• Title/Summary/Keyword: 무인비행기

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무인항공기의 제어기술개발 동향

  • Gang, Yeong-Sin;Park, Beom-Jin;Yu, Chang-Seon
    • Current Industrial and Technological Trends in Aerospace
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    • v.4 no.2
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    • pp.55-67
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    • 2006
  • 20세기에 탄생한 동력비행기는 인간의 이동능력을 비약적으로 향상시켰다. 인류의 미개척지였던 항공분야의 발전은 지속적인 기술개발을 통해 더 빨리, 더 멀리, 더 높이 향하기 위해서 계속 나아가고 있다. 이러한와중에 최근에 괄목할 만한 성장을 이룬 컴퓨터와 소프트웨어 산업의 발전은 비행임무에 따라 위험성이 높거나, 사람이 하기 힘든 반복적이고 지루한 비행을 대신하기위한 로봇 비행체 즉, 무인항공기의 개발을 가능하게 하였다. 무인항공기의 탄생 초기에는 조종사의 희생을 줄이기 위해 군사 분야에서 주로 사용되었으나, 산림감시나 해안정찰, 기상관측, 재난관측, 조난자 수색 등 민수분야의 임무로 점차 활동영역이 넓혀지고 있다. 현재 무인항공기에 탑재된 인공지능의 수준은 안정된 비행이 가능하도록 하는 자동조종(autopilot)과 주어진 비행경로를 추종하기위한 항법유도(Navigation & Guidance)정도이며, 비행 중 발생하는 비상상황에 대처하기 위한 의사판단은 지상의 조종자에 의해 결정된다. 앞으로는 계획되지 않은 상황을 맞이했을 때 무인기 스스로 판단하여 경로를 변경하고, 동시에 여러 무인기들과 협력하여 임무를 수행함으로써 임무효율을 높이는 방향으로 인공지능의 수준이 향상될 것이다. 본 논문에서는 최근의 무인항공기 개발추세와 이들 무인기에 고려되고 있는 제어기에 대해 살펴보고, 향후 무인항공기에 적용될 자율비행 알고리듬과 제어기 시스템의 개발동향에 대해 고찰하였다.

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Real-Time Estimation of Control Derivatives for Control Surface Fault Detection of UAV (실시간 조종미계수 추정에 의한 무인비행기 조종면 고장검출)

  • Lee, Hwan;Kim, Eung-Tae;Choi, Hyoung-Sik;Choi, Ji-Young;Lee, Sang-Kee
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.11
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    • pp.999-1005
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    • 2007
  • In case of an abnormal condition of control surface, the real-time estimation of aerodynamic derivatives are required for the reconfigurable control system to be flight for missions or return to the head office. The goal of this paper is to represent a technique of fault detection to the control surface as a base research to the fault tolerant control system for safety improvement of UAV. The real-time system identification for the fault detection to the control surface was applied with the recursive Fourier Transform and verified through the HILS and flight test. The failures of the control surface are detected by comparing the control derivatives in fault condition with the normal condition. As a result from the flight test, we have confirmed that the control derivatives of fault condition less than about 50% in the normal condition.

CFD Analysis of CRW Unmanned Aerial Vehicle and Drag Reduction Strategy (CRW 무인 항공기의 공력 해석 및 항력 감소 방안)

  • Kim, Cheol-Wan;Chung, Jin-Deog
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.10
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    • pp.20-27
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    • 2004
  • In this study, CFD analysis for 2D ellipse and 3D CRW UAV are performed. Furthermore, flow analysis around a hub connecting body and rotor is analyzed and a strategy to reduce the drag caused by the hub is sought. Also, the idea of fairing installation is confirmed by a wind tunnel test.

Development of Small UAV Wi-Fi Communication Environment (소형 무인 비행체 Wi-Fi 통신 환경 개발)

  • Choi, Hyo Hyun;Jo, Su Han;Kang, Min Seong
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2012.07a
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    • pp.63-64
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    • 2012
  • 본 논문에서는 소형 무인 비행체 (Unmanned Aerial Vehicle, UAV)를 스마트폰을 이용하여 제어하기 위한 방법을 제안하고. UAV에 Wi-Fi 통신 모듈 설계 및 개발 과정을 설명한다. 스마트폰과 UAV는 Wi-Fi를 통해 통신하며, 이것의 instruction set은 MCU에서 C언어로 다운로드 된 로직으로 수행하게 된다. 데이터의 송수신은 Serial 포트를 이용하여 흐름을 제어하며 확인할 수 있다. 또한 관련 모듈들을 통합하기 위해 PCB(Printed Circuit Board)과정을 진행, 소형화하여 개발하였다.

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Design and Demonstration of Morphing Wing Sections Using Lightweight Piezoceramic Composite Actuator (LIPCA) (압전 작동기 LIPCA를 이용한 형상가변익 설계 및 작동구현)

  • Im,Sang-Min;Lee,Sang-Gi;Park,Hun-Cheol;Yun,Gwang-Jun;Gu,Nam-Seo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.10
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    • pp.34-39
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    • 2003
  • Morphing wing sections actuated by piezoceramic actuator LIPCA have been designed and their actuation displacements estimated by using the therml analogy and MSC/NASTRAN based on the linear elasticity. The wing sections are fabricated as the design and tested for evaluation. Measured actuation displacements were larger than the estimated values mainly due to the material non-linearity of the PIT wafer. The morphing wing sections can be used for control surfaces of small scale UAVs or MAVs.

Design and Implementation of Simulator Passenger Boarding Bridge Controller in integrated platform management system (통합플랫폼관리 체재에서 PBBC 시뮬레이터 설계와 구현)

  • Kim, Whi-Young
    • Proceedings of the Korea Information Processing Society Conference
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    • 2002.04b
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    • pp.1203-1206
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    • 2002
  • In maned airport, crews may have risks as they manage passenger control system in IPMS in damage situations such as fire in a airport. So the application of unmanned autonomous system can reduce the number of boarding crews and attribute to safe airplane tranportation. PBBC model can be used to obtain control strategy, and airplane and enhance oprators' skill by simulating the airport. The paper suggests an intelligent system of the pbbc control using microprocessor in integrated platform management system which can take measures against passenger situation of a airplane excluding unnecessary warnings with undamaged situations. The system here detected the passenger more accurately and adopted more appriate measures according to airplane status compared with conventional systems.

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A Clustering for Ground Nodes of HAPS Network (HAP 네트워크 지상 노드의 클러스터링)

  • Song, Ha-Yoon
    • Journal of Digital Contents Society
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    • v.9 no.1
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    • pp.87-99
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    • 2008
  • High Altitude Platform network systems utilize Unmanned Aerial Vehicle as routers for ground node communication. For this purpose, geographical clustering of ground nodes must be required. In this paper, we assume mobile ground nodes over wide area and the clusters composed of ground nodes are identified. UAVs can be positioned at the point of centroid of clusters. The number of UAVs are derived from the area size and the number of ground nodes deployed in that area. From the simulation and application of clustering algorithms, we showed visual clustering results with dynamic variance of number of ground nodes.

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A Study on ADS-33E with Application to the Assessment of Handling Quality for Unmanned Rotorcraft (회전익 무인항공기의 비행안정성 규명을 위한ADS-33E 적용기법 연구)

  • Jeong, Hwan-Ho;Suk, Jin-Young;Kim, Byoung-Su;Lee, Sang-Kee
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.3
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    • pp.243-250
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    • 2012
  • In this paper, a systematic consequence of evaluation method, procedure, and flight data analysis is investigated for application of ADS-33E-PRF to UAV. And it is applied to unmanned rotorcraft for evaluation. CNUHELI-020, which is developed in Chungnam National University, is used for assessment of handling quality: decoupled longitudinal and lateral/directional model were used to assess handling qualities. Evaluation flight maneuvers are categorized as hover/low-speed requirements, small-amplitude attitude change, and moderate-amplitude attitude change requirements.

ISAR Imaging of Airplane-like Targets by Matrix Pencil Method (Matrix Pencil 방법에 의한 비행기 모형의 ISAR 영상화)

  • 유지희;권경일;이용희
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.12 no.2
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    • pp.299-307
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    • 2001
  • This paper presents a experimental study of Inverse Synthetic Aperture Radar(ISAR) imaging using Matrix Pencil(MP) method. A series of measurement for two types of target model was done in a Compact Range(CR)facility. The first target is a set of distributed slim cylinders to get a ISAR image of point-like scatterers. The second is UAV model representing a complex real target. The results show that ISAR images by MP method are better than by conventional FFT method under the realistic measurement conditions.

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