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Robust output tracking control of a laboratory helicopter for automatic landing

  • Hao Liu*
  • , Geng Lu
  • , Yisheng Zhong
  • *此作品的通讯作者
  • Tsinghua University

科研成果: 期刊稿件文章同行评审

摘要

In this paper, robust output tracking control problem of a laboratory helicopter for automatic landing in high seas is investigated. The motion of the helicopter is required to synchronise with that of an oscillating platform, e.g. The deck of a vessel subject to wave-induced motions. A robust linear time-invariant output feedback controller consisting of a nominal controller and a robust compensator is designed. The robust compensator is introduced to restrain the influences of parametric uncertainties, nonlinearities and external disturbances. It is shown that robust stability and robust tracking property can be achieved simultaneously. Experimental results on the laboratory helicopter for automatic landing demonstrate the effectiveness of the designed control approach.

源语言英语
页(从-至)2242-2250
页数9
期刊International Journal of Systems Science
45
11
DOI
出版状态已出版 - 2 11月 2014
已对外发布

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