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弹箭与制导学报 >

2021 , Vol. 41 >Issue 5: 1 - 6

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.05.001

导弹纵向平面部分制导控制一体化设计方法

  • 安通 ,
  • 王建华 ,
  • 潘玉龙 ,
  • 陈海山
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  • 1 空军预警学院,武汉 430019
    2 战略支援部队航天工程大学,北京 101400

安通(1993—),男,吉林四平人,助教,硕士,研究方向:飞行器制导与控制.

收稿日期: 2021-06-20

  网络出版日期: 2025-05-30

基金资助

国家自然科学基金(61903379)

收起

Longitudinal Partial Integrated Guidance and Control Scheme for Missile

  • AN Tong ,
  • WANG Jianhua ,
  • PAN Yulong ,
  • CHEN Haishan
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  • 1 Air Force Early Warning Academy, Wuhan 430019, China
    2 Space Engineering University, Beijing 101400, China

Received date: 2021-06-20

  Online published: 2025-05-30

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摘要

针对导弹俯冲段纵向平面制导控制系统设计问题,提出了一种部分制导控制一体化设计方法。建立了一种基于导弹加速度分量的俯仰角速率解析模型。联立导弹-目标相对运动模型和俯仰角速率解析模型,利用滑模控制方法,并引入动态面控制中的低通滤波器思想,制导分系统直接生成俯仰角速率指令及其变化率。姿控分系统基于滑模控制方法实现对俯仰角速率指令的跟踪并解算俯仰舵偏角指令。仿真试验结果表明,该方法能够使导弹准确命中地面目标,并对参数偏差具有较好的鲁棒性。

关键词： 导弹俯冲段; 纵向平面; 部分制导控制一体化; 滑模控制

本文引用格式

安通 , 王建华 , 潘玉龙 , 陈海山 . 导弹纵向平面部分制导控制一体化设计方法[J]. 弹箭与制导学报, 2021 , 41(5) : 1 -6 . DOI: 10.15892/j.cnki.djzdxb.2021.05.001

Abstract

A longitudinal plane partial integrated guidance and control method for missile in dive phase is proposed in this paper. An analytical model of pitch rate is deduced based on the acceleration components of the missile. By combining the analytical model and the relative motion model between the missile and target, the command of pitch rate and its change rate are directly generated based on the sliding mode control approach and the low pass filter theory in the dynamic surface control (DSC) method. In the attitude control subsystem, the sliding mode control method is used to track the command of pitch rate and the command of pitchchannel fin deflection is obtained. The proposed partial integrated guidance and control design method has the advantages of loworder design model, simple design process and more convenient application in engineering. The effectiveness and robustness of the proposed design method are verified by simulation experiments.

Key words： missile in dive phase; longitudinal plane; partial integrated guidance and control; sliding mode control

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