• Title/Summary/Keyword: 무인항공시스템

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무인항공시스템 인증기술 동향

  • Choe, Ju-Won
    • Current Industrial and Technological Trends in Aerospace
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    • v.4 no.1
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    • pp.100-107
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    • 2006
  • 민간 무인기의 용도는 수색 및 구조, 환경 및 공해감시, 기상 측정, 화재 및 재난의 조기감지, 국경 및 해양정찰, 항공촬영과 지도제작, 농약살포 그리고 교통감시 등 사람이 수행하기 힘든 3D 임무 및 우리의 실생활에 도움을 줄 수 있는 새로운 용도로 개발되고 있다. 그러나 향후 무인항공기의 상업적 성공 여부는 민간 공역으로의 진입 여부에 달려 있으며, 공역 내에서의 자유로운 임무수행을 위해서는 안전성 확보를 위한 감항당국의 인증이 필수요소이다. 이에 항공선진국 들은 민간 무인기의 신뢰성 누적과 인증을 위한 실현 가능한 방법부터 법제도 정비에까지 많은 연구를 수행 중에 있다. 본 글에서는 최근 항공선진국들의 무인항공시스템의 신뢰성 추세와 인증동향 그리고 향후 발전 방향에 대하여 제시한다.

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Development of Portable GCS for UAV (이동형 무인항공기 지상통제 시스템 개발)

  • Choe, Seong-Min;Park, Beom-Jin;Kim, Jung-Uk
    • 한국항공운항학회:학술대회논문집
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    • 2015.11a
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    • pp.47-49
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    • 2015
  • 무인항공기는 일반 유인항공기와는 다르게 크기의 제한이 없다. 또한 작은 사이즈의 무인항공기는 적은 인원의 투입으로도 항공기 각 분야의 검증이 가능하므로 소형화된 무인기는 여러 회사 및 연구원 학교등에서 개발되고 있다. 항공기의 크기가 작아지게 되면 운영요원의 숫자 또한 작아지게 되고 이로 인하여 쉽게 이동이 가능하고 운영이 가능한 이동형 무인항공기 지상통제 시스템의 요구가 생기게 된다. 본 논문에서는 한국항공주우연구원의 소형 무인기를 운영하기 위해 개발한 이동형 무인항공기 지상관제 시스템에 관하여 기술 하였다.

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A Study on the Application of Quality System Standards in the Safety Certification of LUAVs (무인동력비행장치 안전성인증에서 품질시스템 기준 적용 방안 연구)

  • Ji-Hun Kwon;Shin-Duck Kang;Tae-Seok Oh;Seok-Min Pae;Sauk-Hoon Im
    • Journal of Aerospace System Engineering
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    • v.18 no.2
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    • pp.64-70
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    • 2024
  • The demand for safety certification of Light Unmanned Aerial Vehicles (LUAVs), weighing between 25kg and 150kg, is rapidly increasing in Korea. Unfortunately, the number of LUAV safety certification failures is also on the rise, with manufacturing quality issues being identified as the main culprit. However, there is a lack of quality system standards for manufacturers within the LUAV safety certification system. As a result, this paper aims to analyze the domestic safety certification system and the quality standards set by the American Society for Testing and Materials (ASTM) for small Unmanned Aerial Systems (sUAS). The goal is to establish quality system inspection standards specifically tailored for LUAV manufacturers. To achieve this, we propose additional inspection items that reflect the characteristics of the manufacturing quality system. These items will be identified through on-site inspections of LUAV manufacturers, ensuring that the resulting quality system standard aligns with the actual situation of domestic manufacturers. In order to gauge the feasibility and effectiveness of the proposed quality system standard, we conducted a survey of seven domestic LUAV manufacturers.

Soil Volume Computation Technique at Slope Failure Using Photogrammetric Information (영상정보를 활용한 사면 붕괴 토사량 산정 기법)

  • Bibek, Tamang;Lim, Hyuntaek;Jin, Jihuan;Jang, Sukhyun;Kim, Yongseong
    • Journal of the Korean GEO-environmental Society
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    • v.19 no.12
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    • pp.65-72
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    • 2018
  • The uses of unmanned aerial vehicles (UAV) have been expanding in agriculture surveys, obtaining real time updates of dangerous facilities where human access is difficult, disaster monitoring, and 3D modeling. In reality, there is an upsurge in the application of UAVs in fields like, construction, infrastructure, imaging, surveying, surveillance and transportation. Especially, when the slope failure such as landslide occurs, the uses of UAVs are increasing. Since, the UAVs can fly in three dimensions, they are able to obtain spatial data in places where human access is nearly impossible. Despite of these advantages, however, the uses of UAVs are still limited during slope failure. In order to overcome these limitations, this study computes the soil volume change during slope failure through the computation technique using photogrammetric information obtained from UAV system. Through this study, it was found that photogrammetric information from UAV can be used to acquire information on amount of earthworks required for repair works when slope collapse occurs in mountainous areas, where human access in difficult.

Flight Scenario Trajectory Design of Fixed Wing and Rotary Wing UAV for Integrated Navigation Performance Analysis (통합항법 성능 분석을 위한 고정익, 회전익 무인항공기의 비행 시나리오 궤적 설계)

  • Won, Daehan;Oh, Jeonghwan;Kang, Woosung;Eom, Songgeun;Lee, Dongjin;Kim, Doyoon;Han, Sanghyuck
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.30 no.1
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    • pp.38-43
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    • 2022
  • As the use of unmanned aerial vehicles increases, in order to expand the operability of the unmanned aerial vehicle, it is essential to develop an unmanned aerial vehicle traffic management system, and to establish the system, it is necessary to analyze the integrated navigation performance of the unmanned aerial vehicle to be operated. Integrated navigation performance is affected by various factors such as the type of unmanned aerial vehicle, flight environment, and guidance law algorithm. In addition, since a large amount of flight data is required to obtain high-reliability analysis results, efficient and consistent flight scenarios are required. In this paper, a flight scenario that satisfies the requirements for integrated navigation performance analysis of rotary and fixed-wing unmanned aerial vehicles was designed and verified through flight experiments.

Autonomous Flight System of UAV through Global and Local Path Generation (전역 및 지역 경로 생성을 통한 무인항공기 자율비행 시스템 연구)

  • Ko, Ha-Yoon;Baek, Joong-Hwan;Choi, Hyung-Sik
    • Journal of Aerospace System Engineering
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    • v.13 no.3
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    • pp.15-22
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    • 2019
  • In this paper, a global and local flight path system for autonomous flight of the UAV is proposed. The overall system is based on the ROS robot operating system. The UAV in-built computer detects obstacles through 2-D Lidar and generates real-time local path and global path based on VFH and Modified $RRT^*$-Smart, respectively. Additionally, a movement command is issued based on the generated path on the UAV flight controller. The ground station computer receives the obstacle information and generates a 2-D SLAM map, transmits the destination point to the embedded computer, and manages the state of the UAV. The autonomous UAV flight system of the is verified through a simulator and actual flight.

Real-time Linux based Rotor UAV Control Software Development (실시간 리눅스 기반의 회전익 무인항공기 제어 소프트웨어 개발)

  • Park, Kiseok;Park, Joong Hee;Wie, Young Jun;Park, Jungkeun;Moon, Chang Joo
    • Proceedings of the Korea Information Processing Society Conference
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    • 2010.11a
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    • pp.1613-1616
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    • 2010
  • 본 논문은 실시간 운영체제인 Xenomai 를 사용하여, 회전익 무인항공기 소프트웨어 개발에 대한 내용을 설명하고 있다. 실시간 운영체제 사용하여 고정 순위 우선 스케줄링을 채택함으로써 데드라인의 타이밍(Timming) 결정성을 보장하였고, 이기종 시스템과의 호환성과 확장성을 고려하여 POSIX API 를 사용하여 멀티 쓰레드를 구현하였다. 또한 실시간 드라이버 모델(RTDM : Real-Time Driver Model)을 사용하여 획득한 데이터를 실시간 전송이 가능하도록 하였다. 본 논문은 실시간 운영체제를 무인항공기에 적용하고 구현된 비행제어 컴퓨터와 제어 소프트웨어를 비율 단조 스케줄링을 적용하여 무인항공기의 쓰레드들의 응답 속도 및 안정성을 보장하는 방안을 제시하였다.

Study on Revision of Aviation Safety act for RPAS (무인항공기 안전운용을 위한 항공안전법 개정방향에 대한 연구)

  • Hong, Hye-Jung;Han, Jae-Hyun
    • The Korean Journal of Air & Space Law and Policy
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    • v.35 no.3
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    • pp.65-93
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    • 2020
  • With the development of information and communication technology, the unmanned aerial vehicle industry began to attract attention as a new growth industry as it entered the fourth industrial revolution. As the size of the unmanned aerial vehicles and the scope of airspace vary from small drones to large unmanned aerial vehicles, the developed countries such as USA and Europe are developing plans for the integrated operation of manned and unmanned aerial vehicles. ICAO is also working on amendments to the relevant ICAO annexes to establish international standards and recommendations for unmanned aerial vehicles. Korea also needs to prepare for the integrated operation of manned and unmanned aerial vehicles that will come in the future, and for this purpose, it is necessary to review and revise the national regulation systems for the safe operation of unmanned aerial vehicles. This study analyzes the amendments of related annexes discussed on the Remotely Piloted Aircraft System (RPAS) pannel, and suggests the direction of revision of the Aviation Safety Act for the safe operation of unmanned aerial vehicles in comparison with the existing Aviation Safety Act.

Simulation System Design for Integrated Operation of Manned/Unmanned Aerial Vehicles (유무인기 통합 운용 시뮬레이션 시스템 설계 방안)

  • O, Eun-Mi;Kim, Hyeon-Gyeong;Eun, Yeon-Ju;Jeon, Dae-Geun
    • 한국항공운항학회:학술대회논문집
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    • 2016.05a
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    • pp.228-232
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    • 2016
  • 유/무인기가 통합되어 운용되는 환경을 고려한 시뮬레이션 시스템 설계 방안을 제시하였다. 기존의 관제 공역 내의 유인기를 대상으로 하는 항공 교통 시뮬레이션 시스템의 기능과 무인기 시스템의 기본적인 기능을 고려하였으며, 이를 기반으로 유/무인기 복합 운용의 새로운 개념을 적용하여 모의할 수 있는 시뮬레이션 환경을 구성하였다. 모의 환경의 확장성을 고려하여, 무인기는 관제 공역에 진입하여 유인기와 복합 운용되는 무인항공기 시스템과 비관제 영역에서 운용되는 소형 무인비행장치로 구분하여 구성하였다. 시뮬레이션 시스템을 구현하기 위한 운용 개념에 대해 서술하였으며, 이를 기반으로 필요로 하는 주요 기능 요소들을 구성하고 각 요소에서 고려되어야 하는 주요 요구 사항을 제시하였다.

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A Study on Development of Certification Basis for VTOL UAS Based on Analysis of Certification Criteria for Fixed/Rotary Wing UAS and SC-VTOL (고정익/회전익 인증기준 및 수직이착륙 특수기술기준 분석 기반의 수직이착륙 무인항공기 인증기준 개발 방안)

  • Yoo, Minyoung;Kim, Suho;Oh, Yeonkyeong;Jin, Kyunghoon;Lee, Hwan;Kim, Woogyeom;Gong, Byeongho
    • Journal of Aerospace System Engineering
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    • v.15 no.5
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    • pp.16-23
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    • 2021
  • Domestic and foreign manufacturers are developing VTOL UASs in various shapes in line with demand for future technologies. UASs have been developed in a shape classified as fixed/rotary wing, and verified by appropriate certification standards. However, airworthiness certification of recent VTOL UASs is strict with the absence of VTOL-specific certification standards. In this paper, criteria applicable to VTOL UAS were presented through analysis of STANAG-4671 and STANAG-4702, which are certification standards for fixed/rotary wing UAS of the North Atlantic Treaty Organization (NATO) and the Special Condition for VTOL Aircraft (SC-VTOL) of European Aviation Safety Agency (EASA). For this, the categorization criteria of general/fixed-wing/VTOL characteristics were established for each standard item and utilized for analysis.