MISSILES AND GUIDANCE TECHNOLOGY

Terminal Adaptive Proportional Guidance Law for Guided Bomb

  • LI Jiongliang ,
  • LIU Huaixun ,
  • WANG Hang ,
  • XUE Xiaodong
Expand
  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2013-06-26

  Online published: 2025-05-30

Abstract

An adaptive proportional guidance law with angular constraint is developed for guided bomb, which meets the requirements of strap-down seeker and penetrating attack. Firstly, a gain variable proportional navigation guidance law was derived by classical proportional navigation and desired impact angle. Then, a closed-loop correction of guided coefficients was proposed for the sake of robustness enhance-ment of the guidance law. Simulation studies show that the presented guidance law can implement efficiently the angular constraint mission as well as preferable guidance precision.

Cite this article

LI Jiongliang , LIU Huaixun , WANG Hang , XUE Xiaodong . Terminal Adaptive Proportional Guidance Law for Guided Bomb[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(6) : 54 -56,67 . DOI: 10.15892/j.cnki.djzdxb.2014.06.014

References

[1]
蔡洪, 胡正东, 曹渊.具有终端角度约束的导引律综述[J].宇航学报, 2010, 31(2):315-323.
[2]
Ashwini R, Debasish G.Impact angle constrained interception of stationary targets[J].Journal of Guidance, Control and Dynamics, 2008, 31(6):1816-1821.
[3]
Kim B S, Kee J G, Han H S, et al.Homing guidance with terminal angular constraint against non-maneuvering and maneuvering tatgets, AIAA-97-3474[R].1997.
[4]
朱战霞, 王建培.一种攻击地面固定目标的变系数比例导引律[J].飞行力学, 2000, 18(4):46-49.
[5]
胡正东.天基对地打击武器轨道规划与制导技术研究[D].长沙:国防科学技术大学, 2009.
[6]
程国采.战术导弹导引方法[M].北京:国防工业出版社, 1996.
[7]
宋建梅, 张天桥.带末端落角约束的变结构导引律[J].弹道学报, 2001, 13(1):16-20.
[8]
林波, 孟秀云, 刘藻珍.有末端姿态角约束的机载布撒器导引律设计[J].弹箭与制导学报, 2005, 25(2):18-20.
[9]
梁卓.SINS/GPS制导炸弹变结构控制系统设计与研究[D].南京:南京理工大学, 2009.
Outlines

/