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MISSILES AND GUIDANCE TECHNOLOGY

Design and Simulation of Diving Guidance Law for Terminal Phase Trajectory of Glide-warhead

  • LIU Kaifeng ,
  • CHEN Ying ,
  • LIANG Liwei ,
  • MENG Haidong
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  • 1 The Second Artillery Engineering University, Xi'an 710025, China
    2 The Second Artillery Equipment Academy, Beijing 100085, China

Received date: 2013-06-01

  Online published: 2025-05-30

Abstract

Glide-warhead long flies in near space where aerodynamic environment is complicated, so the entry precision can not be guaranteed. In order to realize accurate attack and considering the demand for attack angle control, the motion equation of glide warhead at terminal phase was built in target coordinates, the dive guidance law based on expanded proportion guidance with terminal-velocity direction control was derived. Simulation results show that when parameters at the dive beginning point are reasonable, method in this paper performs efficiently to control the precision of attack angle.

Cite this article

LIU Kaifeng , CHEN Ying , LIANG Liwei , MENG Haidong . Design and Simulation of Diving Guidance Law for Terminal Phase Trajectory of Glide-warhead[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(3) : 25 -28 . DOI: 10.15892/j.cnki.djzdxb.2014.03.036

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References

[1]
吴鹏. 带末端攻击角度约束的制导方法研究[D]. 哈尔滨: 哈尔滨工业大学, 2009.
[2]
覃天陈, 万春, 邢晓岚. 一种带落角约束的精确导引方法[J]. 宇航学报, 2012, 33(5): 570-576.
[3]
陈海兵. 导弹跳跃段弹道规划与导引技术研究[D]. 长沙: 国防科技大学, 2006.
[4]
Bollino K P, Oppenheimer M W, Doman D D. Optimal guidance command generation and tracking for reusable launch vehicle reentry[C]// AIAA Guidance, Navigation, and Control Conference Proceedings. Keystone, Colorado, 2006:4614-4636.
[5]
Bollino K P. High-fidelity real-time trajectory optimization for reusable launch vehicles[D]. Monterey, California: Naval Postgraduate School, 2006.
[6]
周荻. 寻的导弹新型导引规律[M]. 北京: 国防工业出版社, 2002.
[7]
赵汉元. 飞行器再入动力学和制导[M]. 长沙: 国防科技大学出版社, 1997.
Outlines

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