MISSILES AND GUIDANCE TECHNOLOGY

Study of Super Low Level High Parabolic Trajectory Design and Simulation of Ground-to-air Missile Weapon System

  • YANG Xuanchun ,
  • SUN Liang ,
  • ZHU Shiqing
Expand
  • 1 No.95948 Unit, Lanzhou 732750, China
    2 The 8th Institute of Shanghai Academy of Spaceflight Technology, Shanghai 200233,China

Received date: 2009-04-03

  Online published: 2025-05-28

Abstract

By analyzing the mirror interference principle and builds the mathematical model, and analyzes the relation between grazing angle and earth reflective factor, establishing the Brewster angle. Herein, we design the super low level high-parabolic trajectory and the discrimination criterion of mirror interference, and the control instruction gray prediction with mirror interference. The simulation and actual flight test results show that the super low level high-parabolic trajectory can avoid the mirror interference when it is close to or reach the Brewster angle at the initial stage of trajectory, and the mirror interference will be suppressed and consequently the expand the short extent of killing zone at the end of trajectory.

Cite this article

YANG Xuanchun , SUN Liang , ZHU Shiqing . Study of Super Low Level High Parabolic Trajectory Design and Simulation of Ground-to-air Missile Weapon System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(3) : 47 -51,54 . DOI: 10.15892/j.cnki.djzdxb.2010.03.035

References

[1]
梁棠文. 导弹技术词典[M]. 北京: 中国宇航出版社, 1991.
[2]
黄培康. 雷达目标特征信号[M]. 北京: 宇航出版社, 1993.
[3]
方挥煜. 防空导弹武器系统仿真[M]. 北京: 宇航出版社, 1995.
[4]
杨榜林, 岳全发. 军事装备试验学[M]. 北京: 国防工业出版社, 2002.
[5]
邓聚龙. 灰预测与灰决策[M]. 武汉: 华中科技大学出版社, 2005.
Outlines

/