Robust Adaptive Variable Structure Control of a Flexible Spacecraft Containing Input Nonlinearity/Dead-Zone

• HU Qinglei

  Department of Control Science and Engineering, Harbin Institute of Technology

• MA Guangfu

  Department of Control Science and Engineering, Harbin Institute of Technology

収録刊行物

• TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

  TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 49 (165), 187-191, 2006

  一般社団法人 日本航空宇宙学会

キーワード

• Variable Structure Control
• Vibration Suppression
• Flexible Spacecraft
• Attitude Maneuver
• Input Nonlinearity

詳細情報

• CRID: 1390001204079153280
• NII論文ID: 10018428228
• NII書誌ID: AA0086707X
• DOI: 10.2322/tjsass.49.187
• ISSN: 21894205
• ISSN: 05493811
• NDL書誌ID: 8537299
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I8537299
• Web Site: https://www.jstage.jst.go.jp/article/tjsass/49/165/49_165_187/_pdf
• 本文言語コード: en
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles