• Title/Summary/Keyword: 무인항공시스템

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Lightweight Metallic Bipolar Plates of PEMFC for a Small Reconnaissance UAV (소형 정찰 UAV를 위한 고분자 전해질막 연료전지의 경량의 금속 분리판)

  • Kim, Ki-In;Lee, Jong-Kwang;Jang, Bo-Sun;Kwon, Se-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.10
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    • pp.1031-1037
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    • 2010
  • This paper proposed lightweight aluminum bipolar plates as an alternative for conventional graphite bipolar plates in fuel cell systems used as a power source for small reconnaissance UAVs. Since bipolar plates occupy more than 80% of the total weight of the fuel cell system, lightweight aluminum bipolar plates can improve the overall payload and flight time of the fuel cell UAV. The aluminum and graphite bipolar plates were fabricated to compare the performance of each of them. A 15% higher performance per weight was obtained from aluminum bipolar plates than the graphite bipolar plates. Also, the performance of a single cell using aluminum bipolar plates was evaluated under various operating conditions.

Static Aerodynamics-Structure Coupling Analysis of a 3D Flexible Wing Flying at Low Speed (저속 비행 3차원 유연날개 정적 공력-구조 연계해석)

  • Han, Hyungseok;Park, Joohee;Lee, Nawon;Han, Cheolheui
    • Journal of Aerospace System Engineering
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    • v.9 no.2
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    • pp.1-6
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    • 2015
  • 태양광 고고도 장기체공형 무인기나 인간동력 항공기 등에 사용되는 높은 종횡비를 가진 유연날개는 공력 및 구조 상호작용으로 인하여, 구조적 비선형 처짐 및 양력감소 등의 문제가 발생한다. 본 연구에서는 저속 비행하는 높은 종횡비를 가진 날개의 단방향 공력-구조 연계해석을 수행하였다. XFOIL을 사용하여 공력천이현상을 포함한 저 레이놀즈수 익형 공력특성 자료 확보를 기반으로 3차원 양력선 이론을 사용하여 공력해석 연구를 수행했다. 구조해석은 상용소프트웨어 ANSYS를 사용하여 구조변형이나 응력해석 연구를 수행했다. 단방향 공력-구조 연계해석 결과를 바탕으로 인간동력 항공기 주 날개의 형상설계 연구를 수행했다.

A Study on Manufacturing Methods of Cocuring Composite Wings of Solar-Powered UAV (복합재 태양광 무인기 날개 일체성형 제작기법 연구)

  • Yang, Yongman;Kwon, Jeongsik;Kim, Jinsung;Lee, Sooyong
    • Journal of Aerospace System Engineering
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    • v.10 no.1
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    • pp.43-50
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    • 2016
  • In order to suggest the optimal manufacturing technology of composite wings of solar-powered unmanned aerial vehicles, this study compared forming technologies to reduce wing weight for long-endurance flight and to improve the manufacturing process for cost-saving and mass production. It compared the manufacturing time and weight of various composite wing molding technologies, including cocuring, secondary bonding, and manufacturing by balsa. As a result, wing weight was reduced through cocuring methods such as band type composite fiber/tape lamination technology, which enabled prolonged flight duration. In addition, the reduced manufacturing time led to a lower cost, which is a good example of weight lightening for not only small solar-powered UAVs, but also composite aircraft.

Heave Motion Estimation of a Ship Deck for Shipboard Landing of a VTOL UAV (수직이착륙 무인기 함상 착륙점의 상하 운동 추정)

  • Cho, Am;Yoo, Changsun;Kang, Youngshin;Park, Bumjin
    • Journal of Aerospace System Engineering
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    • v.8 no.3
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    • pp.14-19
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    • 2014
  • When a helicopter lands on a ship deck in high sea states, one of main difficulties is the ship motion by sea wave, In case of a manned helicopter, a pilot lands a helicopter on the deck during quiescent period of ship motion, which is perceived from different visual cues around landing spot. The capability to predict this quiescent period is very important especially for shipboard recovery of VTOL UAV in harsh environments. This paper describes how to predict heave motion of a ship for shipboard landing of a VTOL UAV. For simulation, ship motion by sea wave was generated using a 4,000 ton class US destroyer model. Heave motion of ship deck was predicted by applying auto-regression method to generated time series data of ship motion.

Composite Skid Landing Gear Optimal Design for Light VTOL UAV (경량 수직이착륙 무인기의 복합재료 스키드 착륙장치 최적설계)

  • Lee, Jungjin;Kim, Myungjun;Kim, Yongha;Shin, Jungchan;Hwang, Kyungmin
    • Journal of Aerospace System Engineering
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    • v.9 no.4
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    • pp.55-61
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    • 2015
  • In this study, we peformed optimal design of a composite skid landing gear, one of the solid spring shock absorbers, for light vertical takeoff and landing aircraft. Although a solid spring type has poor energy dissipation capability, it is commonly used for light aircraft where sink speeds are low and shock absorption is non-critical in terms of simplicity, low cost and weight reduction. In this paper, design parameters of solid spring such as sink speed, gear leg length, deflection and landing load factor were reviewed. In order to meet structural requirements such as deflection and strength, finally, we conducted optimal design of the composite skid landing gear for VTOL UAV using genetic algorithm and pattern search algorithm.

Fabrication and Resistance Characteristics of Smart Paint for Temperature Sensor (온도 센서를 위한 스마트 페인트 제작 및 저항 특성)

  • Ahn, Ju-Hun;Lee, Chang-Yull
    • Journal of Aerospace System Engineering
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    • v.13 no.2
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    • pp.43-50
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    • 2019
  • Satellite and aircraft components are greatly affected by the possibility for missions and safety due to temperature effects. In the field of fuel cells, research is actively carried out for UAV. For the efficiency and stability of the fuel cells, the temperature for operations must be confirmed. In this paper, a smart paint was fabricated with $BaTiO_3$ and $SrTiO_3$ ceramics in order to take advantage of the rapid characteristics of the PTC thermistor, which is the resistance changes abruptly above the Curie point. A coating agent was prepared to prevent the paint from peeling off the samples and the coated models were checked for resistance changes. Moreover, the resistance change of the $BaTiO_3$ and $SrTiO_3$ with temperature conditions was measured before and after coating.

2019 Incheon FIR Aerial Collision Risk Analysis (2019년도 인천 FIR 공중 충돌 위험도 분석)

  • Jae-young Ryu;Hyeonwoong Lee;Bae-Seon Park;Hak-Tae Lee
    • Journal of Advanced Navigation Technology
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    • v.25 no.6
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    • pp.476-483
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    • 2021
  • In order to maintain the safety of the airspace with ever increasing traffic volume, it is necessary to thoroughly analyze the collision risk with the current data. In this study, collision risk analysis was conducted using Detect and Avoid (DAA) Well-Clear (DWC) metrics, risk induces developed for the DAA systems of unmanned aerial vehicles. All flights in year 2019 that flew within the Incheon Flight Information Region (FIR) boundary were analyzed using the recorded Automatic Dependent Surveillance-Broadcast(ADS-B) data. High risk regions as well as trends by airports and seasons were identified. The results indicate that the risk is higher around the congested area near Incheon International Airport and Gimpo International Airport. Seasonally, the risk was highest in August that coincides with the Summer vacation period. The result will be useful for the baseline data for various aviation safety enhancement activities such as revision of routes and procedures and training of the field specialists.

Assessment of Parallel Computing Performance of Agisoft Metashape for Orthomosaic Generation (정사모자이크 제작을 위한 Agisoft Metashape의 병렬처리 성능 평가)

  • Han, Soohee;Hong, Chang-Ki
    • Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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    • v.37 no.6
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    • pp.427-434
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    • 2019
  • In the present study, we assessed the parallel computing performance of Agisoft Metashape for orthomosaic generation, which can implement aerial triangulation, generate a three-dimensional point cloud, and make an orthomosaic based on SfM (Structure from Motion) technology. Due to the nature of SfM, most of the time is spent on Align photos, which runs as a relative orientation, and Build dense cloud, which generates a three-dimensional point cloud. Metashape can parallelize the two processes by using multi-cores of CPU (Central Processing Unit) and GPU (Graphics Processing Unit). An orthomosaic was created from large UAV (Unmanned Aerial Vehicle) images by six conditions combined by three parallel methods (CPU only, GPU only, and CPU + GPU) and two operating systems (Windows and Linux). To assess the consistency of the results of the conditions, RMSE (Root Mean Square Error) of aerial triangulation was measured using ground control points which were automatically detected on the images without human intervention. The results of orthomosaic generation from 521 UAV images of 42.2 million pixels showed that the combination of CPU and GPU showed the best performance using the present system, and Linux showed better performance than Windows in all conditions. However, the RMSE values of aerial triangulation revealed a slight difference within an error range among the combinations. Therefore, Metashape seems to leave things to be desired so that the consistency is obtained regardless of parallel methods and operating systems.

Evaluation of Possibility for the Classification of River Habitat Using Imagery Information (영상정보를 활용한 하천 서식처 분류 가능성 평가)

  • Lee, Geun-Sang;Lee, Hyun-Seok
    • Journal of the Korean Association of Geographic Information Studies
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    • v.15 no.3
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    • pp.91-102
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    • 2012
  • As the basis of the environmental ecological river management, this research developed a method of habitat classification using imagery information to understand a distribution characteristics of fish living in a natural river. First, topographic survey and investigation of discharge and water temperature were carried out to analyze hydraulic characteristics of fish habitat, and the unmanned aerial photography was applied to acquire river imagery at the observation time. Riffle, pool, and glide regions were selected as river habitat to analyze fish distribution characteristics. Analysis showed that the standard deviation of RGB on the riffle is higher than pool and glide because of fast stream flow. From the classification accuracy estimation on riffle region according to resolution and kernel size using the characteristics of standard deviation of RGB, the highest classification accuracy was 77.17% for resolution with 30cm and kernel size with 11. As the result of water temperature observation on pool and glide using infrared camera, they were $19.6{\sim}21.3^{\circ}C$ and $15.5{\sim}16.5^{\circ}C$ respectively with the differences of $4{\sim}5^{\circ}C$. Therefore it is possible to classify pool and glide region using the infrared photography information. The habitat classification to figure out fish distribution can be carried out more efficiently, if unmanned aerial photography system with RGB and infrared band is applied.

Replay Attack based Neutralization Method for DJI UAV Detection/Identification Systems (DJI UAV 탐지·식별 시스템 대상 재전송 공격 기반 무력화 방식)

  • Seungoh Seo;Yonggu Lee;Sehoon Lee;Seongyeol Oh;Junyoung Son
    • Journal of Aerospace System Engineering
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    • v.17 no.4
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    • pp.133-143
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    • 2023
  • As drones (also known as UAV) become popular with advanced information and communication technology (ICT), they have been utilized for various fields (agriculture, architecture, and so on). However, malicious attackers with advanced drones may pose a threat to critical national infrastructures. Thus, anti-drone systems have been developed to respond to drone threats. In particular, remote identification data (R-ID)-based UAV detection and identification systems that detect and identify illegal drones with R-ID broadcasted by drones have been developed, and are widely employed worldwide. However, this R-ID-based UAV detection/identification system is vulnerable to security due to wireless broadcast characteristics. In this paper, we analyze the security vulnerabilities of DJI Aeroscope, a representative example of the R-ID-based UAV detection and identification system, and propose a replay-attack-based neutralization method using the analyzed vulnerabilities. To validate the proposed method, it is implemented as a software program, and verified against four types of attacks in real test environments. The results demonstrate that the proposed neutralization method is an effective neutralization method for R-ID-based UAV detection and identification systems.