논문상세정보
' 고정익 수직이착륙 무인항공기를 위한 하이브리드-전기 추진시스템의 타당성 연구' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • battery(배터리)
  • electricmotor(전기모터)
  • power management system(전력 제어 시스템)
  • series hybrid-electric propulsion system(직렬 하이브리드-전기 추진시스템)
  • vtol fixed wing uav(고정익 수직이착륙 무인항공기)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
38 0

0.0%

' 고정익 수직이착륙 무인항공기를 위한 하이브리드-전기 추진시스템의 타당성 연구' 의 참고문헌

  • 다극 브레이크 모터의 긴 전류 제어주기 고속영역 제어
    이근호 제어.로봇.시스템학회 논문지 21 (2) : 137 ~ 144 [2015]
  • World’s first serial hybrid electric aircraft to fly at LeBourget
    Martini, F. Le Bourget [2011]
  • Unmanned Vehicles Anual handbook issue 22
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    William, W. [2015]
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  • Power managements of a hybrid electric propulsion system for UAVs
    Bohwa Lee Journal of Mechanical Science and Technology 26 (8) : 2291 ~ 2299 [2012]
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    Tomažič, T. Strojniški vestnik-Journal of Mechanical Engineering 57 (12) : 869 ~ 878 [2011]
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    Harmon CALIFORNIA UNIV DAVIS DEPT OF MECHANICAL AND AERONAUTICAL ENGINEERING, No. CI04-1076 [2005]
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    Robertson, P. Cambridge Energy [2008]
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    Schömann, Joachim Technische Universität München [2014]
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    Husain, I. CRC Press [2011]
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    Fredericks, W. J. AIAA Aviation Technology, Integration, and Operations (ATIO) Conference 12 (14) [2013]
  • Battery System for Smart Electric Vehicles
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