• Title/Summary/Keyword: 항공운항시스템

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Preliminary Study of Ionosphere for Global Navigation Satellite Systems (위성항법시스템 적용을 위한 전리층 기본 연구)

  • Yang, T.H.;Lee, Y.J.;Jun, H.S.;Nam, G.W.;Kim, J.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.14 no.1
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    • pp.55-62
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    • 2006
  • Ionospheric signal delay is a critical factor for precision differential GNSS(Global Navigation Satellite Systems) applications such as GBAS(Ground-Based Augmentation System) and SBAS (Satellite-Based Augmentation System). Most concern is the impact of the ionospheric storm caused by the interaction between Solar and geomagnetic activities. After brief description of the ionosphere and ionospheric storm, ionospheric models for SBAS are discussed. History of recent ionospheric storms is reviewed and their impact on GNSS is discussed. In order to support Korean GNSS augmentation system development, a preliminary study on the regional ionosphere performed. A software tool for computing regional ionospheric maps is being developed, and initial results during a recent storm period is analyzed.

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Application of GNSS Non-Precision and Precision Approaches to a Circle-to-Land Approach Airport (선회착륙공항에서의 GNSS 비정밀접근 및 정밀접근 적용 연구)

  • Kim, Y.M.;Kang, J.Y.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.12 no.3
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    • pp.65-85
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    • 2004
  • Circling to land is a relatively dangerous maneuver. It contains the worst elements of IFR flight. There is a minimum obstruction clearance, a limited space in which to maneuver, an absence of visual reference, and trying to keep the runway in sight while preparing to land. At night it is quite a bit more than dangerous. The required continuous turn in marginal conditions that keeps the airport in sight is hazardous. Therefore, this paper proposes an application of GNSS to circling approach to reduce or remove chances of accidents which may occur under such unfavorable flight conditions. The study reviews relevant documents published by ICAO and FAA and provides scenarios for non-precision and precision approaches and circling approach based on the GNSS for Kimhae airport. Also requirements for the ground facility design are studied and provided.

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The Research on the Latent Failure to Improve Human Factors of the Helicopters (회전익 항공기 인적요인 향상을 위한 잠재원인에 관한 연구)

  • Choi, Jin-Kook;Byeon, A-Reum
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.25 no.4
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    • pp.195-203
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    • 2017
  • Around 70% of domestic aircraft accidents in helicopter aircraft. The causal factors of the helicopter accidents are identified as human factors. People have focused mostly on unsafe acts to prevent the accident. The accidents should be analysed on human factors to reduce accident. The unsafe acts can be managed effectively if the latent failures were identified through the HFACS. This paper is to introduce about the latent failure classified by the HFACS and provide the analysis regarding the latent failure of the helicopters by the aviation safety advisors through the interviews.

A Study on CNS/ATM and Performance Based Navigation (위성항법시스템과 성능기반항법에 대한 고찰)

  • Kim, Chang-Hwan;Jeong, Jong-Chul;Kang, Ja-Young
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.18 no.1
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    • pp.45-50
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    • 2010
  • Air Traffic Management aims to fulfill the requirement of the aviation demander by constructing the most effective and safety aviation systems for providing safety and cost-effective service. All concerned parties of aviation present the needs of improving Air Traffic Management system for solving the issue of the current system and the air traffic capacity in the 21st century, and introduce the significant improvements from the conventional technology and method for the past 40 years. Accordingly, ICAO promotes the development of innovative procedures and technologies to solve the problems and meet the demands. It is the concept of Performance based Navigation(PBN) based on Communication, Navigation, and Surveillance/Air Traffic Management(CNS/ATM). This study defines differences between RNAV and RNP RNAV as methods of air navigation based on the CNS/ATM, and needs and requirements of PBN as an emerging global standard. It also outlines basic elements supporting and implementing the PBN concept.

A Study on the Autonomous Powered Ram Air Parafoil System Considering Wind Effect (바람 효과를 고려한 동력 램에어 파라포일 자동비행 시스템 연구)

  • Kim, Tae-Wook;Song, Yongkyu;Jeong, Dongho;Gwon, Oseong
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.24 no.1
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    • pp.55-61
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    • 2016
  • In this work a guidance and control system for an a powered ram air parafoil under wind disturbance is considered. After analyzing a 6 Dof and 9 Dof nonlinear dynamic models of the parafoil, wind effect is added to them. In order to actively respond to the wind acting on the transverse direction of the vehicle a new guidance algorithm is proposed. After a Hardware-In-the-Loop Simulation (HILS) study, flight tests are performed to demonstrate its potential under wind disturbances.

Sensor Redundancy Management using Kalman Filter for a Duplex Filght Control System (칼만필터를 이용한 2중 비행제어시스템의 센서 다중화 관리)

  • Lee, Seung-Hyun;Lee, Jang-Ho;Kim, Eung-Tae;Sung, Ki-Jung
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.18 no.4
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    • pp.9-15
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    • 2010
  • This paper presents a duplex flight control system of design concepts and sensor fault detection algorithm using Kalman Filter. The algorithm was verified to use HILS that is composed of two FCCs, motion table, visualization system, cockpit, and flight model computer. The FCC was developed to be able to mount on small aircraft.

FBW System and Operational Flight Program Development for Small Aircraft (소형항공기를 위한 FBW 시스템과 비행운영 프로그램 개발)

  • Lee, Seung-Hyun;Kim, Eung Tai;Seong, Kiejeong
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.1
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    • pp.1-7
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    • 2013
  • To have the competitiveness in the future worldwide small aircraft market, we should be able to develop the aircraft which is highly safe, easy to fly, and having excellent flight characteristics. FBW(Fly-By Wire) system is essential for the enhancement of flight safety and control easiness. FBW system that has been applied only to the modern fighter and transport aircraft is recently applied to smaller aircraft such as regional aircraft, business aircraft and even small aircraft. The purpose of this research includes the development of flight control computer, the definition of FBW system component, the design concept of each component for redundant management, OFP(Operational Flight Program) development, FBW system integration and HILS(Hardware In-the Loop Simulation) verification environment to test this FBW system.

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

  • Jeong, Seongkyun;Kim, Taehee;Lee, Jae-Eun;Lee, Sanguk
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.1
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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.

A Tracking Filter Design of the Radar Beacon System for Automatic Take-off and Landing of Unmanned Aerial Vehicle (무인항공기 자동이착륙을 위한 레이다 비콘 시스템의 추적필터 설계)

  • Kim, Man-Jo;Hwang, Chi-Jung
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.1
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    • pp.23-29
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    • 2013
  • This paper presents a tracking filter of radar beacon system (RBS) for automatic takeoff and landing of an unmanned aerial vehicle. The proposed tracking filter is designed as the decoupled tracking filter to reduce the computational burden. Also, an adaptive estimation method of the measurement error covariance is proposed to provide an improved tracking performance compared to the conventional decoupled tracking filter whenever the accuracy of RBS observations is degraded. 100 times Monte Carlo runs performed to analyze the performance of the proposed tracking filter in case of normal operation and degraded operations, respectively. The simulation results show that the proposed tracking filter provides the improved tracking accuracy in comparison with the conventional decoupled tracking filter.

The Study on the quality of the system and Information in the Airline transportation industry -Focused on KARST- (도심공항터미널의 시스템 및 정보 품질에 관한 연구 -KARST를 중심으로-)

  • Park, Hye-Yoon;Park, So-Yeon;Kim, Min-Su
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.2
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    • pp.72-84
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    • 2013
  • The purpose of the research was to examine how the quality of service provided by the employee and KARST dealing with the quality of the systems and the information systems affect the satisfaction of the users. Second purpose was to find out which of three factors play greater or lesser roles in affecting the customers of the KARST by examining customer satisfaction and the causal relationship between them so that it can aid in finding areas that need to be further developed or improved when designing and operating airports as well as improve customer service by KARST employees.