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BALLISIIC AND AIRDYNAMICS

Research on Trajectory Correction Simulation Device

  • HAO Yongping ,
  • ZHANG Jian ,
  • LI Xinfu ,
  • LI Xiang ,
  • ZHANG Jiayi
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  • 1 Research and Development Center of CAD/CAM, Shenyang ligong University, Shenyang 110159, China
    2 Military Representative Office in No. 724 Factory, Shenyang 110159, China

Received date: 2014-04-01

  Online published: 2025-05-26

Abstract

In order to achieve high-speed stability control of two-dimensional correction projectile, the spin-decelerating moment of a two-dimensional correct projectile with rubber and fin under different speed was studied by simulation experiment based on the principle of trajectory correction. The equipment motor damping to stir oil which oil box under spin-decelerating moment simulate spin-decelerating moment of the correction projectile. The spin torque calculated by FLUENT simulation software, the oil box simulation result was measured by strain gauge dynamometer, the of the motor and oil box were measured by hall speed sensor, and the test data was analyzed by MATLAB. The experiment result indicates that the designed equipment could meet the test requirement of correction projectile control.

Cite this article

HAO Yongping , ZHANG Jian , LI Xinfu , LI Xiang , ZHANG Jiayi . Research on Trajectory Correction Simulation Device[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(1) : 91 -94 . DOI: 10.15892/j.cnki.djzdxb.2015.01.023

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Outlines

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