• Title/Summary/Keyword: 무인항공 시스템

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Research and development of safety corridor simulation environment for Chungbuk-type UAM using GAZEBO (GAZEBO를 활용한 충북형 UAM의 안전회랑 시뮬레이션 환경 연구 개발)

  • Jeonghun Lee;Hoseop Lee;Jaeeun Kim;Hyejeong Lim;Sungwook Cho
    • Journal of Aerospace System Engineering
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    • v.17 no.2
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    • pp.103-110
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    • 2023
  • In order for future UAVs to be used as means of transportation, a simulation environment in which they can be tested in advance is essential. Accordingly, to demonstrate future air transport systems among six future industries of Chungcheongbuk-do, a simulation environment was condensed and built, focusing on virtual safety corridor connecting Osong Station and Cheongju Airport.

Air Transport Rack Design and Temperature Test Study for UAV (무인항공기용 ATR 설계 및 온도시험에 관한 연구)

  • Kim, Sung-Su;Kim, Do-Yul;Choi, Kee-Young;Park, Choon-Bae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.3
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    • pp.253-259
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    • 2007
  • Standard design and suitable environmental test method should be applied to increase the reliability of UAV flight control systems. UAV flight control systems under development domestically have enough capabilities for complicated missions. However, most low cost systems are not designed with concepts of compatibility, adaptability, and environmental compliance. This paper explains ATR(Air Transport Rack) standard that is widely used on aircraft. The paper presents a design uses commercial off-the-shelf parts. The paper also presents various environmental standards for airborne equipments, including U.S. military specifications. The developed FCS was tested under these specifications. The paper shows the test procedures and results.

Development Trend of the Autonomous Flight Control Technology (자율비행기술 동향)

  • Seong, Kie-Jeong;Kim, Eung-Tai;Kim, Seong-Pil
    • Current Industrial and Technological Trends in Aerospace
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    • v.6 no.2
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    • pp.143-153
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    • 2008
  • This paper describes the current research trend and future development direction of autonomous flight of the aircraft. The autonomous flight means that aircraft control system recognize and cope with the emergency situation confronted during the flight by itself. Current research for autonomous flight technology is mainly performed for the application to unmanned air vehicle. Considering advent of future air traffic management system and increasing demand of the unmanned air vehicle application, however, autonomous flight technology required to be combined with future air traffic management system. In this paper, the current air traffic management system and anticipating change in future air traffic management system was investigated and research activities of autonomous flight technology was described as well as future prospect.

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항공기 자동 착륙방식에 대한 비교

  • Yun, Seok-Jun
    • The Journal of Aerospace Industry
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    • s.65
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    • pp.89-106
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    • 2003
  • 항공기의 자동 착륙 알고리즘을 위한 고 정밀 유도방식에 IBLS(Integrity Beacons Landing System)나 MLS(Microwave Landing System)와 같은 유도 제어 방식을 사용하여 유인 항공기나 무인 항공기의 유도 착륙에 사용하고 있다. 당 연구에서는 무인항공기의 자동 착륙을 위한 실제적인 요구사항들이 분석되었고, 자동 착륙 유도장치로 IBLS와 MLS가 선택되어 각각의 기능과 특성들이 수학적으로 모델링 되었다. 또한 고전제어와 최적제어의 2가지 방식으로 무인항공기의 자동 착륙을 통제하기 위한 autopilot이 설계되어 그 유효성과 특징들이 분석되었다. IBLS, MLS, autopilot, 그리고 이러한 자동 착륙 유도제어 시스템이 적용되는 대상체인 무인항공기와 대기환경 및 외란에 대한 수학적 모델들은 Simulink와 ANSI C를 사용하여 단위 S/W 모듈들로 작성되었고, 여기에 GUI모듈이 추가되어 하나의 통합 시뮬레이션 S/W가 완성되었다. 모의시험평가는 총 2단계로 구성되었는데, 대기 외란이 주어졌을 때 IBLS와 MLS의 유효성을 1차적으로 검증하였고, 2단계 모의수치실험에서는 MLS 유도센서 방식에 따른 고전제어기 및 최적제어기의 항공기 종 방향 운동에 대한 강인성 비교를 시도하였다.

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A Study on the Wind Estimation for Unmanned Parafoil System (무인 파라포일 시스템을 위한 바람 추정 기법 연구)

  • Kim, Tae-Wook;Song, Yong-Kyu
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.23 no.1
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    • pp.8-13
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    • 2015
  • In this paper, a simple algorithm is proposed to estimate wind speed and direction which can significantly improve the landing performance of an unmanned parafoil. The proposed algorithm is applied to flight test data along with other known algorithms and the results are compared and discussed. The proposed algorithm shows comparable performance while it can still be applied to the parafoil under control.

Aircraft design and manufacturing for UAV (무인 항공기 기체 설계 및 제작)

  • Hwang, Hyun-Su;Heo, Seop;Kim, Jong-Hyuk;Bae, Jae-Sung
    • Journal of Aerospace System Engineering
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    • v.2 no.4
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    • pp.38-43
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    • 2008
  • Since UAV has been developed, the demand of uav is increasing because of the advantage which are no injury people and less cost. Also, it has easy maintenance and adaptation because it will carry out each mission by only change payload. So, in this study, we performed aircraft design and manufacturing which it could have maximum payload weight when consider each mission has different weight of payload

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Acquiring Precise Coordinates of Ground Targets through GCP Geometric Correction of Captured Images in UAS (무인 항공 시스템에서 촬영 영상의 GCP 기하보정을 통한 정밀한 지상 표적 좌표 획득 방법)

  • Namwon An;Kyung-Mee Lim;So-Young Jeong
    • Journal of the Korea Institute of Military Science and Technology
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    • v.26 no.2
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    • pp.129-138
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    • 2023
  • Acquiring precise coordinates of ground targets can be regarded as the key mission of the tactical-level military UAS(Unmanned Aerial System) operations. The coordinates deviations for the ground targets estimated from UAV (Unmanned Aerial Vehicle) images may depend on the sensor specifications and slant ranges between UAV and ground targets. It has an order of several tens to hundreds of meters for typical tactical UAV mission scenarios. In this paper, we propose a scheme that precisely acquires target coordinates from UAS by mapping image pixels to geographical coordinates based on GCP(Ground Control Points). This scheme was implemented and tested from ground control station for UAS. We took images of targets of which exact location is known and acquired the target coordinates using our proposed scheme. The experimental results showed that errors of the acquired coordinates remained within an order of several meters and the coordinates accuracy was significantly improved.

Automatic Flight Control System Development for Optionally Piloted Vehicle (유무인 겸용 비행체의 자동비행조종시스템 개발)

  • Lee, Sangjong;Choi, Hyoung Sik;Seong, Kie-Jeong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.11
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    • pp.968-973
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    • 2014
  • Optionally Piloted Vehicle is one of the UAV development technology and method, which can provide the economic and efficient unmanned system. Existing manned aircraft is evaluated through much flight operations and it can supply the reliable aircraft platform, engine and subsystems for operation. In addition, OPV can be operated both manned and unmanned vehicle to satisfy the mission requirement. under the certain flight conditions. This paper describes main development procedures for automatic flight control system of OPV and summarizes the technical issues and results.

The study of drone's navigation and 𝜇­ - UTM of the vertical SKYWAY based on the ground highway and traffic system (지상도로망의 상공 확장기반 가상 SKYWAY 항법 및 관제체계(𝜇 - UTM)에 관한 연구)

  • Lee, Sang-Gi;Jo, Yeong-Seon;Hong, Dan-Bi
    • 한국항공운항학회:학술대회논문집
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    • 2016.05a
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    • pp.233-239
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    • 2016
  • NASA(미국 항공우주청)를 중심으로 무인항공기교통관리(UTM) 체계를 이용한 드론 항공교통통제 모의시험을 진행하고 있다. 국내에서도 2017년부터 안전한 무인항공기교통관리(UTM) 체계 구축을 위한 '저고도 무인기 감시관리 기술 개발 및 시스템 시범 운용사업'을 진행할 예정이다. 본 논문은 지상도로망을 버드뷰(Birdview)처럼 내려다보며 비행할 수 있는 저고도 드론이 안전하고 효율적인 운항을 보장하기 위해서는, 상공에 장애물이 없는 지상도로망의 상공에 가상도로망과 가상신호체계를 확장시킨 한국형 가상 'SKYWAY' 항법 및 관제 체계(${\mu}$ATM)에 관한 기획 연구에 관한 것이다.

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Validation on the Utilization of Small-scale Unmanned Aerial Systems(sUAS) for Topographic Volume Calculations (토공량 산정을 위한 소형무인항공시스템의 활용성 평가)

  • Lee, Yong-Chang
    • Journal of Cadastre & Land InformatiX
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    • v.47 no.1
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    • pp.111-126
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    • 2017
  • Small-scale UAS(Fusion technique of Unmanned Aerial Vehicles platform and Sensors, 'sUAS') opens various new applications in construction fields and so becoming progressively common due to the considerable potentials in terms of accuracy, costs and abilities. The purpose of this study is that the investigation of the validation on the utilization of sUAS for earth stockpile volume calculations on sites. For this, generate 3D models(DSM) with sUAS aerial images on an cone shaped soil stockpile approximately $270m{\times}300m{\times}20m$, which located at Baegot Life Park in Siheung-si, compared stockpile volume estimates produced by sUAS image analysis, against volume estimates obtained by GNSS Network-RTK ground surveying method which selected as the criteria of earth stockpile volume. The result through comparison and examination show(demonstrate) that there was under 2% difference between the volume calculated with the GNSS Network RTK data and the sUAV data, especially sUAS imaged-based volume estimate of a stockpile can be greatly simplified, done quickly, and very cost effective over conventional terrestrial survey methods. Therefore, with consideration of various plan to assess the height of vegetation, sUAS image-based application expected very useful both volume estimate and 3D geospatial information extraction in small and medium-sized sites.