• 제목/요약/키워드: Smart Unmanned Aerial Vehicle

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Design and Development of Multi-rotorcraft-based Unmanned Prototypes of Personal Aerial Vehicle

  • Muljowidodo, Muljowidodo;Budiyono, Agus
    • International Journal of Aeronautical and Space Sciences
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    • 제10권2호
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    • pp.140-147
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    • 2009
  • The paper presents the design, development and testing activities of the multi-rotorcraft-based unmanned aerial vehicle at the Center for Unmanned System Studies, Institut Teknologi Bandung (ITB), Indonesia. The multi-rotor system was selected as the design stepping stone for future development of personal aerial vehicle prototypes. A step-by-step design program is conducted to study the technology building blocks and critical issues associated with the design, development and operation of personal aerial vehicles. A number of multi-rotor configurations have been investigated providing basic guidelines for developing a stable unmanned aerial platform. The benefit of the presently selected configuration is highlighted and some preliminary testing results are presented.

무인항공기 기반 빅데이터 처리 시스템의 프로토타입 설계 (Prototype Design for unmanned aerial vehicle-based BigData Processing)

  • 김사웅
    • 스마트미디어저널
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    • 제5권2호
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    • pp.51-58
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    • 2016
  • 최근 국내는 물론 전 세계적으로 새로운 관심을 끌고 있는 기술은 무인 항공기이며, 과학, 군사, 마케팅, 스포츠, 엔터테인먼트 등 다양한 분야를 가리지 않고 발휘하는 다재다능함이 드론 열풍의 원동력이다. 또한 활용 범위가 광범위한 만큼 향후 산업화된다면 그 잠재력 또한 무궁무진할 것으로 기대된다. 본 논문에서는 무인항공기 기반의 빅데이터 처리 시스템의 프로토타입을 설계 및 제안 하였다.

동적인 위협이 존재하는 전장에서의 무인 항공기 지역경로계획 (A Local Path Planning for Unmanned Aerial Vehicle on the Battlefield of Dynamic Threats)

  • 김기태;남용근;조성진
    • 산업경영시스템학회지
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    • 제35권1호
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    • pp.39-46
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    • 2012
  • An unmanned aerial vehicle (UAV) is a powered aerial vehicle that does not carry a human operator, uses aerodynamic forces to provide vehicle lift, can fly autonomously or be piloted remotely, can be expendable or recoverable, and can carry a lethal or non-lethal payload. An UAV is very important weapon system and is currently being employed in many military missions (surveillance, reconnaissance, communication relay, targeting, strike, etc.) in the war. To accomplish UAV's missions, guarantee of survivability should be preceded. The main objective of this study is a local path planning to maximize survivability for UAV on the battlefield of dynamic threats (obstacles, surface-to-air missiles, radar etc.). A local path planning is capable of producing a new path in response to environmental changes. This study suggests a $Smart$ $A^*$ (Smart A-star) algorithm for local path planning. The local path planned by $Smart$ $A^*$ algorithm is compared with the results of existing algorithms ($A^*$ $Replanner$, $D^*$) and evaluated performance of $Smart$ $A^*$ algorithm. The result of suggested algorithm gives the better solutions when compared with existing algorithms.

Smart-UAV를 위한 Ku-대역 탑재영상 송수신시스템의 설계 및 해석 (Analysis and Design of Ku-Band Airborne Video Transceiver System for Smart-UAV)

  • 김봉경;김종만;이동국;김태식;김인규
    • 한국통신학회논문지
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    • 제29권7A호
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    • pp.807-813
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    • 2004
  • 본 논문은 21세기 지식기반경제의 국제사회에서 경쟁할 수 있는 우리만의 강점기술을 전략적 선택으로 집중개발 필요성 증대에 따라 추진하게 된 ‘21세기 뉴-프론티어 연구개발사업’ 의 일환인 ‘스마트 무인기(Smart Unmanned Aerial Vehicle) 기술개발’ 에 해당되며, 이 중 스마트 무인기의 운용에 필요한 원격명령(Tele-Command)신호의 수신기능과 동시에 영상(Video)신호 및 원격측정(Tele-Metry)신호를 송신하는 기능 등을 수행하는 Ku-대역 탑재영상 송수신시스템을 설계하였다. 또한, 설계된 전체 통신시스템의 체계요구에 만족하기 위하여 이를 해석하였으며, 전체 시스템의 모듈별 시뮬레이션 및 제작을 통해 본 논문의 타당성을 보였다.

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.

무인비행체를 이용한 건축물의 긴급 위험도 평가 기술 (SMART SKY EYE) 개발 (Rapid Structural Safety Evaluation Method of Buildings using Unmanned Aerial Vehicle (SMART SKY EYE))

  • 정동민;이종훈;이다혜;주영규
    • 대한건축학회논문집:구조계
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    • 제35권2호
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    • pp.3-11
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    • 2019
  • The recent earthquake of Pohang (M5.4) and the Gyeongju earthquake (M5.8) suggested the possibility of a strong earthquake in Korea and reminded us that the Korea is no longer an earthquake-safe zone. In the disaster recovery stage in a disaster like an earthquake, the investigation of the damage situation and the safety assessment of the building serve to provide important information for the initial action such as establishment of the recovery strategy and rescue of the survivor. However, the research that depends on manpower can not cope with the difficulty of processing a large number of doses in a short time, and the expertise of the manpower must be taken into consideration, which may result in delayed initial action. In this study, we propose an rapid safety evaluation technique of building using unmanned aerial vehicle which evaluates the performance and safety of buildings by integrating conventional safety inspection method with unmanned aerial vehicle technology and developed evaluation method of each evaluation factor. In order to verify this, the buildings damaged by the earthquake in Pohang were checked and compared using this system. The results are consistent with the results of the existing emergency earthquake risk assessment. As a result, the possibility of checking the emergency safety using the unmanned aerial vehicle for the damaged structures in case of a large-scale disaster such as an earthquake was confirmed.

스마트무인기 로터 블레이드 국산화 개발 (Localization Development of Rotor Blade for Smart Unmanned Aerial Vehicle)

  • 이명규
    • 항공우주기술
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    • 제10권2호
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    • pp.11-19
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    • 2011
  • 스마트무인기 로터 블레이드의 국산화 개발이 수행되었다. 국산화 개발은 원소재와 물성치가 가장 유사한 국내 생산 복합소재의 선정, 새로운 소재의 물성치 데이터 구축을 위한 쿠폰시험, 블레이드 단면 물성치의 재계산, 공진, 정적/피로 강도, 공탄성 안정성의 구조동역학 설계요구조건에 대한 검증 등을 포함하며, 그 결과에 대하여 기술하였다. 또한 본 논문에서는 스마트무인기 국산화 블레이드 개발과정에서 개선된 공정에 대하여 간략히 기술하였다.

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.

스마트 무인기 풍동시험 (Wind Tunnel Testing for Smart Unmanned Aerial Vehicle)

  • 장진덕;최성욱;이장연
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.37-40
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    • 2006
  • Wind tunnel testings to develope tilt-rotor Smart Unmanned Aerial Vehicle (SUAV) were intensively performed. Small wind tunnel was used to find and evaluate design parameters and to fix general layout of configuration. The application of large tunnel with 40% scaled model is to collect performance and stability related aerodynamic data. During large scale model test wind tunnel is used as a tool to compare Flaperon types, to improve lift characteristics by using different height vortex generators and to alleviate nacelle separated flow effects on the wing.

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Smart tracking design for aerial system via fuzzy nonlinear criterion

  • Wang, Ruei-yuan;Hung, C.C.;Ling, Hsiao-Chi
    • Smart Structures and Systems
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    • 제29권4호
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    • pp.617-624
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    • 2022
  • A new intelligent adaptive control scheme was proposed that combines the control based on interference observer and fuzzy adaptive s-curve for flight path tracking control of unmanned aerial vehicle (UAV). The most important contribution is that the control configurations don't need to know the uncertainty limit of the vehicle and the influence of interference is removed. The proposed control law is an integration of fuzzy control estimator and adaptive proportional integral (PI) compensator with input. The rated feedback drive specifies the desired dynamic properties of the closed control loop based on the known properties of the preferred acceleration vector. At the same time, the adaptive PI control compensate for the unknown of perturbation. Additional terms such as s-surface control can ensure rapid convergence due to the non-linear representation on the surface and also improve the stability. In addition, the observer improves the robustness of the adaptive fuzzy system. It has been proven that the stability of the regulatory system can be ensured according to linear matrix equality based Lyapunov's theory. In summary, the numerical simulation results show the efficiency and the feasibility by the use of the robust control methodology.