导弹与制导技术

制导炸弹自适应比例末制导律研究

  • 李炯良 ,
  • 刘怀勋 ,
  • 王航 ,
  • 薛晓东
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  • 中国空空导弹研究院,河南洛阳 471009

李炯良(1988-),男,甘肃白银人,硕士研究生,研究方向:飞行器制导系统仿真。

收稿日期: 2013-06-26

  网络出版日期: 2025-05-30

Terminal Adaptive Proportional Guidance Law for Guided Bomb

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

Received date: 2013-06-26

  Online published: 2025-05-30

摘要

针对制导炸弹采用捷联导引头和进行侵彻型攻击的技术要求,设计了一种具有终端角度约束的自适应比例导引律。基于经典比例导引关系,首先以期望落角为性能指标推导出变系数导引律,然后利用反馈的误差信息对导引系数进行自适应闭环校正,以增强导引律的鲁棒性。仿真结果表明,所设计的制导律具有较高的制导精度,并且满足落角约束要求。

本文引用格式

李炯良 , 刘怀勋 , 王航 , 薛晓东 . 制导炸弹自适应比例末制导律研究[J]. 弹箭与制导学报, 2014 , 34(6) : 54 -56,67 . DOI: 10.15892/j.cnki.djzdxb.2014.06.014

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.

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