• Title/Summary/Keyword: 복수 무인항공기

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Theoretical Maximum Throughput (TMT) Analysis of the Multiple UAVs datalink system using WLAN (IEEE 802.11b) (무선랜 기반의 복수 무인기 통신링크 최대 처리량 분석)

  • Kim, In-Kyu;Moon, Sang-Man
    • Aerospace Engineering and Technology
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    • v.12 no.2
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    • pp.118-122
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    • 2013
  • In this study, We show that multiple UAVs (Unmaned Air Vehicle) have datalink system which includes the IEEE 802.11b technology. we are predicting and calculating to the number of the UAV and data rate between UAV and ground control system, using the IEEE 802.11 standards which include the transmit/receive the delay time and theoretical maximum throughput (TMT).

Optimal path planning and analysis for the maximization of multi UAVs survivability for missions involving multiple threats and locations (다수의 위협과 복수의 목적지가 존재하는 임무에서 복수 무인기의 생존율 극대화를 위한 최적 경로 계획 및 분석)

  • Jeong, Seongsik;Jang, Dae-Sung;Park, Hyunjin;Seong, Taehyun;Ahn, Jaemyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.6
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    • pp.488-496
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    • 2015
  • This paper proposes a framework to determine the routes of multiple unmanned aerial vehicles (UAVs) to conduct multiple tasks in different locations considering the survivability of the vehicles. The routing problem can be formulated as the vehicle routing problem (VRP) with different cost matrices representing the trade-off between the safety of the UAVs and the mission completion time. The threat level for a UAV at a certain location was modeled considering the detection probability and the shoot-down probability. The minimal-cost path connecting two locations considering the threat level and the flight distance was obtained using the Dijkstra algorithm in hexagonal cells. A case study for determining the optimal routes for a persistent multi-UAVs surveillance and reconnaissance missions given multiple enemy bases was conducted and its results were discussed.

Development of Ground Control Software for Operation of Multiple Unmanned Aerial Vehicles (복수 무인항공기의 운용을 위한 지상통제 소프트웨어 개발)

  • Shin, Yoon-Ho;Cho, Sang-Wook;Jo, Sung-Beom;Kim, Sung-Hwan;Lyu, Chang-Kyung;Choi, Kee-Young
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.6
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    • pp.542-547
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    • 2012
  • Until recently, most of GCS(Ground Control Software) has been required to visualize attitude, position, status of vehicle and to transmit control and mission commands for a single UAV(Unmanned Aerial Vehicle). However, the GCS needs to expand its functions to handle more complex situations. Simultaneous operation of multiple UAVs is emerging as a new practice. Hence, we set up requirements for operation of multiple UAVs and suggest the architecture of GCS that satisfy the requirements. In this study, we analyze the upper requirements and define the total structure of GCS at first. Then we design the inner structure for requirements in detail. Finally, we verify the functions of GCS on PILS(Processor In the Loop Simulation) System.

Development of Adaptive Ground Control System for Multi-UAV Operation and Operator Overload Analysis (복수 무인기 운용을 위한 적응형 지상체 개발 및 운용자 과부하 분석)

  • Oh, Jangjin;Choi, Seong-Hwan;Lim, Hyung-Jin;Kim, Seungkeun;Yang, Ji Hyun;Kim, Byoung Soo
    • Journal of Advanced Navigation Technology
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    • v.21 no.6
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    • pp.529-536
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    • 2017
  • The general ground control system has control and information display functions for the operation of a single unmanned aerial vehicle. Recently, the function of the single ground control system extends to the operation of multiple UAVs. As a result, operators have been exposed to more diverse tasks and are subject to task overload due to various factors during their mission. This study proposes an adaptive ground control system that reflects the operator's condition through the task overload measurement of multiple UAV operators. For this, the ground control software is developed to control multiple UAVs at the same time, and the simulator with six degree-of-freedom aircraft dynamics is constructed for realistic human-machine-interface experiments by the operators.

Design of Photographing System for Multiple Users based on UAV (UAV 기반 복수의 사용자를 촬영하기 위한 촬영 시스템 설계 연구)

  • Kwak, Jeonghoon;Sung, Yunsick
    • Proceedings of the Korea Information Processing Society Conference
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    • 2018.05a
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    • pp.479-480
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    • 2018
  • 최근 무인항공기(Unmanned Aerial Vehicle, UAV)에 부착된 카메라로 사용자를 촬영함으로써 레저 및 여행 중 영상을 기록하기 위해 활용하고 있다. UAV에 부착된 카메라로 사용자를 촬영하기 위해 사용자가 직접 조종하거나 NUI/NUX 기술을 활용한다. UAV가 비행해야 되는 비행경로를 미리 설정하거나 단일 사용자를 추적해서 자동적으로 UAV가 비행하며 UAV에 부착된 카메라로 단일 사용자 중심으로 촬영한다. 하지만 레저 및 여행 중 영상을 기록하는 과정에서 단일 사용자 중심이 아니라 복수의 사용자를 고려하여 촬영해야 되는 경우가 있다. UAV가 복수의 사용자 위치를 고려하여 복수의 사용자를 촬영하는 시스템이 필요하다. 본 논문에서는 복수의 사용자를 촬영하기 위한 촬영 시스템을 설계한다. 촬영 시스템은 복수의 사용자 위치의 변화를 기반으로 UAV를 제어한다.

Determining UAV Flight Direction Control Method for Shooting the images of Multiple Users based on NUI/NUX (NUI/NUX 기반 복수의 사용자를 촬영하기 위한 UAV 비행방향 제어방법)

  • Kwak, Jeonghoon;Sung, Yunsick
    • Proceedings of the Korea Information Processing Society Conference
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    • 2018.05a
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    • pp.445-446
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    • 2018
  • 최근 무인항공기 (Unmanned Aerial Vehicle, UAV)에 장착한 카메라를 활용하여 사용자의 눈높이가 아닌 새로운 시각에서 사용자를 촬영한 영상을 제공한다. 사용자를 추적하며 촬영하기 위해 저전력 블루투스 (Bluetooth Low Energy, BLE) 신호, 영상, 그리고 Natural User Interface/Natual User Experience(NUI/NUX) 기술을 활용한다. BLE 신호로 사용자를 추적하는 경우 사용자의 후방에서 추적하며 사용자만을 추적하며 촬영 가능한 문제가 있다. 하지만 복수의 사용자를 전방에서 추적하며 촬영하는 방법이 필요하다. 본 논문에서는 복수의 사용자를 추적하며 전방에서 촬영하기 위해 UAV의 비행방향을 결정하는 방법을 설명한다. 복수의 사용자로부터 측정 가능한 BLE 신호들을 UAV에서 측정한다. 복수개의 BLE 신호의 변화를 활용하여 UAV의 비행방향을 결정한다.

Development of Operation System for Network of Multiple UAVs (복수 무인기 네트워크 통합 운영 시스템 개발)

  • Kim, Sung-Hwan;Cho, Sang-Ook;Kim, Sung-Su;Ryoo, Chang-Kyung;Choi, Kee-Young
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.11
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    • pp.1042-1051
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    • 2011
  • In this paper, a total operating environment equipped with onboard wireless communication systems and ground-based mission control systems is proposed for simultaneous operation of multiple UAVs. A variety of operating structures are studied and classified systematically based on types and usages of the components. For each operating system, the strength, weakness and reliability aspects are investigated. Based on these results, a proper operating system configuration is determined and components are developed for mission formation flight. Proposed system can make a formation flight of various UAVs, execute complex missions decentralizing mission to several UAVs and cooperate several missions.

Design and Implementation of Mobile Network Based Long-Range UAV Operational System for Multiple Clients (모바일 네트워크를 이용한 복수의 클라이언트용 무인항공기 원거리 운용 시스템 설계 및 구현)

  • Park, Seong-hyeon;Song, Joon-beom;Roh, Min-shik;Song, Woo-jin;Kang, Beom-soo
    • Journal of Advanced Navigation Technology
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    • v.19 no.3
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    • pp.217-223
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    • 2015
  • This paper describes the design and implementation of a network system for UAV for multiple clients that enables long-range operation based on a commercial mobile network. A prototype data modem is developed with a commercial embedded M2M module in order to provide an access to the mobile network. A central server with a database is constructed to record all of real-time flight and video data and communicate with a ground control system. A GCS is developed for the central control, the single UAV and the smart phone version to be used for different purposes. Performance tests were progressed for data delay, video frame rate and state of clients. Flight tests were also performed to verify the reliability of the modem with respect to altitude.

Aerodynamic Characteristics of the Blended-Wing-Body for the Position and Aspect Ratio of the Inlet and Outlet of an Embedded Distributed Propulsion System (Embedded Type 분산 추진 장치의 입·출구 형상 및 위치 변화에 따른 융합익기의 공력해석)

  • Kim, Hyo-Seop;Choi, Hyun-Min;Cho, Jin-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.6
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    • pp.467-474
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    • 2012
  • UAVs for reconnaissance and intelligence operations require long endurance capability, which demands high efficiency of the propulsion system. The distributed propulsion system(DPS) generates the thrust by replacing a large propulsion system with a number of small propulsion systems. A DPS distributed along the wing span can produce gains in propulsion efficiency by reducing ejection velocity. Also, the ingestion of boundary layers through the distributed DPS inlet and ejecting flow from the outlet can improve the lift to drag ratio of the vehicle. This study investigates the effects of locations and size of the inlet and outlet of the DPS on the blended-wing-body design based on Eppler 337 airfoil, with a CFD tool. The fans in the DPS are modeled as actuator disks for computational efficiency. The best location and aspect ratio of the inlet and outlet are found from lift-to-drag ratio and pitching moment considerations.