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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

Research output: Contribution to journalArticlepeer-review

3 Scopus citations

Abstract

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.

Original languageEnglish
Pages (from-to)38-44
Number of pages7
JournalHsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University
Volume46
Issue number4
StatePublished - Apr 2012
Externally publishedYes

Keywords

  • Control loading system
  • Electro-hydraulic servo
  • Flight simulation
  • Inverse model
  • Semi-physical simulation
  • System identification

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