Vertical landing of a fixed-wing UAV using the flat spin

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

1 被引用数 (Scopus)

抄録

This paper studies a feasibility of a novel landing method especially in a limited space for an ordinary Unmanned Aerial Vehicle (UAV) using the flat spin. Use of the combination of an all-flying tail with large deflection angle has been found effective for quick intentional flat spin entry, and the higher propeller rotational speed as well as the high all-flying tail deflection angle has been also found effective for flatter or even positive pitch attitude during the spin. One of the key issues to realize flat-spin landing is to control its descent path toward the desired landing point. The influences of change in pitch attitude on the descent path are examined in flight tests, and the periodic pitch attitude change caused by the deflection of the all-flying tail with full throttle was found effective for the descent path control.

本文言語英語
ホスト出版物のタイトル31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
出版社International Council of the Aeronautical Sciences
ISBN(電子版)9783932182884
出版ステータス出版済み - 1 1 2018
イベント31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018 - Belo Horizonte, ブラジル
継続期間: 9 9 20189 14 2018

出版物シリーズ

名前31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018

その他

その他31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
Countryブラジル
CityBelo Horizonte
Period9/9/189/14/18

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering
  • Control and Systems Engineering
  • Materials Science(all)
  • Aerospace Engineering

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