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Design and simulation of elastic guiding mechanism for missile

  • Harbin Institute of Technology

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

Abstract

This study designs a new type of elastic separation guiding mechanism made up of the elastic rod and the steel ball. The mechanism can be used into the long stroke separation of missile and take full advantage of the elastic rod's damping effect to reduce the relative deflection and collision probability of the separation bodies. A mathematical model regarding the guiding mechanism and the separation process has been established in this paper to detect the influence of the stiffness coefficient and the preload force of the guiding mechanism having on the separation process. The simulation results demonstrate that both the stiffness coefficient and the preload force are very important for missile separation, and then we further obtain their optimal values in a certain stage separation process.

Original languageEnglish
Title of host publicationProceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages4005-4009
Number of pages5
ISBN (Electronic)9781479970179
DOIs
StatePublished - 17 Jul 2015
Event27th Chinese Control and Decision Conference, CCDC 2015 - Qingdao, China
Duration: 23 May 201525 May 2015

Publication series

NameProceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015

Conference

Conference27th Chinese Control and Decision Conference, CCDC 2015
Country/TerritoryChina
CityQingdao
Period23/05/1525/05/15

Keywords

  • Elastic guide
  • Long stroke separation
  • Simulation

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