[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2016 , Vol. 36 >Issue 3: 78 - 81

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2016.03.021

ROCKETS TECHNOLOGY

Research on Coupling Interaction between Rocket Stage Separation and Attitude Control

  • ZHAI Zhangming ,
  • ZHANG Jian ,
  • LIN Song ,
  • ZHOU Yilei ,
  • XU Mingzhao
Expand
  • 1 College of Aerospace Science and Engineering, National University of Defense Technolog, Changsha 410073, China
    2 Beijing Institute of Astronautical Systems Engineering, Beijing 100076, China

Received date: 2015-05-18

  Online published: 2025-05-30

Fold

Abstract

In order to analyze coupling interaction between stage separation and attitude control, the method for calculating coupling between separation and attitude control was proposed based on upper-stage nozzle's maximum swing angular velocity and real time control, and calculating model of coupling between stage separation and attitude control was established.According to calculation of stage separation of some certain rocket, the coupling calculating method based on upper-stage real-time control truly reveals stage separating process under upper-stage attitude control force, can provide precise reference for installing boundary design of rocket-borne equipment.

Key words： stage separation; attitude control; coupling influence

Cite this article

ZHAI Zhangming , ZHANG Jian , LIN Song , ZHOU Yilei , XU Mingzhao . Research on Coupling Interaction between Rocket Stage Separation and Attitude Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(3) : 78 -81 . DOI: 10.15892/j.cnki.djzdxb.2016.03.021

[an error occurred while processing this directive]

References

[1]
郭凤美, 余梦伦. 导弹分离设计技术研究[J]. 导弹与航天运载技术, 2014 (1): 5-10.
[2]
沙建科, 徐敏, 施雨阳. 导弹级间分离干扰动力学仿真研究[J]. 应用力学学报, 2014, 31(3): 364-369.
[3]
贾沛然, 陈克俊, 何力. 远程火箭弹道学[M]. 长沙: 国防科技大学出版社, 1993: 36-48.
[4]
孙平, 刘昆. 小型固体运载器一、二级分离动力学与仿真研究[J]. 国防科技大学学报, 2010, 32(2): 27-32.
[5]
杨涛, 王中伟, 张为华,等. 导弹级间分离特性的数学分析研究[J]. 弹箭与制导学报, 2007, 27(2): 80-82.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]