한국항공운항학회지 (Journal of the Korean Society for Aviation and Aeronautics)

  • 제30권1호
  • /
  • Pages.38-43
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  • 2022
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  • 1225-9705(pISSN)
  • /
  • 2466-1791(eISSN)
한국항공운항학회 (The Korean Society for Aviation and Aeronautics)
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통합항법 성능 분석을 위한 고정익, 회전익 무인항공기의 비행 시나리오 궤적 설계

Flight Scenario Trajectory Design of Fixed Wing and Rotary Wing UAV for Integrated Navigation Performance Analysis

  • 원대한 (한서대학교 항공시스템공학과) ;
  • 오정환 (한서대학교 항공시스템공학과) ;
  • 강우성 (한서대학교 항공시스템공학과) ;
  • 엄송근 (한서대학교 항공시스템공학과) ;
  • 이동진 (한서대학교 무인항공기학과) ;
  • 김도윤 (한국항공우주연구원) ;
  • 한상혁 (한국항공우주연구원)
  • 투고 : 2021.11.24
  • 심사 : 2022.03.25
  • 발행 : 2022.03.31
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초록

As the use of unmanned aerial vehicles increases, in order to expand the operability of the unmanned aerial vehicle, it is essential to develop an unmanned aerial vehicle traffic management system, and to establish the system, it is necessary to analyze the integrated navigation performance of the unmanned aerial vehicle to be operated. Integrated navigation performance is affected by various factors such as the type of unmanned aerial vehicle, flight environment, and guidance law algorithm. In addition, since a large amount of flight data is required to obtain high-reliability analysis results, efficient and consistent flight scenarios are required. In this paper, a flight scenario that satisfies the requirements for integrated navigation performance analysis of rotary and fixed-wing unmanned aerial vehicles was designed and verified through flight experiments.

키워드

과제정보

본 연구는 과학기술정보통신부 무인이동체 미래선도핵심기술개발사업의 연구과제(과제고유번호: NRF-2017M1B3A2A01049995)의 지원으로 수행되었습니다.

참고문헌

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