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Design and implementation of a compound load simulator

  • Chunwei Yang*
  • , Jianhui Dai
  • , Shusheng Bi
  • , Guanghua Zong
  • *Corresponding author for this work
  • Beihang University
  • China Aviation Industry Corporation

Research output: Contribution to journalArticlepeer-review

Abstract

With the devised load decoupling component, a compound load simulator used to compositely simulate loads like bending moment, axial force and torque was designed based on the principle of a kind of zero-torsion parallel mechanism. The core of its control system was a programmable multi-axis motion controller (PMAC). By load feedbacks from force or torque sensors, the system can realize the load simulation of torque, bending moment or axial force in the form of sine wave with the control method of triple close-loops including force, position and current. Meanwhile, it can effectively avoid the influences to the sensors' signal from system electromagnetic interference. Some field tests of compound load simulation were made to validate the correctness of the mechanical design and the control method.

Original languageEnglish
Pages (from-to)1660-1664
Number of pages5
JournalBeijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
Volume39
Issue number12
StatePublished - Dec 2013

Keywords

  • Load decoupling
  • Load simulator
  • Parallel mechanism
  • PMAC(programmable multi-axis motion controller)

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