Takeoff and landing control using force sensor by electrically-powered helicopters

Akira Shimada, Masanori Fujita

研究成果査読

8 被引用数 (Scopus)

抄録

A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the focre sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost take off from the base. Concurrently, the forse sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value cprresponding to the weight. This paper introduces the design process including system modeling and the experimental results.

本文言語English
ページ62-65
ページ数4
DOI
出版ステータスPublished - 2006 11 21
イベント9th IEEE International Workshop on Advanced Motion Control, 2006 - Istanbul, Turkey
継続期間: 2006 3 272006 3 29

Conference

Conference9th IEEE International Workshop on Advanced Motion Control, 2006
国/地域Turkey
CityIstanbul
Period06/3/2706/3/29

ASJC Scopus subject areas

  • 制御およびシステム工学
  • モデリングとシミュレーション
  • コンピュータ サイエンスの応用
  • 電子工学および電気工学

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