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      전원부하분석을 통한 무인항공기 전기시스템 설계 및 검증 = Design and Verification of Electrical System for Unmanned Aerial Vehicle through Electrical Load Power Analysis

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      https://www.riss.kr/link?id=A105927404

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      다국어 초록 (Multilingual Abstract)

      In this paper, we have proposed a design and verification methods of electrical system and power loads for unmaned aeriel vehicles(UAVs) through electrical load analysis. In order to meet a UAV system requirement and electrical system specifications, we have designed an electrical power system for efficient power supply and distribution and have theoretically analyzed the power loads according to the power consumption and power bus design of UAV. Using electrical system rig, the designed electrical power system has been experimentally verified.
      Also, we have performed several flight tests to verify the UAV electrical system and power loads. It is concluded that the proposed design and verification method of electrical system for UAV system.
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      In this paper, we have proposed a design and verification methods of electrical system and power loads for unmaned aeriel vehicles(UAVs) through electrical load analysis. In order to meet a UAV system requirement and electrical system specifications, ...

      In this paper, we have proposed a design and verification methods of electrical system and power loads for unmaned aeriel vehicles(UAVs) through electrical load analysis. In order to meet a UAV system requirement and electrical system specifications, we have designed an electrical power system for efficient power supply and distribution and have theoretically analyzed the power loads according to the power consumption and power bus design of UAV. Using electrical system rig, the designed electrical power system has been experimentally verified.
      Also, we have performed several flight tests to verify the UAV electrical system and power loads. It is concluded that the proposed design and verification method of electrical system for UAV system.

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      참고문헌 (Reference)

      1 Lester F. Faleiro, "Trends Towards a More Electrical Aircraft" 2006

      2 Spitzer, C. R., "The All-Electric Aircraft: A Systems View and Proposed NASA Research Programs" NASA Langley Research Center 261-266, 1984

      3 David Blanding, "Subsystem Design and Integration for The More Electric Aircraft" 2006

      4 Miguel A. Maldonado, "Power Management and Distribution System for a More-Electric Aircraft (MADMEL) - Program Status" 274-279, 1997

      5 Rosero, J.A., "Moving Towards a More Electric Aircraft" IEEE 22 (22): 2007

      6 "MIL-STD-704F, Aircraft Electric Power Characteristics"

      7 "MIL-E-7061F, Aircraft Electric Load and Power Source Capacity"

      8 H. C. Woo, "Electrical System of Unmanned Aerial Vehicle, Patent Number : 10-1719480"

      9 D. Izquierdo, "Electrical Power Distribution System(HV270DC), for Application in More Electric Aircraft" IEEE 2010

      10 M. Howse, "All Electric Aircraft" 17 : 35-37, 2003

      1 Lester F. Faleiro, "Trends Towards a More Electrical Aircraft" 2006

      2 Spitzer, C. R., "The All-Electric Aircraft: A Systems View and Proposed NASA Research Programs" NASA Langley Research Center 261-266, 1984

      3 David Blanding, "Subsystem Design and Integration for The More Electric Aircraft" 2006

      4 Miguel A. Maldonado, "Power Management and Distribution System for a More-Electric Aircraft (MADMEL) - Program Status" 274-279, 1997

      5 Rosero, J.A., "Moving Towards a More Electric Aircraft" IEEE 22 (22): 2007

      6 "MIL-STD-704F, Aircraft Electric Power Characteristics"

      7 "MIL-E-7061F, Aircraft Electric Load and Power Source Capacity"

      8 H. C. Woo, "Electrical System of Unmanned Aerial Vehicle, Patent Number : 10-1719480"

      9 D. Izquierdo, "Electrical Power Distribution System(HV270DC), for Application in More Electric Aircraft" IEEE 2010

      10 M. Howse, "All Electric Aircraft" 17 : 35-37, 2003

      11 Emadi, K., "Aircraft Power Systems:Technology, State of the Art, and Future Trends" IEEE 15 (15): 2000

      12 E. H. J. Pallet, "Aircraft Electrical System" Pearson, Prentice Hall 1991

      13 H. C. Woo, "A Study on the Simulation Test Method of Unmanned Aerial Vehicle Electrical System" KSAS 129-138, 2015

      14 M. David Kankam, "A Servey of Power Electronics Applications in Aerospace Technologies" 2001

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2026 평가예정 재인증평가 신청대상 (재인증)
      2020-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2017-01-01 평가 등재학술지 유지 (계속평가) KCI등재
      2013-01-01 평가 등재 1차 FAIL (등재유지) KCI등재
      2010-01-01 평가 등재학술지 유지 (등재후보2차) KCI등재
      2007-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2006-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.13 0.13 0.1
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.09 0.09 0.244 0.04
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