DOI QR코드

DOI QR Code

A Study on Design and Verification of Power Monitoring Unit for Unmanned Aerial Vehicle

무인항공기용 전원모니터링장치 설계 및 검증에 관한 연구

  • Received : 2019.11.28
  • Accepted : 2020.03.30
  • Published : 2020.04.01

Abstract

This paper describes a Power Monitoring Unit (PMU) for Unmanned Aerial Vehicle (UAV) electrical system, It is designed for the PMU which performs data sensing of generator, transformer rectifier unit (TRU), battery and gear box installed in UAV and operate power ON/OFF devices of mission equipment. The PMU measures the voltage and current for the aircraft power source (generators, transformer rectifier unit and battery), measures the pressure and temperature of the gearbox, and performs the mission equipment power command received from the mission computer. The PMU was designed to meet the requirements of the UAV, and was performed through structure/thermal analysis, environmental test, EMI test and ground/flight tests.

본 논문은 무인항공기 전기시스템을 위한 전원모니터링장치에 대해서 기술하고 있으며, 무인항공기에 장착되는 AC/DC 발전기, 전원변환기, 배터리 및 기어박스의 데이터 측정과 임무장비의 전원 ON/OFF 장치를 운용하는 전원모니터링장치에 대한 설계를 기술하였다. 전원모니터링장치는 비행체 전원(발전기, 전원변환기 및 배터리)에 대한 전압과 전류를 측정하고, 기어박스의 압력과 온도를 측정하며, 임무컴퓨터로부터 수신된 임무장비의 전원명령을 수행한다. 전원모니터링장치는 무인항공기 비행체 요구사항을 만족하도록 설계하였으며, 구조/열 해석, 환경/EMI 및 지상/비행시험을 통하여 검증을 수행하였다.

Keywords

References

  1. Izquierdo, D., Azcona, R., Lopez del Cerro, F. J., Fernandez, C., and Delicado, B., "Electrical Power Distribution System (HV270DC), for Application in More Electric Aircraft," Applied Power Electronics Conference and Exposition, IEEE, CA, February 21-25, 2010.
  2. Spitzer, C. R., "The All-Electric Aircraft: A Systems View and Proposed NASA Research Programs," NASA Langley Research Center, Aerospace and Electronic Systems, IEEE Transactions, Vol. AES-20, Issue 3, May 1984, pp. 261-266 https://doi.org/10.1109/TAES.1984.310509
  3. Faleiro, L. F., "Trends Towards a More Electrical Aircraft," Proceeding of ICAS 2006.
  4. Howse, M., "All Electric Aircraft," Power Engineer, Vol. 17, 2003, pp. 35-37. https://doi.org/10.1049/pe:20030410
  5. Blanding, D., "Subsystem Design and Integration for The More Electric Aircraft," Proceeding of ICAS 2006.
  6. Rosero, J. A., Ortega, J. A., Aldabas, E., and Romeral, L., "Moving Towards a More Electric Aircraft" Aerospace and Electronic Systems Magazine, IEEE, Volume 22, Issue 3, March 2007.
  7. Kankam, M. D., "A Servey of Power Electronics Applications in Aerospace Technologies," 36th Intersociety Energy Conversion Engineering Conference Cosponsored by the ASME, IEEE, AIChE, ANS, SAE, and AIAA Savannah, Georgia, July 29-August 2, 2001.
  8. Kang, J. M., Jeong, K. S., Kang, B. S., and Kim, J. M., "Study on Production of Power Monitoring Unit for Electric Propulsion UAV," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 45, No. 2, February 2017, pp. 140-148 https://doi.org/10.5139/JKSAS.2017.45.2.140
  9. Woo, H. C., and Kim, Y. T., "Electrical System of Unmanned Aerial Vehicle", Korean Intellectual Property Office, Patent Number : 10-1719480, March 2017.
  10. Woo, H. C., "Design and Verification of Electrical System for Unmanned Aerial Vehicle through Electrical Load Power Analysis," Journal of the Korea Institute of Military Science and Technology, Vol. 21, No. 5, October 2018, pp. 675-683 https://doi.org/10.9766/KIMST.2018.21.5.675
  11. MIL-STD-461F, "Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment," Department of Defense, 2007.
  12. MIL-STD-810G, "Environmental Engineering Considerations and Laboratory Tests," Department of Defense, 2008.