• 제목/요약/키워드: Smart-UAV

검색결과 221건 처리시간 0.024초

무인항공기와 GIS를 이용한 논 가뭄 발생지역 분석 (Analysis of Rice Field Drought Area Using Unmanned Aerial Vehicle (UAV) and Geographic Information System (GIS) Methods)

  • 박진기;박종화
    • 한국농공학회논문집
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    • 제59권3호
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    • pp.21-28
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    • 2017
  • The main goal of this paper is to assess application of UAV (Unmanned Aerial Vehicle) remote sensing and GIS based images in detection and measuring of rice field drought area in South Korea. Drought is recurring feature of the climatic events, which often hit South Korea, bringing significant water shortages, local economic losses and adverse social consequences. This paper describes the assesment of the near-realtime drought damage monitoring and reporting system for the agricultural drought region. The system is being developed using drought-related vegetation characteristics, which are derived from UAV remote sensing data. The study area is $3.07km^2$ of Wonbuk-myeon, Taean-gun, Chungnam in South Korea. UAV images were acquired three times from July 4 to October 29, 2015. Three images of the same test site have been analysed by object-based image classification technique. Drought damaged paddy rices reached $754,362m^2$, which is 47.1 %. The NongHyeop Agricultural Damage Insurance accepted agricultural land of 4.6 % ($34,932m^2$). For paddy rices by UAV investigation, the drought monitoring and crop productivity was effective in improving drought assessment method.

고온 내열재료를 사용한 스마트 무인기 덕트의 열 구조 해석 (Thermal Structural Analysis of a Duct with Heat Resistant Metal Materials for Smart UAV)

  • 임종빈;윤동영;이근명;박정선
    • 한국항공운항학회지
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    • 제12권2호
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    • pp.17-28
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    • 2004
  • In unmanned aerial vehicle (UAV), the high temperature results from friction with the air, combustion of fuel and combustion gas of a nozzle etc. It causes serious problems in the UAV structure. The characteristic analysis of heat resistant metal and ceramic materials and creep analysis for the functionally graded material (FGM) is presented in this paper. FGM is composed of two constituent materials that are mixed up according to the specific volume fraction distribution in order to withstand high heat condition. In addition, the creep behavior of FGM applied in duct structure of an engine is analyzed.

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지능형 성숙도 모델을 이용한 소프트웨어 집약 시스템의 전투실험 프로세스 설계 및 적용 (Design and Application of the Warfighting Experiment Process Using the Intelligent Maturity Model in Software Intensive Systems)

  • 강동수;윤희병
    • 한국지능시스템학회논문지
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    • 제17권5호
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    • pp.668-673
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    • 2007
  • 본 논문에서는 지능형 성숙도 모델을 이용한 소프트웨어 집약 시스템의 전투실험 프로세스 설계를 제안하고 스마트 무인항공기의 표적탐색 능력에 적용한 결과를 제시한다. 이를 위해 먼저 소프트웨어 집약 시스템의 지능형 정도를 평가할 수 있는 지능형 성숙도 모델을 영역 수준 및 지능 수준을 고려하여 설계한다. 그런 다음 전투실험 프로세스 설계를 위해 ISO/IEC-12207과 CMMI 프로세스를 LITO 분야별로 분류하고 이를 전투실험 5요소와 매핑하여 전투실험 요소별 그리고 전투실험 단계별로 프로세스를 도출한다. 도출된 프로세스를 기반으로 IDEF0 표기법을 이용하여 전투실험 프로세스를 설계한다. 마지막으로 제안한 전투실험 프로세스는 스마트 무인항공기(UAV)를 개발하거나 획득 시에 요구되는 표적탐색 능력에 적용하며 그 결과도 제시한다.

지능형 액추에이터와 제어면 재분배를 이용한 무인항공기 고장대처 제어시스템 (Fault-Tolerant Control System for Unmanned Aerial Vehicle Using Smart Actuators and Control Allocation)

  • 양인석;김지연;이동익
    • 제어로봇시스템학회논문지
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    • 제17권10호
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    • pp.967-982
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    • 2011
  • This paper presents a FTNCS (Fault-Tolerant Networked Control System) that can tolerate control surface failure and packet delay/loss in an UAV (Unmanned Aerial Vehicle). The proposed method utilizes the benefits of self-diagnosis by smart actuators along with the control allocation technique. A smart actuator is an intelligent actuation system combined with microprocessors to perform self-diagnosis and bi-directional communications. In the event of failure, the smart actuator provides the system supervisor with a set of actuator condition data. The system supervisor then compensate for the effect of faulty actuators by re-allocating redundant control surfaces based on the provided actuator condition data. In addition to the compensation of faulty actuators, the proposed FTNCS also includes an efficient algorithm to deal with network induced delay/packet loss. The proposed algorithm is based on a Lagrange polynomial interpolation method without any mathematical model of the system. Computer simulations with an UAV show that the proposed FTNCS can achieve a fast and accurate tracking performance even in the presence of actuator faults and network induced delays.

합성곱 신경망을 이용한 정사사진 기반 균열 탐지 기법 (Crack Detection Technology Based on Ortho-image Using Convolutional Neural Network)

  • 장아름;정상기;박진한;강창훈;주영규
    • 한국공간구조학회논문집
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    • 제22권2호
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    • pp.19-27
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    • 2022
  • Visual inspection methods have limitations, such as reflecting the subjective opinions of workers. Moreover, additional equipment is required when inspecting the high-rise buildings because the height is limited during the inspection. Various methods have been studied to detect concrete cracks due to the disadvantage of existing visual inspection. In this study, a crack detection technology was proposed, and the technology was objectively and accurately through AI. In this study, an efficient method was proposed that automatically detects concrete cracks by using a Convolutional Neural Network(CNN) with the Orthomosaic image, modeled with the help of UAV. The concrete cracks were predicted by three different CNN models: AlexNet, ResNet50, and ResNeXt. The models were verified by accuracy, recall, and F1 Score. The ResNeXt model had the high performance among the three models. Also, this study confirmed the reliability of the model designed by applying it to the experiment.

Fault Detection System Design and HILS Evaluation for the Smart UAV FCS

  • Nam, Yoon-Su;Jang, Hu-Yeong;Hong, Sung-Kyung;Park, Sung-Su
    • International Journal of Control, Automation, and Systems
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    • 제5권1호
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    • pp.104-109
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    • 2007
  • This paper is about a redundancy management system design for the Smart UAV(unmanned aerial vehicle) which utilizes the tilt..rotor mechanism. In order to meet the safety requirement on the PLOC(probability of loss of control) of $1.7{\times}10^{-5}$ per flight hour for FCS (flight control system) failures, a digital FCS is mechanized with a dual redundant structure. A fault detection system which is composed of a CCM(cross channel monitor) and analytic redundancy using the Kalman filtering is designed, and its effectiveness is evaluated through experiments. A threshold level and persistence count for managing redundant sensors are designed based on the statistical analysis of the FCS sensors. To increase the survivability of the UAV after the loss of critical sensors in the SAS(stability augmentation system) and to provide reference information for a tie-breaking condition at which an ILM(in-line monitor) cannot distinguish the faulty channel between two operating ones, the Kalman filter approach is investigated.