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Multivariable finite-time output feedback trajectory tracking control of quadrotor helicopters

  • Bailing Tian*
  • , Hanchen Lu
  • , Zongyu Zuo
  • , Qun Zong
  • , Yunpeng Zhang
  • *此作品的通讯作者
  • Tianjin University
  • Northeastern University China
  • National Key Laboratory of Science and Technology on Aircraft Control

科研成果: 期刊稿件文章同行评审

摘要

A continuous multivariable output feedback control scheme is developed for trajectory tracking and attitude stabilization of quadrotor helicopters. The whole closed-loop system is composed by position loop and attitude loop. The homogeneous technique is used to design finite-time stabilizing controller and observer in each loop. The virtual control is introduced in position loop to ensure that the real control is smooth enough such that it can be tracked by attitude loop. The finite-time stability of the closed-loop system is guaranteed through homogeneity and Lyapunov analysis. Finally, the efficiency of the proposed algorithm is illustrated by numerical simulations.

源语言英语
页(从-至)281-295
页数15
期刊International Journal of Robust and Nonlinear Control
28
1
DOI
出版状态已出版 - 10 1月 2018

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