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带落角约束与过载约束的寻初比例导引法

  • 王煜东 ,
  • 许承东 ,
  • 郑学恩 ,
  • 孙光辉 ,
  • 简益梅
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  • 北京理工大学宇航学院,北京 100081

王煜东(1994-),男,黑龙江牡丹江人,硕士研究生,研究方向:导航、制导与控制,飞行力学。

收稿日期: 2018-09-04

  网络出版日期: 2025-05-19

Initial Value Proportional Navigation with Impact Angle Constraint and Overload Constraint

  • WANG Yudong ,
  • XU Chengdong ,
  • ZHENG Xueen ,
  • SUN Guanghui ,
  • JIAN Yimei
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  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received date: 2018-09-04

  Online published: 2025-05-19

摘要

为实现反坦克导弹以较大落角攻击目标,提高导弹毁伤效率,结合落角约束与过载约束提出一种寻初比例导引法。首先建立落角预测模型,得出影响落角的参数;其次,结合导弹过载约束计算比例系数范围;最后,将落角预测模型与适当的比例系数相结合,得出满足战技指标的初值,实现导弹以较大落角命中目标。通过仿真结果表明该设计方法的正确性。

本文引用格式

王煜东 , 许承东 , 郑学恩 , 孙光辉 , 简益梅 . 带落角约束与过载约束的寻初比例导引法[J]. 弹箭与制导学报, 2019 , 39(4) : 29 -32 . DOI: 10.15892/j.cnki.djzdxb.2019.04.008

Abstract

In order to make the anti-tank missile attack the target at a larger impact angle, to improving missile damage efficiency, A new proportional navigation method combining angle constraint and overload constraint is proposed. First, setting up the prediction model of impact angle, obtain the factors that affect the impact angle: Then, the range of proportional coefficients is calculated with missile overload constraint: Finally, the prediction model is combined with appropriate proportional coefficient, obtain the initial value that satisfies the tactical index, and realize the missile hitting the target at a larger angle of attack. The simulation results show the correctness of the design method.

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