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Force tracking control of an electro-hydraulic control loading system on a flight simulator using inverse model control and a damping compensator

  • Jinsong Zhao
  • , Gang Shen*
  • , Weidong Zhu
  • , Chifu Yang
  • , Sunil K. Agrawal
  • *Corresponding author for this work
  • Yanshan University
  • China University of Mining and Technology
  • University of Maryland, Baltimore County
  • Columbia University

Research output: Contribution to journalArticlepeer-review

Abstract

The electro-hydraulic control loading system (EHCLS) of a flight simulator is mainly used to simulate the force feel of flying a real airplane. A double-loop model, including control and hydraulic mechanism of the EHCLS, is established and its force–displacement impedance is analysed to evaluate force tracking performances and its stability. An approximated feed-forward inverse model controller is designed using a zero phase error compensation method for expanding the frequency bandwidth of the inner loop because the identified force closed-loop model is a nonminimum phase system and its direct inverse model is unstable. Modelling error between the designed feed-forward inverse model and the actual plant is discussed and a damping compensator is presented to increase stability of the EHCLS. Theoretical analysis, simulation and experimental results show that the control methods presented are feasible and can effectively improve force feel fidelity and stability of the EHCLS.

Original languageEnglish
Pages (from-to)135-147
Number of pages13
JournalTransactions of the Institute of Measurement and Control
Volume40
Issue number1
DOIs
StatePublished - 1 Jan 2018

Keywords

  • Electro-hydraulic control loading system
  • feed-forward inverse model
  • force tracking control
  • force–displacement impedance
  • system identification

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