• 제목/요약/키워드: UAVs(Unmanned Aerial Vehicles)

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5G 기반 무인 비행체 운용 표준화 동향 (Standardization Trends for Operation of Unmanned Aerial Vehicles based on 5G)

  • 이현;배정숙;방승재;이희수
    • 전자통신동향분석
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    • 제36권4호
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    • pp.13-22
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    • 2021
  • Among the activities of 3GPP for operating 5G-based unmanned aerial vehicles, we introduce several use cases of UAVs in 5G mobile communication such as radio access node onboard UAV, simultaneous support data transmission for UAVs and eMBB users, autonomous UAVs controlled by AI, isolated deployment of radio access through UAV, and separation of UAV service area. From this, we further summarize 5G mobile communication requirements for UAVs, including definition and operational criteria of UAS, UAS remote identification requirements, UAS usage requirements, and performance requirements. Finally, regarding 5G mobile communication-based UAS connectivity, identification and tracking support, we discuss the 3GPP UAV architecture, seven major problems, the proposed solutions to each problem, and propose the results for future specification work.

다중 무인 항공기의 협동 작업을 위한 무 충돌 비행 계획 (Collision-free Flight Planning for Cooperation of Multiple Unmanned Aerial Vehicles)

  • 박재병
    • 전자공학회논문지SC
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    • 제49권2호
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    • pp.63-70
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    • 2012
  • 본 논문에서는 3차원 공동 작업 공간에서 다중 무인항공기의 협동 작업을 위한 확장 충돌 지도 기반 무 충돌 비행 계획 기법을 제안한다. 먼저 무인항공기는 회전과 같은 3차원 움직임을 고려해 구로 모델링하였다. 공동 작업 영역에 진입 후 진출할 때까지 무인 항공기는 직선 경로를 따라 이동하고 모든 무인 항공기의 우선순위는 미리 정해져 있다고 가정한다. 가정에 따라 3차원에서 정의된 구와 구 사이의 충돌 검출 문제를 2차원에서 정의된 원과 직선 사이의 충돌 검출 문제로 축소할 수 있다. 원과 직선 사이의 충돌영역은 계산의 편의성과 안전성을 위해 충돌사각형으로 근사화 하였다. 이렇게 정의된 충돌사각형을 이용하여 무인 항공기들 간의 충돌을 회피할 수 있도록 각 무인 항공기의 공동 작업 공간 진입 시간을 조율한다. 이와 같은 방법으로 모든 무인 항공기는 공동 작업 공간에 진입해서 진출할 때까지 서로 간에 충돌 없이 이동 할 수 있게 된다. 제안된 무충돌 비행 계획의 효율성을 증명하기 위해 12대의 무인 항공기를 이용한 시뮬레이션을 수행하였다.

Navigation Performance Analysis Method for Integrated Navigation System of Small Unmanned Aerial Vehicles

  • Oh, Jeonghwan;Won, Daehan;Lee, Dongjin;Kim, Doyoon
    • International journal of advanced smart convergence
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    • 제9권3호
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    • pp.207-214
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    • 2020
  • Currently, the operation of unmanned aerial vehicle (UAV) is regulated to be able to fly only within the visible range, but in recent years, the needs for operation in the invisible area, in the urban area and at night have increased. In order to operate UAVs in the invisible area, at night, and in the urban area, a flight path for UAVs must be prepared like those operated by manned aircraft, and for this, it is necessary to establish an unmanned aircraft system traffic management (UTM). In order to establish the UTM, information on the minimum separation distance to prevent collisions with UAVs and buildings is required, and accordingly, information on the navigation performance of UAVs is required. In order to analyze the navigation performance of an UAV, total system error (TSE), which is the difference between the planned flight path and the actual location of the UAV, is required. If the collected data are insufficient and classification according to integrity, independence, and direction is not performed, accurate navigation performance is not derived. In this paper, propose a navigation performance analysis method of UAV that is derived TSE using flight data and modeled with normal distribution, analyze performance.

Improvement of Communication Reliability of Small UAV by a Tapered Stacked Antenna

  • Kim, Duck-Hwan;Lee, Kyu-Hwan;Kim, Young-Sik
    • ETRI Journal
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    • 제28권6호
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    • pp.796-798
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    • 2006
  • This letter proposes a tapered stacked microstrip antenna for application in small unmanned aerial vehicles (UAVs), which has advantages in mountainous terrains. With its tapered structure and increased bandwidth designed to operate at the resonance frequency of 2.4 GHz, the proposed antenna improves directivity, accuracy, and precision of small UAVs. The test flight results show the proposed tapered antenna has a three times higher impedance capability of 350 MHz based on VSWR<2. The transmission pattern is also more reliable than that of previous antenna designs.

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소형 무인항공기 감항인증 기술기준 및 에너지 충돌기법 분석 연구 (Analysis for Unmanned Aerial Vehicle Airworthiness Certification Criteria)

  • 임준완;김용래;최병철;고준수
    • 한국항공운항학회지
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    • 제22권4호
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    • pp.65-74
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    • 2014
  • Unmanned aerial vehicles(UAVs) refer to the aircraft which carries no human pilot and is operated under remote control or in autonomous operational mode. As the UAVs can perform the dull, dangerous and difficult missions, various kinds of UAVs with different sizes and weights have been developed and operated for both civil and military application. As the avionics and communication technology related to the UAVs are matured, the demand for the UAVs is dramatically increased. Therefore, It is important to develope airworthiness process and regulations of the UAVs to minimize related risk to the man and environment. This paper describes related regulations and classification of the small UAVs for different international airworthiness authorities. The analysis of the CS-LURS verses Stanag 4702 and Stanag 4703 can provide guidelines for the generation of the airworthiness certification criteria for the small UAVs in civil sector. This paper conducted kinetic impact energy analysis of the loss of the small UAVs control scenarios and of the very small UAVs under 66 joules. Based on the analysis, the energy impact analysis can be considered before the design certification approval for the small UAVs.

Waypoint Planning Algorithm Using Cost Functions for Surveillance

  • Lim, Seung-Han;Bang, Hyo-Choong
    • International Journal of Aeronautical and Space Sciences
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    • 제11권2호
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    • pp.136-144
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    • 2010
  • This paper presents an algorithm for planning waypoints for the operation of a surveillance mission using cooperative unmanned aerial vehicles (UAVs) in a given map. This algorithm is rather simple and intuitive; therefore, this algorithm is easily applied to actual scenarios as well as easily handled by operators. It is assumed that UAVs do not possess complete information about targets; therefore, kinematics, intelligence, and so forth of the targets are not considered when the algorithm is in operation. This assumption is reasonable since the algorithm is solely focused on a surveillance mission. Various parameters are introduced to make the algorithm flexible and adjustable. They are related to various cost functions, which is the main idea of this algorithm. These cost functions consist of certainty of map, waypoints of co-worker UAVs, their own current positions, and a level of interest. Each cost function is formed by simple and intuitive equations, and features are handled using the aforementioned parameters.

연료전지-배터리 기반 무인항공기 추진시스템 동특성 분석을 위한 모델 개발 (Model Development for Analysis of the System Dynamic Characteristics for Fuel Cell-battery Based Unmanned Aerial Vehicles)

  • 현대일;홍석무;한재영
    • 한국수소및신에너지학회논문집
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    • 제34권5호
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    • pp.490-496
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    • 2023
  • Unmanned aerial vehicles (UAVs) research is recently actively underway. Especially, fuel cell battery hybrid systems are widely used to overcome the limitations of continuous operation. However, fuel cell systems must be operated in combination with a battery due to their low specific output characteristics. Therefore, a hybrid power system model for UAVs is developed. The rule-based strategy is applied to the model to properly distribute power to batteries and fuel cells. As a result, the designed rule-based power distribution control operates UAVs while maintaining battery state of charge(SOC) at an appropriate level.

Calculating coniferous tree coverage using unmanned aerial vehicle photogrammetry

  • Ivosevic, Bojana;Han, Yong-Gu;Kwon, Ohseok
    • Journal of Ecology and Environment
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    • 제41권3호
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    • pp.85-92
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    • 2017
  • Unmanned aerial vehicles (UAVs) are a new and yet constantly developing part of forest inventory studies and vegetation-monitoring fields. Covering large areas, their extensive usage has saved time and money for researchers and conservationists to survey vegetation for various data analyses. Post-processing imaging software has improved the effectiveness of UAVs further by providing 3D models for accurate visualization of the data. We focus on determining the coniferous tree coverage to show the current advantages and disadvantages of the orthorectified 2D and 3D models obtained from the image photogrammetry software, Pix4Dmapper Pro-Non-Commercial. We also examine the methodology used for mapping the study site, additionally investigating the spread of coniferous trees. The collected images were transformed into 2D black and white binary pixel images to calculate the coverage area of coniferous trees in the study site using MATLAB. The research was able to conclude that the 3D model was effective in perceiving the tree composition in the designated site, while the orthorectified 2D map is appropriate for the clear differentiation of coniferous and deciduous trees. In its conclusion, the paper will also be able to show how UAVs could be improved for future usability.

3차원 격자지도 기반 생존성 극대화를 위한 다수 무인 항공기 임무경로 계획 (Mission Path Planning to Maximize Survivability for Multiple Unmanned Aerial Vehicles based on 3-dimensional Grid Map)

  • 김기태;전건욱
    • 산업공학
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    • 제25권3호
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    • pp.365-375
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    • 2012
  • An Unmanned Aerial Vehicle (UAV) is a powered pilotless aircraft, which is controlled remotely or autonomously. UAVs are an attractive alternative for many scientific and military organizations. UAVs can perform operations that are considered to be risky or uninhabitable for humans. UAVs are currently employed in many military missions and a number of civilian applications. For accomplishing the UAV's missions, guarantee of survivability should be preceded. The main objective of this study is to suggest a mathematical programming model and a $A^*PS$_PGA (A-star with Post Smoothing_Parallel Genetic Algorithm) for Multiple UAVs's path planning to maximize survivability. A mathematical programming model is composed by using MRPP (Most Reliable Path Problem) and MTSP (Multiple Traveling Salesman Problem). After transforming MRPP into Shortest Path Problem (SPP),$A^*PS$_PGA applies a path planning for multiple UAVs.

연료전지 무인항공기의 고도와 체공시간에 대한 특성 분석 및 최신 연구동향 (Research Trend and Analysis of Altitude and Endurance for Fuel Cell Unmanned Aerial Vehicles)

  • 조성현;김민진;손영준;양태현
    • 한국수소및신에너지학회논문집
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    • 제25권4호
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    • pp.393-404
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    • 2014
  • Unmanned aerial vehicles (UAVs) have been applied to not only military missions like surveillance and reconnaissance but also commercial missions like meteorological observation, aerial photograph, communication relay, internet network build and disaster observation. Fuel cells make UAVs eco-friendly by using hydrogen. Proton exchange membrane fuel cells (PEMFCs) show low operation temperature, high efficiency, low noise and high energy density and those characterisitcs are well fitted with UAVs. Thus Fuel cell based UAVs have been actively developed in the world. Recently, fuel cell UAVs have started to develope for high altitude UAVs because target altitude of UAVs is expanded upto stratosphere altitude. Long endurance of UAVs is essential to improve effects of the missions. Improvement of UAV endurance time could be fulfilled by developing a hydrogen fuel storage system with high energy density and reducing the weight of UAVs. In this paper, research trend and analysis of fuel cell UAVs are introduced in terms of their altitude and endurance time and then the prospect of fuel cell UAVs are shown.