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Flight control design for small-scale helicopter using disturbance- observer-based backstepping

  • Hao Lu
  • , Cunjia Liu*
  • , Lei Guo
  • , Wen Hua Chen
  • *此作品的通讯作者
  • Beihang University
  • School of Instrumentation Science and Opto-Electronics Engineering
  • Loughborough University
  • National Key Laboratory on Aircraft Control Technology

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

A study adopts the disturbance-observer-based control scheme to enhance the flight control performance. This method is known as an active anti-disturbance strategy where the lumped disturbances from various sources are estimated by a disturbance observer (DO) and then incorporated into a nominal controller to compensate for their adverse effects. A preliminary study has demonstrated the disturbance rejection ability of this control strategy on a small-scale helicopter. The study proposes a novel disturbance-observer design that extends the scope of the classical one to a partial-state unmeasurable system.

源语言英语
页(从-至)2235-2240
页数6
期刊Journal of Guidance, Control, and Dynamics
卷38
期11
DOI
出版状态已出版 - 2015

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