• Title/Summary/Keyword: 스마트 무인항공기

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Design of Intelligence Maturity Model for Judging a requirement of Smart UAV's Searching Ability (스마트 무인항공기의 표적탐색 능력 소요판단을 위한 지능화 성숙도 모델 설계)

  • Gang, Dong-Su;Yun, Hui-Byeong
    • Proceedings of the Korean Institute of Intelligent Systems Conference
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    • 2006.11a
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    • pp.310-313
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    • 2006
  • 본 논문은 스마트 무인항공기를 개발하거나 획득시에 요구되는 전투실험 수행 중 지능화 정도에 대한 평가 및 실험방향을 제시를 위한 지능화 성숙도 모델을 제안한다. 먼저 표적탐색 소요검증 전투실험 절차를 제시하고, 지능화 정도를 4단계로 나누어 단계별 요구되는 지능수준을 제시한다. 분류된 지능수준별로 기술수준, 동작수준, 상호운용성 수준 영역의 4단계 각 수준별 요구 능력을 분석, 제시하여 지능화 정도를 측정할 수 있는 지능화 성숙도 모델을 설계한다. 마지막으로 표적탐색 소요판단을 위한 전투실험시 활용 가능한 중점분야를 지능화 성숙도 모델 영역별로 식별하고, 단계별 식별된 중점분야를 실험할 수 있는 전투실험 평가요소를 제시한다.

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

  • Kim, Sa Woong
    • Smart Media Journal
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    • v.5 no.2
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    • pp.51-58
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    • 2016
  • Recently, the unmanned aerial vehicle Drone technology is attracting new interest around the world. The versatilities in science, military, marketing, sports, and entertainment fields are the driving force of the drone fever. Thus, the potential power of future industrial is expected as the application range is extensive. In this paper, we design and propose the prototype of unmanned aerial vehicle-based bigdata processing system.

Research for improving vulnerability of unmanned aerial vehicles (무인항공기 보안 취약점 개선을 위한 연구)

  • Lee, Kyung-Hwan;Ryu, Gab-Sang
    • Smart Media Journal
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    • v.7 no.3
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    • pp.64-71
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    • 2018
  • Utilization of unmanned aerial vehicles (UAVs) are rapidly expanding to various fields ranging from defense, industry, entertainment and personal hobbies. Due to the increased activities of unmanned airplanes, many security problems have emerged, including flight path errors to undesired destinations, secondary threats due to exposed securities caused by the capture of unmanned airplanes in hostile countries. In this paper, we find security vulnerabilities in UAVs such as GPS spoofing, hacking captured video information, malfunction due to signal attenuation through jamming, and exposure of personal information due to image shooting. In order to solve this problem, the stability of the unstructured data is secured by setting the encryption of the video shooting information section using the virtual private network (VPN) to prevent the GPS spoofing attack. In addition, data integrity was ensured by applying personal information encryption and masking techniques to minimize the secondary damage caused by exposure of the UAV and to secure safety. It is expected that it will contribute to the safe use and stimulation of industry in the application field of UAV currently growing.

A Study on Efficient Methods of Pesticide Control Using Agricultural Unmanned Aerial Vehicles (농업용 무인항공기를 활용한 농약방제 효율성 방안에 관한 연구)

  • Jeong, Ga-Young;Cho, Yong-Yoon
    • Journal of Internet of Things and Convergence
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    • v.8 no.2
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    • pp.35-40
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    • 2022
  • In the agricultural environment, pesticide control requires a high risk of work and a high labor force for farmers. The effectiveness of pesticide control using unmanned aerial vehicles varies according to climate, land type, and characteristics of unmanned aerial vehicles. Therefore, an effective method for pesticide control by unmanned aerial vehicles considering the spraying conditions and environmental conditions is required. In this paper, we propose an efficient pesticide control system based on agricultural unmanned aerial vehicles considering the application conditions and environmental information for each crop. The effectiveness of the proposed model was demonstrated by measuring the drop uniformity of pesticides according to the change in altitude and speed after attaching the sensory paper and measuring the penetration rate of the drug inside the canopy according to the change in crop growth conditions. Experiment result, the closer the height of the UAV is to the ground, the more evenly the crops are sprayed, but for safety reasons, 2m more is suitable, and on average a speed of 2m/s is most suitable for control. The proposed control system is expected to help develop intelligent services based on the use of various unmanned aerial vehicles in agricultural environments.

Current Status and Futures of Drones (무인항공기 개발 현황 및 발전방향)

  • Yun, Chul Yong;Kang, Wanggu
    • Proceedings of the Korean Society of Broadcast Engineers Conference
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    • 2015.07a
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    • pp.310-311
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    • 2015
  • 최근 스마트폰등 ICT기반의 전자제품들이 보편화 되면서 무인항공기에 적용 가능한 전자기술들이 급속히 개발되어, 항공 기술과 ICT 기반 전자 기술이 융복합되어 무인항공기는 군용위주의 활동 영역을 넘어 민간분야에서 까지 활발히 진출하고 있다. 현재까지는 전통적인 항공 선도 업체들이 군용무인기 중심의 고가의 무인기를 생산하여 시장을 장악하였으나, 이제는 공공 및 민간영역에서 무인기를 상업화하기 위한 기업들이 등장하고 있어 민수영역에서 무인기 시장은 급성장세에 있다. 국내의 무인기 기술은 기술혁신과 시장창출 주도가 가능한 선진권 수준이며, 무인기의 핵심인 ICT기반 전자부품 기술은 세계 최고의 수준으로 두 분야의 기술을 융복합화하여 경쟁력 있는 무인기 개발을 신속히 진행하면, 전 세계적으로 성장하는 무인기 개발 시장은 우리에게 새로운 성장 동력이 될 수 있다. 자율비행, 상황인식 및 회피 기능 등 미래 무인기 선도기술을 개발하고, 국산화지연 또는 외국의 수출제한 품목에 대한 국산화 개발 및 핵심 부품의 국산 경쟁력 강화를 통하여 무인기 산업의 고부가가치를 창출할 수 있다.

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The Development of Performance Analysis Code for Pre-Conceptual Design of VTOL UAV (수직이착륙/고속순항 무인기 초기개념설계를 위한 성능예측 프로그램 개발)

  • Jung, Won-Hyung;Lee, Kyung-Tae;Kim, Jung-Yub
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.5
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    • pp.1-9
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    • 2004
  • The performance analysis code has been developed for vertical take-off and landing(VTOL) UAV which can be utilized as a trade analysis tool in the pre-conceptual design phase. The UAV requires VTOL capability and high speed cruise performance. The main logic of this performance analysis code is to estimate performance parameters of each mission segment by mission fuel weight iteration. The reliability of this performance analysis code is discussed by comparing the data of existing dual flight mode VTOL UAVs such as Boeing CRW and Bell Tilt Rotor.

Loads Analysis of Smart UAV Using ARGON (ARGON을 이용한 스마트 무인기 비행하중해석)

  • Shin, Jeong-Woo;Kim, Sung-Chan;Hwang, In-Hee
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.7
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    • pp.76-84
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    • 2005
  • For flight loads analysis of Smart UAV, applicable regulations and loads conditions should be prepared in advance, and modeling for aerodynamics, weight, and structure should be performed. Panel method is usually adopted for aircraft loads analysis to obtain aerodynamic loads. In this study, ARGON which is a multidisciplinary fixed wing aircraft design software co-developed by KARI and TsAGI was used for loads analysis. ARGON can be utilized for flutter and stress analysis as well as for flight and ground loads analysis. In this paper, flight loads analysis of Smart UAV which is a FAR 23 category airplane was performed with ARGON and the results were presented.

A Study on the Development of Airworthiness Standards for VTOL UAS (수직이착륙(VTOL) 무인항공기 감항기준 개발에 대한 연구)

  • Gil, Ginam;Yoo, Minyoung;Park, Jongsung
    • Journal of Aerospace System Engineering
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    • v.14 no.1
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    • pp.44-53
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    • 2020
  • In conjunction with the Fourth Industrial Revolution, the unmanned aerial vehicle industry is being developed to a new paradigm by combining advanced technologies such as AI, Big Data and the IoT. Aeronautical developed countries such as the U.S. are focusing their efforts on the development of the safer unmanned aerial vehicles. The Korea Aerospace Research Institute, as part of the national R&D project in 2011, had succeeded in developing the first vertical takeoff and landing (VTOL) UAS, called Smart-UAV. However, although the development technology of the VTOL UAS is possessed, developing and operating of the VTOL UAS for commercial or military use are limited. The type certification procedure of the VTOL UAS developed by domestic technology is stipulated in the Korean Aviation Safety Act, but the Korean VTOL UAS airworthiness standards (KAS) hsve not been established. Thus, this study investigated the development trends of the VTOL UAS in Korea and abroad and national certification systems and procedures, and benchmarked the special conditions for the VTOL aircraft, announced by the EASA on July 2, 2019, to establish standards for type certificate of the VTOL UAS in Korea.

Development of Transient Simulation Program for Smart UAV Propulsion System (스마트 무인기 추진기관의 천이 모사 프로그램 개발)

  • Lee, Chang-Ho;Ki, Ja-Young
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.6
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    • pp.63-69
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    • 2011
  • The Smart UAV must have the control characteristics of propulsion system necessary for both rotary aircraft and fixed wing aircraft though it equips turbo-shaft engine. To develop an electronic engine controller in the future, it is necessary to accumulate the experience of engine operation and data of tilt rotor aircraft. For this purpose, the computer programs which predict engine performance in the steady state and transient state can be utilized for the supplementation of flight test data. In this work, we developed a dynamic analysis program using engine performance data gathered during the flight tests. In addition the accuracy of the program was verified through comparison with flight test data and the results of steady-state performance analysis program.

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

  • Kang, Dong-Su;Yoon, Hee-Byung
    • Journal of the Korean Institute of Intelligent Systems
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    • v.17 no.5
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    • pp.668-673
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    • 2007
  • We propose the design of the warfighting experiment process for software intensive systems using the intelligent maturity model and suggest the application results of the target searching capability in smart UAV. For this, we design the intelligent maturity model to evaluate the intelligent degree of the software intensive systems considering the domain and intelligent level. Then we classify the IS0/1EC-12207 process and CMMI process as LITO domain for designing the warfighting experiment process, map the classifed process to the five factors of the warfighting experiment and derive the process as warfighting experiment element and phase. Based on the derived process, we design the warfighting experiment process using the IDEF0. Finally we apply the proposed process to the target search capability and suggest the results which are required to develop and acquire the smart UAV.