 본 논문에서는 SDP 시스템이 충족해야 할 요구 규격을 검증하기 위하여 시험 환경 구축 방안을 제안하였다. SDP 시험 환경은 기능/성능/안정성 시험을 수행할 수 있도록 기존 항공관제시스템의 서브 시스템들과 동일한 기능을 수행하는 Simulation System들과 항적 추적 성능을 검증하기 위한 Eurocontrol의 SASS-C와 SMART 시스템으로 구축하였다. 또한 SDP 시험에 있어 Test Case 및 Test Procedure를 구성하여 SDP 요구 규격에 대한 정확한 검증을 수행할 수 있도록 시험 절차를 정의하였다. 제안된 시험 환경 및 시험 절차는 모의 시험을 통해 소프트웨어 구현 과정에서의 시스템 요구 규격에 대한 충족도를 보다 높일 수 있다.

  • PDF

A Study on the Design and Realization of the VHF Transmitter for Air Traffic Control (항공관제용 VHF대역 송신기 설계 및 구현에 관한 연구)

  • Park, Wook-Ki;Kang, Suk-Youb;Park, Hyo-Dal
    • Journal of Advanced Navigation Technology
    • /
    • v.9 no.2
    • /
    • pp.121-130
    • /
    • 2005
  • In this paper, we designed and fabricated the VHF wireless transmitter for air traffic control. Fundamental performance of the investigated wireless transmitter is designed and fabricated to satisfy existing commercial wireless transmitter specification for air traffic control. 25 W and 50 W of output power can be generated by changing the power amplification part only. It is based on transmitting voice communication using AM modulation. Investigated wireless transmitter for air traffic control consists of four module parts: power supply, control, low power transmission and power amplification. We designed 1W transmitter to operate without power amplification part. It can be used properly in a basic component of CNS/ATM.

  • PDF

관제사 의사결정지원을 위한 인공지능 도입 및 활용방안

  • 이정구;이현석
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
    • /
    • 2022.06a
    • /
    • pp.33-35
    • /
    • 2022
  • 빅데이터·인공지능 등 4차 산업혁명 기술은 교통·의료·환경 등 다양한 분야에서 기술개발을 추진하고 이미 많은 기술이 실제 활용되고 있다. 특히, 철도관제와 항공 관제분야에서도 인공지능 기반 시스템이 접목되어 운영되고 있으나 선박교통관제 분야는 현장에 접목되어 활용되는 기술은 극히 드물다. 선박교통관제사가 관제구역 내에서 적게는 수척, 많게는 수십척의 선박을 동시에 관제하며 발생할 수 있는 인적 과실을 줄이기 위한 인프라 구축은 선박의 안전확보를 위해 필수요소이다. 본 연구는 해양경찰청 선박교통관제기술개발단에서 자체 개발한 음주운항 자동탐지 시스템과 닻 끌림 자동탐지 시스템에 활용한 기술을 소개하고 향후 고도화 및 활용방안을 제시하고자 한다.

  • PDF

A Study on Flight Control Position State and Flow Management in Flight Control (항공관제에서 관제석 상태 및 흐름 관리에 관한 연구)

  • Lee, Deok Gyu;Han, Jong-Wook
    • Proceedings of the Korea Information Processing Society Conference
    • /
    • 2013.05a
    • /
    • pp.1124-1125
    • /
    • 2013
  • 본 논문은 비행자료의 상태 및 흐름을 관리하여 내부 혹은 외부의 바이러스의 피해 및 비행자료 변조 및 수정 등의 해킹 발생에서 비행자료 시스템의 가용성, 신뢰성 및 무결성을 강화시켜 비행자료시스템 운영 시 관제 서비스를 마비시키는 다양한 사이버 테레에 대응하여 실시간으로 자동으로 재해를 복구하는 시스템 및 그 방법에 대한 것이다. 관제사가 비행자료 상태 및 흐름 관리함에 있어 비행자료를 일방향으로 상태를 변경하거나, 진행하는 방식이 아닌, 일정 시간동안 비행자료의 시간차를 두어상태를 관리함으로써 비행자료를 보호하여 시스템을 안전하게 운용할 수 있는 장점을 갖는다.

Domestic Application Plan of Fatigue Risk Management System by Air Traffic Controller (항공교통관제사의 피로위험관리시스템 도입에 따른 국내 적용 방안)

  • Lee, Young-Jong
    • Journal of Advanced Navigation Technology
    • /
    • v.23 no.6
    • /
    • pp.501-506
    • /
    • 2019
  • This paper presents a prescriptive alternative for establishing a FRMS suitable for us based on scientific data ahead of the introduction and implementation of the FRMS for air traffic controllers in order to meet the International Civil Aviation Organization (ICAO) international standards. I would like to present. Therefore, we confirmed the operation of each air traffic control agency against the current domestic operating standards, and compared and reviewed the operation methods and standards of air traffic control agencies in each country. The controller in Korea defines 10 hours of working hours per day, 8 hours of minimum breaks, and 40 hours per week. Currently, in the case of air traffic control agencies, the daytime and the appropriate working hours are used in the daytime, but in the nighttime, the average time exceeds 5.9 hours. In the case of 40 hours a week, they work an average of 15.7 hours overtime. By adjusting the nighttime work time, this work can be solved by diversifying the form of the worker's input method according to the personal schedule rather than the two-day (day / night) method, as well as the appropriate nighttime time distribution by supplementing the personnel.

A Study on the air traffic control system of Korea Light Aircraft Carrier (한국형 경항공모함 항공관제체계에 대한 연구)

  • Choi, Youn-chul;Jung, Yong-tae;Cho, Young-jin
    • Journal of Advanced Navigation Technology
    • /
    • v.26 no.5
    • /
    • pp.272-280
    • /
    • 2022
  • An aircraft carrier is a combat ship that acts as an aircraft base at sea and performs combat through aircraft mounted as a military ship operating the aircraft. The Navy proposed a 40,000-ton light aircraft carrier operation plan that could be equipped with vertical takeoff and landing fighter jets and helicopters around 2033, and based on this, this study examined the operation of aircraft control equipment among the aviation support systems required for operating light aircraft carriers in Korea. PriFly, TWR's ILARTS, ILM for airspace control, ASR, PAR, LAAS or RNAV, PALS (JPALS) for access control are required as essential equipment, and communication network and SCATT-16 are required along with URN-25 TACAN, ICLS (El/Az), ACLS OLS, MOVAS, IFLOLS, etc. This study consists of two parts, and part 2 will describe a specific control method on an aircraft carrier.

A Study on the Identification and Improvement of Risk Factors by Region through Case analysis of Safety report in the ROKAF Integrated Air Conrtrol Management System (공군 항공관제통합관리체계 내(內) 안전보고 사례분석을 통한 지역(기지)별 위해요인 식별 및 개선 연구)

  • Hakbong Lee
    • Journal of Aerospace System Engineering
    • /
    • v.17 no.4
    • /
    • pp.34-42
    • /
    • 2023
  • This study aims to analyze safety reports received through the recently added SMS safety self-report in the Air Force's "integrated air control management" system, identify hazards, present improvements by region (base), and lay the foundation for future data-based safety management. To identify risk factors, it was first classified by base based on data classified into 16 groups in the autonomous reporting system, and second classified in detail based on the type and description. Risk factors were analyzed for the most reported control cooperation (306) items, and improvements were derived by dividing risk factors into information sharing, regulations, procedures, education, training, and equipment items based on the analysis results. It was confirmed that risk factors and specific improvements vary by base (12), which is important data that can present statistical analysis and the direction of safety management in the flight control field by base (region). In addition, since there is no data-based risk factor analysis study for each specific base (region), it can be used in the future as basic research data for data-oriented safety management.

A Study on the Design and Realization of a VHF Receiver for Air Traffic Control (항공관제용 VHF대역 수신기 설계 및 구현에 관한 연구)

  • Kang, Suk-Youb;Park, Wook-Ki;Go, Min-Ho;Kim, Yong-Kyun;Song, Byoung-Jin;Park, Hyo-Dal
    • Journal of Advanced Navigation Technology
    • /
    • v.10 no.1
    • /
    • pp.26-33
    • /
    • 2006
  • This paper discusses the design and fabrication of a wireless VHF receiver for use in air traffic control. The VHF receiver was designed and tested in three modules: a control module, a receiver module and a power module, all of which were integrated into a single block for final testing. The fundamental performance of the receiver, and in particular, sensitivity, the most important factor, is designed to satisfy existing commercial wireless transmitter specifications for air traffic control. The receiver displays a sensitivity of -113 dBm, which is higher performance than existing commercial products, and is suitable for use as a basic component of CNS/ATM.

  • PDF

Target Tracking Performance Verification of Surveillance Data Processing System for Air Traffic Control (항공관제용 감시자료처리시스템 항적 추적 성능 검증)

  • Eun, Yeonju;Jeon, Dae-Keun;Yeom, Chan-Hong
    • Aerospace Engineering and Technology
    • /
    • v.11 no.2
    • /
    • pp.171-181
    • /
    • 2012
  • As a sub-system of an air traffic control system, SDP(Surveillance Data Processor) provides with the system tracks of aircraft using the surveillance sensor data from various air traffic surveillance sensors, such as radars. Therefore, the high accuracy of tracking results is a crucial requirement for safe flights, and verification of the required system performance of SDP is an essential step in development. Moreover, the quantitative evaluation of target tracking accuracy is important for newly developed SDP, since there are several tracking methods for Multi-Sensor Multi-Target Tracking, such as MRT(Multi Radar Tracking), inevitably required as the main function of SDP. In this study, definition of required system performances, establishment of test environment, and test results for MRT performance evaluation of SDP, which is being developed in KARI(Korea Airspace Research Institute) are presented.