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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 1: 131 - 132,138

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.01.049

ROCKETS TECHNOLOGY

The Optimization of Thrust Vector Control Device for Load Moment

  • HUANG Shuaijun ,
  • ZHANG Hongfei ,
  • YANG Xiaoguang ,
  • LIU Xianwei ,
  • LIN Xueshu
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  • 1 China Airborne Missile Academy, Henan Luoyang 471009, China
    2 Military Representive Office of Army Aviation in Beijing Area, Beijing 100176, China

Received date: 2011-05-03

  Online published: 2025-05-29

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Abstract

To solve the problem of high load moment, the mathematic model and systematic analysis of thrust vector control were founded. Two different methods including extra lubrication as well as change of rolling friction were used for descending the affected factor in friction. The experiment shows that the peak value of extra lubrication descends 56% and that of change of rolling friction is even 66.4% lower than the un-optimized. The profile of load moment is smooth. All the experiment results illustrate the validity of optimization measures.

Key words： missile; thrust vector control; load moment; optimization

Cite this article

HUANG Shuaijun , ZHANG Hongfei , YANG Xiaoguang , LIU Xianwei , LIN Xueshu . The Optimization of Thrust Vector Control Device for Load Moment[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(1) : 131 -132,138 . DOI: 10.15892/j.cnki.djzdxb.2012.01.049

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References

[1]
刘代军, 崔颢. 推力矢量控制技术与第四代空空导弹[J]. 航空兵器, 2005 (5): 28- 31.
[2]
刘代军. 气动力/推力矢量复合控制空空导弹关键技术研究[D]. 西安: 西北工业大学, 2000.
[3]
温诗铸, 黄平. 摩擦学原理[M]. 3版. 北京: 清华大学出版社, 2008.
[4]
成大先. 机械设计手册[M]. 4版. 北京: 化学工业出版社, 2004.
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