跳到主要导航 跳到搜索 跳到主要内容

Inverse model control for inner loop of control loading system on flight simulator

  • School of Mechatronics Engineering, Harbin Institute of Technology
  • China University of Mining and Technology
  • Suzhou Lingyun Test System Co. Ltd

科研成果: 期刊稿件文章同行评审

3 引用 (Scopus)

摘要

To improve force feel simulation fidelity of the control loading system on the flight simulator based on force loop, the effect of inner loop tracking performance on the fidelity of force feel simulation is analyzed. A controlling strategy combining proportion with feedforward inverse model compensation is put forward following the structure invariance principle for restraining surplus force. On the premise of loop stability, this strategy can expand inner loop bandwidth. Simulation and hardware-in-the-loop experiment on the RT-LAB based rapid prototype control platform show that the proposed control strategy improves the inner loop tracking performance, thus significantly enhances the force feel simulation fidelity of control loading system.

源语言英语
页(从-至)38-44
页数7
期刊Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University
46
4
出版状态已出版 - 4月 2012
已对外发布

学术指纹

探究 'Inverse model control for inner loop of control loading system on flight simulator' 的科研主题。它们共同构成独一无二的学术指纹。

引用此