Attitude control system design of a helicopter experimental system

• Inoue, Akira

• Deng, Mingcong

• Harima, Takanori

• Nakano, Seiji

• Ueki, Nobuyuki

抄録

In this paper, we consider the problem of attitude control of a helicopter experimental system. We design a nonlinear controller which combines nonlinear adaptive robust control and nonlinear feedback controls. Simulation and experimental results show the effectiveness of the proposed method.

収録刊行物

• Industrial Technology

  Industrial Technology 1240-1245, 2005-12

キーワード

• adaptive control
• aircraft control
• control system synthesis
• feedback
• helicopters
• nonlinear control systems
• robust control

詳細情報

• CRID: 1050846637628214912
• NII論文ID: 120002305698
• Web Site: https://ousar.lib.okayama-u.ac.jp/30012
• 本文言語コード: en
• 資料種別: journal article
• データソース種別:
  • IRDB
  • CiNii Articles