Engine controller for hybrid powered dual quad-rotor system

Chin-E. Lin, Thanakorn Supsukbaworn, Ying Chi Huang, Kai Ti Jhuang, Chia Hsun Li, Chin Yu Lin, Szu Yu Lo

研究成果: Conference contribution

4 引文 斯高帕斯(Scopus)

摘要

Multi-rotor systems have been developed into better performance for mature applications. Due to lift to weight balance on motor power and battery energy, they are limited in payload and flight endurance. Since gasoline power has 44 times better energy density than battery, integration of gas engine and DC brushless motor into a vertical take-off and landing (VTOL) system will gain much higher lift and longer flight duration in performance. A hybrid power multi-rotor system is designed by dual system of engine-driven quad-rotor and motor-driven quad-rotor, with contributions on lift power by gas engine and flight control, respectively. The proposed multi-rotor system is termed as Quad-in-Quad (QiQ) system. System design considerations on high thrust, reverse torque, vibration, heat dissipation, structure and weight balance are included by carefully weight reduction into fabrication. Microprocessor control system is designed and implemented to make gas engine in both directions in steady balanced operation. A preliminary flight test has completed on this dual quad-rotor VTOL.

原文English
主出版物標題IECON 2015 - 41st Annual Conference of the IEEE Industrial Electronics Society
發行者Institute of Electrical and Electronics Engineers Inc.
頁面1513-1517
頁數5
ISBN(電子)9781479917624
DOIs
出版狀態Published - 2015 一月 1
事件41st Annual Conference of the IEEE Industrial Electronics Society, IECON 2015 - Yokohama, Japan
持續時間: 2015 十一月 92015 十一月 12

出版系列

名字IECON 2015 - 41st Annual Conference of the IEEE Industrial Electronics Society

Other

Other41st Annual Conference of the IEEE Industrial Electronics Society, IECON 2015
國家Japan
城市Yokohama
期間15-11-0915-11-12

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering
  • Industrial and Manufacturing Engineering

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