[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]
MIISSILES AND GUIDANCE TECHNOLOGY

Research on Ship-to-air Missile Miss Distance against an Anti-ship Missile of Snake Maneuver

  • DOU Jihua ,
  • LU Yonghong ,
  • YANG Xingbao
Expand
  • Dalian Navy Academy, Liaoning Dalian 116018, China

Received date: 2009-10-11

  Online published: 2025-05-28

Abstract

For analyzing effect of some factors on the ship-to-air missile miss distance against anti-ship missile of snake maneuver, the 3-D movement simulation models for both missiles were built. The simulation results prove that the main reasons affecting miss distance are radius, section distance, target altitude, course-shortcut, radome slope, turning rate and control system time constant, control system order. The achievements of this paper are believed to benefit the analysis of fighting efficiency and combat employment.

Cite this article

DOU Jihua , LU Yonghong , YANG Xingbao . Research on Ship-to-air Missile Miss Distance against an Anti-ship Missile of Snake Maneuver[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(4) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2010.04.034

[an error occurred while processing this directive]

References

[1]
Zarchan P. Proportional navigation and weaving targets[J]. Journal of Guidance, Control, and Dynamics, 1995, 18 (3): 969- 974.
[2]
顾文锦, 赵红超, 王凤莲. 反舰导弹末端蛇行机动的控制信号射击[J]. 航天控制, 2005, 23 (1): 58- 61.
[3]
张卫锋, 张中南, 熊小龙. 舰空导弹拦截“蛇行机动”反舰导弹的仿真研究[J]. 战术导弹技术, 2007 (3): 82- 85.
[4]
严建钢. 反舰导弹“蛇行机动”与作战能力研究[J]. 海军航空工程学院学报, 2000, 15 (4): 445- 447.
[5]
Imado F, Uehara S. High-g barrel roll maneuvers against proportional navigation from optimal control viewpoint[J]. Journal of Guidance, Control, and Dynamics, 1998, 21 (6): 876- 881.
Outlines

/

[an error occurred while processing this directive]