跳到主要导航 跳到搜索 跳到主要内容

Trajectory Tracking Control for the Flexible Wings of a Micro Aerial Vehicle

  • Wei He
  • , Tingting Meng
  • , Shuang Zhang
  • , Quanbo Ge
  • , Changyin Sun
  • University of Science and Technology Beijing
  • CAS - Academy of Mathematics and System Sciences
  • Hangzhou Dianzi University
  • Southeast University, Nanjing

科研成果: 期刊稿件文章同行评审

32 引用 (Scopus)

摘要

This paper mainly regulates a flexible wing of a micro aerial vehicle to track two spatiotemporally varying trajectories. By utilizing Lyapunov's direct method, two boundary control laws are designed to guarantee uniform boundedness of the closed-loop target system along the time axis. Based on Schur complement lemma, nonlinear inequalities derived from the theoretical deduction are rewritten as matrixes, which are solved through the LMI toolbox in MATLAB. In addition, the tracking control problem is formulated as an optimization problem. The simulation examples are conducted to prove the effectiveness of the proposed boundary control laws.

源语言英语
期刊论文编号8249753
页(从-至)2431-2441
页数11
期刊IEEE Transactions on Systems, Man, and Cybernetics: Systems
48
12
DOI
出版状态已出版 - 12月 2018
已对外发布

学术指纹

探究 'Trajectory Tracking Control for the Flexible Wings of a Micro Aerial Vehicle' 的科研主题。它们共同构成独一无二的学术指纹。

引用此