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Riding comfort analysis for two degrees model for MannedlLunarvVehicle

  • School of Mechatronics Engineering, Harbin Institute of Technology
  • Northeast Electric Power University

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

Abstract

Two degrees of freedom of suspension vibration model was established for deployable manned lunar vehicle. Transfer characteristics and amplitude frequency characteristics of vibration response including body acceleration, suspension dynamic deflection and wheel relative dynamic load were obtained. Then lunar surface random excitation model in time domain was established according to the filtered white noise method. In order to analyze the affection of four parameters that is vehicle natural frequency, damping ratio, stiffness ratio and the mass ratio of two-degree system of manned lunar vehicle on mean square value of the vibration response, numerical integral approach was used to calculate. These provide theoretical basis for suspension design and riding comfort analysis for manned lunar vehicle.

Original languageEnglish
Title of host publicationProceedings - 2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer, MEC 2013
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages3727-3730
Number of pages4
ISBN (Electronic)9781479925650
DOIs
StatePublished - 2013
Externally publishedYes
Event2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer, MEC 2013 - Shenyang, China
Duration: 20 Dec 201322 Dec 2013

Publication series

NameProceedings - 2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer, MEC 2013

Conference

Conference2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer, MEC 2013
Country/TerritoryChina
CityShenyang
Period20/12/1322/12/13

Keywords

  • Lunar random excitation
  • Manned lunar vehicle
  • Two degrees of freedon vibration system
  • Vibration response

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