导弹与制导技术

基于脱靶量预测的脉冲末修迫弹控制方法研究

  • 曹小兵 ,
  • 徐伊岑 ,
  • 常思江 ,
  • 齐斌
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  • 1 无锡职业技术学院控制技术学院, 江苏 无锡 214121
    2 无锡商业职业技术学院机电技术学院, 江苏 无锡 214153
    3 南京理工大学能源与动力工程学院, 南京 210094

曹小兵(1982-), 男, 江苏海安人, 讲师, 博士, 研究方向: 导航、制导与控制。

收稿日期: 2015-06-06

  网络出版日期: 2025-05-23

基金资助

中国博士后科学基金(2013M541676); 江苏省高等职业院校高级访问工程师计划资助项目(2014FG102); 江苏省高校“青蓝工程”基金资助

Research on Control Method for Terminal Correction Mortar Projectiles Subjected to Lateral Impulses Based on Miss Distance Prediction

  • CAO Xiaobing ,
  • XU Yicen ,
  • CHANG Sijiang ,
  • QI Bin
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  • 1 Control Technology Institute, Wuxi Institute of Technology, Jiangsu Wuxi 214121, China
    2 School of Mechatronical Technology, Wuxi Vocational Institute of Commerce, Jiangsu Wuxi 214153, China
    3 School of Energy and Power Engineering, NUST, Nanjing 210094, China

Received date: 2015-06-06

  Online published: 2025-05-23

摘要

针对脉冲末修迫弹的控制问题,提出了一种基于脱靶量预测的控制方法。分析了脉冲控制力与控制力矩,推导了有控六自由度运动方程组;利用捷联激光导引头测得的弹目偏差角及其方位信息,建立了脱靶量预测模型;在此基础上设计了脉冲工作模式,给出了脉冲作用个数与启控方位的确定方法。算例仿真结果表明,利用所提出的控制方法能够将圆概率误差减少约80%,有控弹道落点平均脱靶量为7.85m,证明该方法能够有效修正偏差,提高落点精度。

本文引用格式

曹小兵 , 徐伊岑 , 常思江 , 齐斌 . 基于脱靶量预测的脉冲末修迫弹控制方法研究[J]. 弹箭与制导学报, 2017 , 37(2) : 23 -26,31 . DOI: 10.15892/j.cnki.djzdxb.2017.02.006

Abstract

In view of the control problem of terminal correction mortar projectiles subjected to lateral impulses, a control method based on miss distance prediction was proposed. The impulse control force and control torque were analyzed, and the controlled 6-degree-of-freedom motion equations were deduced. By using the deviation angle and its azimuth information between projectile and target measured by strapdown laser seeker, a miss distance prediction model was established. On this basis, the thruster working mode was designed, also, the methods of determining the number of thrusters needed and the direction of starting control were given. Simulation results indicated that the circular error probable (CEP) was reduced by 80%, and the mean miss distance of the controlled impact points was 7.85 m. It proved that the proposed control method could correct the trajectory deflections effectively and thus improve the hit precision.

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