한국항공우주학회지 (Journal of the Korean Society for Aeronautical & Space Sciences)

  • 제39권10호
  • /
  • Pages.959-965
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  • 2011
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  • 1225-1348(pISSN)
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  • 2287-6871(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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소형 연료전지 무인기의 전기추진시스템용 전력원 모델링 및 시뮬레이션

A Electric Power Source Modeling and Simulation for Electric Propulsion Systems of a Fuel Cell Powered Small UAV

  • 투고 : 2011.06.29
  • 심사 : 2011.09.07
  • 발행 : 2011.10.01
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초록

본 논문에서는 소형 무인기의 전기추진 시스템에 대한 모델링 및 전력 시뮬레이션에 관하여 기술하였다. 각 전력원 모델링 및 시뮬레이션을 위해 Matlab/Simulink를 사용하였고, 연료전지와 배터리를 주 전력원으로 사용하는 200 W급 전기추진 시스템에 대하여 4시간 30분의 비행 시험결과와 시뮬레이션 한 결과를 비교하였다. 그 결과, 시뮬레이션은 각 전력원의 성능 및 동특성을 적절히 모사하였고, 이를 통해 다른 급의 전기추진 시스템에 대한 전력특성변화를 예측하는 도구로 활용 가능함을 알 수 있었다.

A modeling and power simulation of a small UAV's electric propulsion systems is described. Each power source is modeled and simulated in Matlab/Simulink and it is compared flight test data during 4 hr 30 min with simulation results about 200 W electric propulsion system using fuel cell and battery as a main power sources. In result, it is properly simulated performance and dynamic characteristic of each electric power source. Through this, it is revealed that the simulation is available as a means of predicting power characteristic variation for electric propulsion systems of different class.

키워드

참고문헌

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피인용 문헌

  1. A Study on Optimum Takeoff Time of the Hybrid Electric Powered Systems for a Middle Size UAV vol.40, pp.11, 2012, https://doi.org/10.5139/JKSAS.2012.40.11.940
  2. Flight Test of Hybrid Propulsion System for Electrically Powered UAV vol.17, pp.4, 2013, https://doi.org/10.6108/KSPE.2013.17.4.049
  3. Research Trend and Analysis of Altitude and Endurance for Fuel Cell Unmanned Aerial Vehicles vol.25, pp.4, 2014, https://doi.org/10.7316/KHNES.2014.25.4.393