論文

査読有り
2015年4月

Lift control of electric airplanes by using propeller slipstream for safe landing

Proceedings - 2015 IEEE International Conference on Mechatronics, ICM 2015
  • Nobukatsu Konishi
  • ,
  • Hiroshi Fujimoto
  • ,
  • Yasumasa Watanabe
  • ,
  • Kojiro Suzuki
  • ,
  • Hiroshi Kobayashi
  • ,
  • Akira Nishizawa

開始ページ
335
終了ページ
340
記述言語
掲載種別
研究論文(国際会議プロシーディングス)
DOI
10.1109/ICMECH.2015.7083998

© 2015 IEEE. Aircrafts are desired to be more energy efficient and safer due to the increasing demand for air transportations. However, generally speaking, nowadays commercial airplanes tend to loss stability under wind disturbances, especially during landing. On the other hand, electric airplanes (EAs) are believed to satisfy the two demands because electric motors are used for the propulsion. Especially, as the actuators, electric motors can improve the control performances of EAs compared with internal combustion engines (ICEs). In this paper, by utilizing electric motors' advantages, lift control method using propeller slipstream is proposed for safe landing, which might be a key technology to innovate the design of EAs. Moreover, simulations and experiments are conducted to verify the effectiveness of the proposed method.

リンク情報
DOI
https://doi.org/10.1109/ICMECH.2015.7083998
Scopus
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84929377945&origin=inward
Scopus Citedby
https://www.scopus.com/inward/citedby.uri?partnerID=HzOxMe3b&scp=84929377945&origin=inward
ID情報
  • DOI : 10.1109/ICMECH.2015.7083998
  • SCOPUS ID : 84929377945

エクスポート
BibTeX RIS