[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 >

2015 , Vol. 35 >Issue 2: 114 - 117

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2015.02.029

BALLISIIC AND AIRDYNAMICS

Air-launching Missile Trajectory Numeric Simulation for Intercepting Boosting/Ascending Stage Ballistic Missile

  • GUO Xiaonan ,
  • LI Jixin
Expand
  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2014-08-28

  Online published: 2025-05-26

Fold

Abstract

For antimissile interception of the boosting/ascending tactical missile, guidance system model is built, and numeric simulation is carried out. First, 4 guidance laws, including proportion navigation guidance(PNG)、instantaneous miss-distance based forecasting optimal guidance law( OGL)、line of sight acceleration guidance(AAG) and target acceleration compensated proportion navigation(APN), are selected and applied to mid-course guidance to study the performance. According to the guidance performance analysis, 2 schemes are presented, and another two schemes are presented via exorbitant gravitation compensation (EGC). Finally, ‘OGL + APN( EGC)'is demonstrated to be the best one, which behaves better in attack zone, launching restrictions and guidance performance.

Key words： airborne antimissile missile; tactical ballistic missile; guidance law; EGC

Cite this article

GUO Xiaonan , LI Jixin . Air-launching Missile Trajectory Numeric Simulation for Intercepting Boosting/Ascending Stage Ballistic Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(2) : 114 -117 . DOI: 10.15892/j.cnki.djzdxb.2015.02.029

[an error occurred while processing this directive]

References

[1]
戴艳丽. 空中的舞台:浅谈美国空射反导导弹系统[J]. 兵器知识, 2008(2):47-49.
[2]
钱锟. 美国发展低成本空基反导武器系统[J]. 军事装备, 2009(1):50-54.
[3]
李记新, 郭晓楠, 李友年. 空射反导中末制导交接约束与末制导技术指标初步研究[J]. 科技信息, 2012 (2):396-397.
[4]
Zarchan P. Tactical and strategic missile guidance (5th Edition)[M]. Washington DC: American Institute of Aeronautics and Astronautics Inc, 2007.
[5]
谭湘霞, 于本水, 贝超. AAG导引律在拦截机动 TBM 中的应用[J]. 系统工程与电子技术, 2001 (4):64-66.
[6]
Hecht C. Homing guidance using angular acceleration of the line of sight, AIAA-91-2701-CP [R]. 1991: 856-869.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]