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

Akira Shimada, Masanori Fujita

研究成果: Paper

7 引用 (Scopus)

抜粋

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.

元の言語English
ページ62-65
ページ数4
DOI
出版物ステータス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
Turkey
Istanbul
期間06/3/2706/3/29

    フィンガープリント

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Modelling and Simulation
  • Computer Science Applications
  • Electrical and Electronic Engineering

これを引用

Shimada, A., & Fujita, M. (2006). Takeoff and landing control using force sensor by electrically-powered helicopters. 62-65. 論文発表場所 9th IEEE International Workshop on Advanced Motion Control, 2006, Istanbul, Turkey. https://doi.org/10.1109/AMC.2006.1631633