Development of computer controlled loading system of helicopter manipulating booster

  • Zhiqing Sheng*
  • , Yunhua Li
  • *Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Addressing on the requests to measure the working characteristics of helicopter manipulate booster under high frequency aerodynamic load, this paper has developed a hydraulic loading system to simulate the load with large static load and sine dynamic load. The structure and operation principle of load simulator are described and analyzed, and a method to restrain the surplus force is put forward. Signal conditioning circuits of physical signals and power drive circuits of the hydra-electronic servo valves are designed to satisfy high frequency load. The computer control system of the load simulator is developed by using the real-time operating system based on Windows XP and RTX, and the control software programmed by Microsoft Visual C language, and the control processes are also given. The experimental results show that the developed load simulator performance indexes can meet the designed requirements.

Original languageEnglish
Title of host publicationProceedings of 2011 International Conference on Fluid Power and Mechatronics, FPM 2011
Pages715-720
Number of pages6
DOIs
StatePublished - 2011
Event2011 International Conference on Fluid Power and Mechatronics, FPM 2011 - Beijing, China
Duration: 17 Aug 201120 Aug 2011

Publication series

NameProceedings of 2011 International Conference on Fluid Power and Mechatronics, FPM 2011

Conference

Conference2011 International Conference on Fluid Power and Mechatronics, FPM 2011
Country/TerritoryChina
CityBeijing
Period17/08/1120/08/11

Keywords

  • Load simulator
  • RTX
  • Real-time control
  • Software development

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