• Title/Summary/Keyword: 무인항공 시스템

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On-site Demonstration of Topographic Surveying Techniques at Open-pit Mines using a Fixed-wing Unmanned Aerial Vehicle (Drone) (고정익 무인항공기(드론)를 이용한 노천광산 지형측량 기술의 현장실증)

  • Lee, Sungjae;Choi, Yosoon
    • Tunnel and Underground Space
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    • v.25 no.6
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    • pp.527-533
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    • 2015
  • This study performed an on-site demonstration of the topographic surveying technique at a large-scale open-pit limestone mine in Korea using a fixed-wing unmanned aerial vehicle (UAV, Drone, SenseFly eBee). 288 sheets of aerial photos were taken by an automatic flight for 30 minutes under conditions of 300 m altitude and 12 m/s speed. Except for 37 aerial photos in which no keypoint was detected, 251 aerial photos were utilized for data processing including correction and matching, then an orthomosaic image and digital surface model with 7 cm grid spacing could be generated. A comparison of the X, Y, Z-coordinates of 4 ground control points measured by differential global positioning system and those determined by fixed-wing UAV photogrammetry revealed that the root mean squared errors were around 15 cm. Because the fixed-wing UAV has relatively longer flight time and larger coverage area than rotary-wing UAVs, it can be effectively utilized in large-scale open-pit mines as a topographic surveying tool.

미 유군 항공과 Objective Force-달라진 육군과 코만치 헬기의 필수적 역할

  • Heo, Gyeong
    • Defense and Technology
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    • no.1 s.287
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    • pp.86-93
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    • 2003
  • Objective Force의 모든 측면에서 볼 때, 육군항공은 절대 필요한 구성요소이다. 통합개념팀(Intergrated Concept Team)은 현재 Alabama주 Fort Rucker에서 미래 항공력에 대한 작전적 및 조직적(O & O : Operational and Organizational) 개념을 개발하고 있는 중이다. 이러한 노력은 무인항공기, 공중기동수송기, Loitering Attack Munition – Aviation, 새로운 군수 및 공중수송서비스 등과 같은 최근에 생겨난 개념과 시스템들을 획득하는데 목적이 있다.

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Ground Test of the Flight Control System Using PC104 (PC104를 이용한 비행제어 시스템 개발을 위한 지상시험)

  • Heo, Chi-Hoon;Roh, Min-Shik;Cho, Kyeum-Rae;Lee, Dae-Woo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.5
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    • pp.452-459
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    • 2007
  • This paper presents the flight control system using a PC104 with GPS and IMU. This System includes an Auto/Manual conversion module by PIC16 for safety, and homing type guidance algorithm to flight toward a scheduled target. We verify the performance of the flight control system via ground test, and present the possibility of application into UAV control system via comparison with the commercial system.

Comparison of Topographic Surveying Results using a Fixed-wing and a Popular Rotary-wing Unmanned Aerial Vehicle (Drone) (고정익 무인항공기(드론)와 보급형 회전익 무인항공기를 이용한 지형측량 결과의 비교)

  • Lee, Sungjae;Choi, Yosoon
    • Tunnel and Underground Space
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    • v.26 no.1
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    • pp.24-31
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    • 2016
  • Recently, many studies have been conducted to use fixed-wing and rotary-wing unmanned aerial vehicles (UAVs, Drones) for topographic surveying in open-pit mines. Because the fixed-wing and rotary-wing UAVs have different characteristics such as flight height, speed, time and performance of mounted cameras, their results of topographic surveying at a same site need to be compared. This study selected a construction site in Yangsan-si, Gyeongsangnam-do, Korea as a study area and compared the topographic surveying results from a fixed-wing UAV (SenseFly eBee) and a popular rotary-wing UAV (DJI Phantom2 Vision+). As results of data processing for aerial photos taken from eBee and Phantom2 Vision+, orthomosaic images and digital surface models with about 4 cm grid spacing could be generated. Comparisons of the X, Y, Z-coordinates of 7 ground control points measured by differential global positioning system and those determined by eBee and Phantom2 Vision+ revealed that the root mean squared errors of X, Y, Z-coordinates were around 10 cm, respectively.

The Development of Performance Analysis Code for Pre-Conceptual Design of VTOL UAV (수직이착륙/고속순항 무인기 초기개념설계를 위한 성능예측 프로그램 개발)

  • Jung, Won-Hyung;Lee, Kyung-Tae;Kim, Jung-Yub
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.5
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    • pp.1-9
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    • 2004
  • The performance analysis code has been developed for vertical take-off and landing(VTOL) UAV which can be utilized as a trade analysis tool in the pre-conceptual design phase. The UAV requires VTOL capability and high speed cruise performance. The main logic of this performance analysis code is to estimate performance parameters of each mission segment by mission fuel weight iteration. The reliability of this performance analysis code is discussed by comparing the data of existing dual flight mode VTOL UAVs such as Boeing CRW and Bell Tilt Rotor.

Uniformity Analysis of Unmanned Aerial Application with Variable Rate Spray System (무인항공 변량방제 시스템의 살포 균일도 분석)

  • Koo, Young Mo;Bae, Yeonghwan
    • Journal of agriculture & life science
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    • v.52 no.6
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    • pp.111-125
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    • 2018
  • In this study, we evaluated the uniformity of deposition rate and particle size distributions of the variable rate application technique using the unmanned rotorcraft by measuring the spray pattern according to path location in the range of spraying flight. The coefficient of variation (CV) of the lateral coverage rate for the overlapped distribution with the spray swath of 3.6 m in both guidance and auto-pilot flight modes maintaining constant flight speed was about 30% and the CV of the coverage rate by the flight path location was extremely small. Therefore, it was assessed that the variable rate application technology compensating for the variation of ground speed was superior in terms of spray uniformity. In addition, the droplet size distributions in both volume median diameter(VMD) and number median diameter(NMD) were adequate for aerial application and uniform in terms of lateral distribution. Thereafter, we intend to contribute to a precise application on small-scaled fields using the unmanned agricultural rotorcraft by the variable rate application.

Unmanned Parking System with Automatic Parking (자동주차가 가능한 무인 주차 시스템)

  • Kim, Tae-Sun;Park, Yong-heui;Park, Jun-Hyung;Im, Hye-Jin;Shim, In-Bo;Hwang, Hyun-Woo
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2019.07a
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    • pp.235-236
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    • 2019
  • 스마트화 시대로 인해 주차장에서 운전자가 불편함을 줄여줄 수 있는 많은 기능들이 추가되었으나, 여전히 해결되지 못한 불편함은 많이 남아있다. 그 중 협소한 주차 공간에서 발생하는 접촉 사고와 차량을 주차하는데 많은 시간을 소모하는 불편함이 남아있다. 주차 공간 부족으로 인해 아파트 입구와 갓길, 소방차 지정구역에도 차량을 주차하는 등 많은 문제가 발생하고 있다. 아파트 입구의 주차된 차량들로 인해 운전자는 갑자기 튀어나온 어린이들을 발견하지 못하는 사고가 발생한다. 또한 갓길과 소방차 지정구역의 주차로 인해 화재 발생 시 소방차가 진입하지 못하여 화재 진압에 영향을 주어 2차 피해가 발생 하고 있다. 최근 몇 년간 부족한 주차 공간으로 인해 발생하는 문제를 해결하기 위해 소방법 강화 및 지정 주차구역, 주차 요일제 등을 시행하고 있으나, 주차 공간을 증가 시키는 등 직접적인 주차 공간 해결에는 많은 노력을 기울이지 않고 있다. 이러한 사고 피해를 예방하기 위한 연구의 중심으로써 주차 구역으로 설정하였으며, 자동화와 편의성을 추가하고자 하였다. 무인 주차 시스템의 자동화 구현을 위해 아두이노 개발환경에 3가지 센서를 적용하였으며, 편의성을 높이기 위해 RFID카드를 이용한 차량 정보 인식 기능을 적용하였다.

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Application of Geospatial Information Utilization System using Unmanned Aerial Image (무인항공 영상을 이용한 공간정보 응용 시스템 활용 방안)

  • Lee, Keun-Wang;Park, Joon-Kyu
    • Journal of Digital Convergence
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    • v.17 no.2
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    • pp.201-206
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    • 2019
  • Korea is constructing geospatial information application system for geospatial information utilization, but it is trying to establish a system for joint use of geospatial information system centering on Ministry of Land Transport and Transport due to the problem of sharing. The purpose of this study is to investigate and analyze the geospatial information application system operated by local governments, and to suggest the application of geospatial information application system using unmanned aerial images. As a result of the research, it was found that the functions of existing spatial information application system are concentrated on the public services and it is difficult to share and utilize data between administrative departments. In addition, the utilization of the system using unmanned aerial image has been suggested, and additional functions such as vector display, area calculation, and report generation have been derived to improve the usability of geospatial information application system. If additional functions of spatial information application system are added through further studies in the future, it will be possible to use it as a basic data of field survey and policy decision in related fields. And non-experts will be able to improve the efficiency of work by utilizing highly accurate geospatial information in various fields.

A Study on Experimental Special Airworthiness Certification for Unmanned Aircraft Systems (무인항공기시스템의 실험분류 특별감항증명 제도에 관한 고찰)

  • Choi, Mijin
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.28 no.4
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    • pp.55-62
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    • 2020
  • Special airworthiness certificates can be issued if the aircraft does not meet the airworthiness standards, but it is deemed that it can be operated safely by partially limiting the scope of operation and flight performance. Currently, Korea is subject to experimental special certification for UAS(Unmanned Aircraft Systems) exceeding 150 kg of its own weight, but detailed guidelines need to be prepared on how to prove that they can be operated safely in a limited range. Recently, Korea Airworthiness Standard(KAS) Part 21 has been revised to reflect this, but it needs to be supplemented. In this study, through an understanding and analysis of the FAA's procedure of expeirmental special airworthiness certifications for UAS, we would like to suggest what we should consider when developing relevant guidelines in our country.

Study on Practical Design of Datalink in Interoperable UAV Systems (무인기 상호운용시스템에서 실용적인 데이터링크 설계방안 연구)

  • Kyu-Hwan Lee;Myeonggeun Oh;Jihoon Kim
    • Journal of the Korea Institute of Military Science and Technology
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    • v.27 no.1
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    • pp.51-59
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    • 2024
  • Uumanned aerial vehicle(UAV) systems have been used in various fields including industry and military. According to increasing the number of UAVs, the attention on interoperable UAV systems is increasing. In this paper, we propose the practical design of datalink in interoperable UAV systems. For practical design, we firstly review the operational scenarios in the interoperable UAV system. We then propose the system model of the datalink in interoperable UAV system. Consequently, the technical components such as the design of the network, the link management, the support of the multicast transmission, the support for autonomous mission and flight safety, and the datalink security are derived and reviewed for the practical design.