• Title/Summary/Keyword: small unmanned aerial vehicle

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A Feasibility Study of Highway Traffic Monitoring using Small Unmanned Aerial Vehicle

  • Ro, Kap-Seong;Oh, Jun-Seok
    • International Journal of Aeronautical and Space Sciences
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    • v.8 no.2
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    • pp.54-66
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    • 2007
  • Traffic and emergency monitoring systems are essential constituents of Intelligent Transportation System (ITS) technologies, but the lack of traffic monitoring has become a primary weakness in providing prompt emergency services. Demonstrated in numerous military applications, unmanned aerial vehicles (UAVs) have great potentials as a part of ITS infrastructure for providing quick and real-time aerial video images of large surface area to the ground. Despite of obvious advantages of UAVs for traffic monitoring and many other civil applications, it is rare to encounter success stories of UAVs in civil application including transportation. The objective of this paper is to report the outcomes of research supported by the state agency in US to investigate the feasibility of integrating UAVs into urban highway traffic monitoring as a part of ITS infrastructure. These include current technical and regulatory issues, and possible suggestions for a future UAV system in civil applications.

Traffic Control Proposal of Small Unmanned Aerial Vehicle using Altitude Class Concept (고도별 클래스를 통한 소형 무인비행체 교통 제어 방안)

  • Choi, Hyo Hyun
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2016.07a
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    • pp.131-132
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    • 2016
  • 우리는 많은 소형 무인비행체들이 운행될 곧 다가올 미래에 대비하여 무인비행체들 간의 충돌 예방을 할 수 있는 방안에 대하여 연구를 진행하고 있다. 본 논문에서는 높은 밀집도를 가지는 소형 무인 비행체들 간의 충돌을 회피하기 위하여 무인비행체의 성능에 따라 클래스를 부여하고 비행 고도를 지정해주고 지정된 고도 내에서는 수평 비행을 하고 클래스간 이동을 위해서는 몇개의 정해진 지점에서만 수직 비행이 가능하도록 하는 제어 방안을 논하였다.

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A Study of Path-Finding Method of Small Unmanned Aerial Vehicles for Collision Avoidance (소형 무인비행체에서의 충돌회피를 위한 비행경로 생성에 관한 연구)

  • Shin, Saebyuk;Kim, Jinbae;Kim, Shin-Dug;Kim, Cheong Ghil
    • Journal of Satellite, Information and Communications
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    • v.12 no.1
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    • pp.76-80
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    • 2017
  • With the fast growing popularity of small UAVs (Unmanned Aerial Vehicles), recent UAV systems have been designed and utilized for the various field with their own specific purposes. UAVs are opening up many new opportunities in the fields of electronics, sensors, camera, and software for pilots. Increase in awareness and mission capabilities of UAVs are driving innovations and new applications driven with the help of low cost and its capability in undertaking high threat task. In particular, small unmanned aerial vehicles should fly in environments with high probability of unexpected sudden change or obstacle appearance in low altitude situations. In this paper, current researches regarding techniques of autonomous flight of smal UAV systems are introduced and we propose a draft idea for planning paths for small unmanned aerial vehicles in adversarial environments to arrive at the given target safely with low cost sensors.

Performance Analysis of an Electric Powered Small Unmanned Aerial Vehicle (전기동력 소형무인항공기의 성능분석)

  • Lee, Chang-Ho;Kim, Sung-Yug;Kim, Dong-Min
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.4
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    • pp.65-70
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    • 2010
  • A small unmanned aerial vehicle(UAV), which uses a propulsion system consisting of electric motor and battery, weighs less than 8 kg, capable of hand launch. Because it is easy to operate and able to transmit image information in real time, the use of small UAV has been increasing. However, very few analysis methods or analysis results on flight performance of the small UAV have been known so far. In this paper, the performance analysis methods of a small UAV, which is manufactured to study an electric powered UAV, are suggested and their results are achieved. Aerodynamic data of the vehicle are obtained by making use of gliding performance from actual flight test, and required thrust and required power by flight speed are predicted. In addition, the methods to predict range and endurance in case of using battery as power source are suggested and their results are achieved.

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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    • v.9 no.3
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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.

Discrete Noise Prediction of Small-Scale Propeller for a Tactical Unmanned Aerial Vehicle (소형 전술급 무인항공기 프로펠러의 이산소음 수치해석)

  • Ryu, Ki-Wahn
    • Journal of the Korea Institute of Military Science and Technology
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    • v.21 no.6
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    • pp.790-798
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    • 2018
  • Discrete noise signals from a small scale tactical unmanned aerial vehicle(UAV) propeller were predicted numerically using time domain approach. Two-bladed 29 inch propeller in diameter and 150 kgf in gross weight were used for main parameters of the UAV based on the actual size of the similar scale vehicle. Panel method and Farassat formula A1 were adopted for aerodynamic and aeroacoustic analysis respectively. Time domain signals of both thickness and loading noises were transformed into frequency domain to analyze the discrete noise characteristics. Directivity pattern in a plane perpendicular to the rotating disc plane and attenuation of noise intensity according to double distance were also presented.

Automated 3D Model Reconstruction of Disaster Site Using Aerial Imagery Acquired By Drones

  • Kim, Changyoon;Moon, Hyounseok;Lee, Woosik
    • International conference on construction engineering and project management
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    • 2015.10a
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    • pp.671-672
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    • 2015
  • Due to harsh conditions of disaster areas, understanding of current feature of collapsed buildings, terrain, and other infrastructures is critical issue for disaster managers. However, because of difficulties in acquiring the geographical information of the disaster site such as large disaster site and limited capability of rescue workers, comprehensive site investigation of current location of survivors buried under the remains of the building is not an easy task for disaster managers. To overcome these circumstances of disaster site, this study makes use of an unmanned aerial vehicle, commonly known as a drone to effectively acquire current image data from the large disaster areas. The framework of 3D model reconstruction of disaster site using aerial imagery acquired by drones was also presented. The proposed methodology is expected to assist rescue workers and disaster managers in achieving a rapid and accurate identification of survivors under the collapsed building.

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Implementation of Multilateral Control System for Small UAV Control-Focused on Design (소형 무인기 통제를 위한 다자간 방식 관제시스템 구축방안-설계 중심으로)

  • Choi, Hyun-Taek;Kim, Seok-Kwan;Ryu, Gab-Sang
    • Smart Media Journal
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    • v.6 no.4
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    • pp.65-71
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    • 2017
  • In this paper, we propose a design method for the construction of LTE-based small unmanned aerial vehicle control system to quickly and reliably collect multiple small unmanned aerial vehicle position information simultaneously flying all over the country. In particular, the main requirements are the network (N/W), hardware (H/ W), software(SW), Database(DB), development architecture, and business needs. To satisfy these requirements, N/W, H/W, SW, DB design, and architectural design plan were suggested regarding the design requirements of a small UAV system. To effectively control the small unmanned multi-party system in the system design, the architecture is divided into the front-end service area and the back-end service area according to the function and role of the unit system. In the front-end service area that grasps and controls the position and state of small unmanned aerial vehicles (UAVs), we have studied the design part that can be expanded to N through TCP/IP network by applying Client PC method.

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.

Development of Integrated Ground Support System for Integrated Flight Test of Small UAVs (무인항공기의 통합비행시험을 위한 통합형 지상지원시스템 개발)

  • Jeong, Jae-Hyeon;Lim, Byoung-Do;Kim, Sung-Su;Ryoo, Chang-Kyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.9
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    • pp.800-806
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    • 2012
  • This paper proposes design and development of the Integrated Ground Support System (IGSS) for the flight test of the Unmanned Aerial Vehicle (UAV), which combines ground support and ground control. The integrated flight test of the UAV is a necessary procedure to validate the functionality of the Unmanned Aerial System (UAS). In order to execute cost-effective and systematic flight tests, the IGSS is regarded as an inevitable infrastructure of UAS for small laboratories. The proposed IGSS has functions of ground control, radio communication, power generation, transportation and the maintenance of the UAV.