力センサを用いた電動ヘリコプタの離着陸制御 Takeoff and Landing Control using Force Sensor by Electrically-Powered Helicopters

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著者

    • 藤田 真宜 FUJITA Masanori
    • 職業能力開発総合大学校電気システム工学科 Dept. of Electrical System Engineering, Polytechnic University
    • 島田 明 SHIMADA Akira
    • 職業能力開発総合大学校電気システム工学科 Dept. of Electrical System Engineering, Polytechnic University

抄録

This paper introduces a takeoff and landing control technique related to a helicopter. The presented control system consists of a small toy electrically-powered helicopter for indoor flights, a flight base under which a focre sensor is set, and a helicopter control terminal which is connected to a system controller. The force sensor use is intended to realize soft takeoff and landing control. When the helicopter stands on the base, the force sensor outputs lift force data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost takes off from the base. Concurrently, the forse sensor output closes to 0. Thus, if the system controller controls the voltage arbitrarily, it is expected to realize the soft takeoff and landing control. This paper introduces the design process including modeling based on ststem identification technique, and shows the simulation and experimental results of the lift force control.

収録刊行物

  • 電気学会論文誌. D, 産業応用部門誌 = The transactions of the Institute of Electrical Engineers of Japan. D, A publication of Industry Applications Society  

    電気学会論文誌. D, 産業応用部門誌 = The transactions of the Institute of Electrical Engineers of Japan. D, A publication of Industry Applications Society 127(2), 112-117, 2007-02-01 

    The Institute of Electrical Engineers of Japan

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被引用文献:  3件

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各種コード

  • NII論文ID(NAID)
    10018480122
  • NII書誌ID(NCID)
    AN10012320
  • 本文言語コード
    JPN
  • 資料種別
    ART
  • ISSN
    09136339
  • NDL 記事登録ID
    8668297
  • NDL 雑誌分類
    ZN31(科学技術--電気工学・電気機械工業)
  • NDL 請求記号
    Z16-1608
  • データ提供元
    CJP書誌  CJP引用  NDL  J-STAGE 
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