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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 5: 48 - 50

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.05.029

MISSILES AND GUIDANCE TECHNOLOGY

Motion Model of Gas Actuated Roller in Missile Wing Unfolding Mechanism

  • YAO Xiaoning ,
  • TU Xiaochang ,
  • HUANG Yunluan ,
  • JI Xiaogang
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  • Shaanxi Applied Physics and Chemistry Research Institute, Xi'an 710061, Chian

Received date: 2012-06-23

  Online published: 2025-05-29

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Abstract

In view of the application reseach of gas actuated roller in missile wing unfolding mechanism, a motion model was proposed by u-sing mathematical inductive fitting method and model analysing method. This model can be used in production design of gas actuated roller in missile wing unfolding mechanism for providing theoretical basis.

Key words： missile wing unfolding mechanism; gas actuated roller; piston; equation of motion; analysis and research

Cite this article

YAO Xiaoning , TU Xiaochang , HUANG Yunluan , JI Xiaogang . Motion Model of Gas Actuated Roller in Missile Wing Unfolding Mechanism[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(5) : 48 -50 . DOI: 10.15892/j.cnki.djzdxb.2012.05.029

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