• 제목/요약/키워드: aviation navigation

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국내 PBN 이행을 위한 대안 항법 적용 방안 (Alternative Positioning, Navigation, and Timing Applicable to Domestic PBN Implementation)

  • 김무근;강자영;장재호
    • 한국항행학회논문지
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    • 제20권1호
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    • pp.37-44
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    • 2016
  • 한국은 성능기반항행 (PBN; performance-based navigation)으로 전환하기 위한 단계적 PBN 이행계획을 2010년에 수립하고 로드맵에 따른 새로운 비행절차를 개발 중에 있다. PBN 비행절차에는 GNSS (global navigation satellite systems), DME (distance measuring equipment), VOR (VHF omnidirectional range), INS (inertial navigation system) 등의 항행시설 (NAVAID; navigation aid)이 활용되는 것으로 되어있다. 그 중에서 GNSS를 이용한 PBN 업무제공이 중심을 이루고 있는 실정이다. 그러나 위성항법신호의 인위적, 자연적 간섭에 의한 취약성이 발견됨에 따라 세계 각국은 다양한 대안항법(APNT; alternative positioning, navigation and timing) 기술을 연구하고 있다. 본 논문에서는 GNSS 신호가 가용하지 않을 경우 기존의 항행시스템으로 지속적인 PBN 운항이 가능한지를 분석하였으며, 결과적으로 국내 일부 공항은 접근 단계 구역에서 대안항법의 구축이 필요한 것으로 나타났다.

우리나라 성능기반항행(PBN) 도입 10년의 성과와 발전에 관한 연구- 성능기반항행 이행계획과 항행계획의 비교를 중심으로 - (A Study on the Performance and Development of Performance-Based Navigation (PBN) in South Korea for 10 Years - Focusing on the Comparison between the PBN Implementation Plan and the Global Air Navigation Plan (GANP) -)

  • 이승준;김현미;김휘양
    • 한국항공운항학회지
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    • 제30권4호
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    • pp.9-22
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    • 2022
  • With the continuous increase in demand for air transport services and the growth of the air transport industry, the International Civil Aviation Organization (ICAO) and its member states are facing social demands to expand the capacity of the air transport system and improve the efficiency of its operation. ICAO developed the concept of Performance Based Navigation (PBN) for the purpose of solving problems related to the function and performance of the navigation system. Member countries established an implementation plan in accordance with the resolutionof the ICAO General Assembly, and South Korea established a Performance-Based Navigation implementation plan in December 2009. This paper evaluates the progress made so far based on Korea's Performance-Based Navigation implementation plan and proposes a development direction for Performance-Based Navigation based on changes in the international environment.

다목적 전 공역 위성항법보정시스템 개발 및 적용에 대한 연구 (A Study on the development and Implementation of Multi-purpose All Airspace Satellite Based Augmentation System (SBAS))

  • 이근영
    • 한국항공운항학회지
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    • 제22권1호
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    • pp.15-21
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    • 2014
  • Modern aircraft air navigation has been changed from the conventional air navigation aid to utilizing Global Navigation Satellite System. For the air navigation of fast moving aircraft, GNSS required extremely high accuracy and reliability. This study reviews the basic concept of Satellite Based Augmentation System which is discussed in the International Working Group of International Civil Aviation Organization and status of some SBAS leading State's case. In addition to that, a progress of SBAS development and implementation in the Republic of Korea was reviewed with pointing out of general hurdles and counter measures.

GNSS 대안항법시스템 요구사항 및 기술 분석 (Alternative PNT Requirements and Technology Analysis)

  • 조상훈;강승은;강자영;고상호
    • 한국항공운항학회지
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    • 제20권3호
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    • pp.28-34
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    • 2012
  • The recent transition to Performance Based Navigation in aviation enhances the accuracy of aircraft position, safety and efficiency in air traffic operations by using satellite-based navigation system such as GNSS. However, intentional interferences with GNSS signal as well as ones coming from natural phenomena such as solar storm increase. GNSS have very low power and therefore their signals are more susceptible to interferences than ground-based navigation signals. This paper introduces requirements of alternative positioning, navigation and timing(APNT) system and relevant technologies when the GNSS signals are not valid.

Nearness Diagram, Limit-Cycle 및 벡터장법을 이용한 이동로봇의 실시간 장애물 회피 (A Real-Time Obstacle Avoidance of Mobile Robot Using Nearness Diagram, Limit-Cycle and Vector Field Method)

  • 김필겸;정윤호;윤재호;지민석;이강웅
    • 한국항행학회논문지
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    • 제10권2호
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    • pp.145-151
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    • 2006
  • 본 논문에서는 동적인 환경에서 돌발 장애물을 회피하는 방법으로 Nearness Diagram, Limit-Cycle 및 벡터장법을 혼합한 새로운 항법을 제안한다. Limit-Cycle 항법은 정면장애물을 회피 하는데 사용되고, 벡터장법은 측면장애물을 회피 하는데 이용된다. 그리고 Nearness Diagram 항법은 로봇의 근접지역장애물을 회피하는데 사용된다. 제안된 항법은 시뮬레이션을 통해 그 성능을 증명하였다.

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ICAO 표준 기반 KASS 운영 상 완화조치 및 연속성 사례 분석 (The Analysis of KASS Operational Mitigation Methods and Continuity Cases Based on ICAO Standards)

  • 최윤정;배동환;윤효중;윤동환
    • Journal of Positioning, Navigation, and Timing
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    • 제13권2호
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    • pp.131-136
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    • 2024
  • This paper deal with a method for calculating the continuity of Korea Augmentation Satellite System (KASS), which was completed in Korea in December 2023, and a plan to respond in the event that a continuity hazard situation occurs during operation. For this purpose, the International Civil Aviation Organization (ICAO) Satellite Based Augmentation System (SBAS) continuity standards, Wide Area Augmentation System (WAAS), and European Geostationary Navigation Overlay Service (EGNOS) continuity cases are examined in this paper. According to the measures recommended by the ICAO, when the number of continuity risks exceeds a certain level and the level drops drastically, various mitigation operations by country are implemented. Through this, if KASS does not meet ICAO continuity standards in the future, such measures can be referred to. In addition, this paper computes the short-term KASS continuity during the test broadcast period. Although continuity does not meet the ICAO standards, although this test period is too short, further meaningful analysis in the future is required. Additionally, this paper carried out an analysis of the timing and period to systematically calculate the meaningful value of continuity.

조종사의 위성항행시스템 적응방안에 관한 연구 (A Study on the Pilot's Adaptation for GPS Operation)

  • 한경근;송병흠
    • 한국항공운항학회지
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    • 제7권1호
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    • pp.7-18
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    • 1999
  • The FAA, along with the ICAO and other members of the civil aviation community, has recognized that a GNSS will provide the primary stand-alone navigation system in the 21st Century. FAA has initiated plans to transition from its present ground-based navigation and landing system to satellite-based using signals generated by the GPS. In spite of some risks, GPS users are increasing rapidly. About 52 aircraft equipped with various GPS in their system and wide spread of GPS may be expected in Korea. However, the regulations concerning with CPS implementation were not established by the government. Another problem is GPS receiver's interface. The user interface, operating method and capability vary with GPS class and model. As a direct operator for the system, pilots have to ensure these limitations and rules for efficient adaptation and safety. The issues identified by the study are highly interrelated, and are evidence of aviation system problem. To treat one issue in isolation may improve certain aspects of the aviation system, but will ultimately fail to fundamentally increase the safety and efficiency for the system.

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정밀항법 시스템 설계 및 알고리즘 검증 (Design and Algorithm Verification of Precision Navigation System)

  • 정성균;김태희;이재은;이상욱
    • 한국항공운항학회지
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    • 제21권1호
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    • pp.8-14
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    • 2013
  • As GNSS(Global Navigation Satellite System) is used in various filed, many countries establish GNSS system independently. But GNSS system has the limitation of accuracy and stability in stand-alone mode, because this system has error elements which are ionospheric delay, tropospheric delay, orbit ephemeris error, satellite clock error, and etc. For overcome of accuracy limitation, the DGPS(Differential GPS) and RTK(Real-Time Kinematic) systems are proposed. These systems perform relative positioning using the reference and user receivers. ETRI(Electronics and Telecommunications Research Institute) is developing precision navigation system in point of extension of GNSS usage. The precision navigation system is for providing the precision navigation solution to common users. If this technology is developed, GNSS system can be used in the fields which require precision positioning and control. In this paper, we introduce the precision navigation system and perform design and algorithm verification.

AEDT (aviation environmental design tool)을 이용한 김해 국제공항 신 활주로 소음 분석 (Noise Analysis of New Runway at the Gimhae International Airport using Aviation Environmental Design Tool (AEDT))

  • 임은하;황호연
    • 한국항행학회논문지
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    • 제22권5호
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    • pp.343-350
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    • 2018
  • 한국의 공항 중 이용객 수 기준으로 4위 공항인 김해 국제공항은 국제선 이용객수가 점차 증가하고 있다. 이에 따라 동남권 신공항에 대한 필요성이 제기되었고, 국토교통부는 현재 김해 국제공항에 새로운 활주로 1본을 건설하여 확장하기로 결정하였다. 따라서 이로 인해 야기되는 소음을 예측하기 위해 본 연구에서는 FAA (Federal Aviation Administration)의 AEDT (aviation environmental design tool) 소프트웨어를 이용하여 소음 분석을 수행하였다. 본 논문에서는 김해 국제 공항에 신 활주로 건설 시 하루 동안의 항공기 이착륙 자료를 이용하여 현재보다 증가하는 소음 피해지역을 예측하였다.

ECCAIRS 5 Data를 활용한 최근 10년간 항공 사고·준사고 사례분석 (Case Analysis of the Aviation Accident·Incident During the Last 10 Years Using the ECCAIRS 5 Data)

  • 홍승범;최연철
    • 한국항행학회논문지
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    • 제18권4호
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    • pp.334-340
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    • 2014
  • 최근 항공 안전의 발전에도 불구하고, 항공기 사고의 뚜렷한 감소 추세 없이 유지되고 있다. 따라서 국제적인 항공안전관리의 방향은 기존의 항공안전 방식을 탈피하여 자료에 근거하여 분석된 요소들을 통하여 사고예방을 위한 위험요소를 제거하는 것에 관심을 가지고 있다. 본 논문은 전 세계적으로 항공안전 데이터의 보고와 교환을 위한 표준이 되고 있는 ECCAIRS를 소개한다. 또한 최근 10년간의 국내 항공사고 데이터를 활용하여 항공기 분류별(고정익과 회전익)로 항공기 사고와 준사고의 분포, 연도별 및 월별 사고 분포, 비행 단계 분포, 그리고 분류체계 분포 등에 대한 경향을 분석한다. 본 논문의 항공기 사고와 준사고의 추세 분석은 향후 추구해야 할 정량적인 안전관리의 유용한 방향이 될 것이다.