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弹道与气动力技术

远程制导炮弹有控段弹道优化设计

  • 郑友胜 ,
  • 杨剑影 ,
  • 汤蒂莲 ,
  • 周海迎
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  • 1 北京大学,北京 100871
    2 洪都航空工业集团,南昌 330024
    3 东华理工大学土木与环境工程学院,江西抚州 344000
    4 东华理工大学长江学院,南昌 330013

郑友胜(1980-),男,安徽东至人,博士,研究方向:飞行力学建模与飞行控制器的设计。

收稿日期: 2009-12-16

  网络出版日期: 2025-05-28

基金资助

教育部重点项目(J07JJ)

Optimization Design of Control Phase Trajectory About Extended Range Guided Projectile

  • ZHENG Yousheng ,
  • YANG Jianying ,
  • TANG Dilian ,
  • ZHOU Haiying
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  • 1 Peking University,Beijing 100871,China
    2 Hongdu Aviation Industry Group Ltd, Nanchang 330024,China
    3 College of Civil and Environmental Engineering,East China Institute of Technology,Jiangxi Fuzhou 344000,China
    4 Yangzi College,East China Institute of Technology,Nanchang 330013,China

Received date: 2009-12-16

  Online published: 2025-05-28

摘要

文中对某远程制导炮弹进行弹道优化设计,为了能够很好的控制炮弹飞行,将有控段分成滑翔段、增速段和过重补偿段进行研究。根据制导炮弹滑翔段的特点,建立了制导炮弹的弹道模型,然后根据所建立的模型,给出了一种基于滑翔段的弹道优化算法。该算法避免了繁杂的梯度计算,相对于序列二次规划法其计算量大大降低了。仿真结果表明,所设计的弹道方案不仅增大了弹丸的射程,也提高了弹丸的命中概率。

本文引用格式

郑友胜 , 杨剑影 , 汤蒂莲 , 周海迎 . 远程制导炮弹有控段弹道优化设计[J]. 弹箭与制导学报, 2010 , 30(6) : 155 -158 . DOI: 10.15892/j.cnki.djzdxb.2010.06.024

Abstract

Some extended range guided projectile trajectory is best designed by this paper, In order to can control projectile flying path, the control phase was separate into sliding phase, accelerating phase and compensation over gravity phase go on research. According to the characteristic of guided projectile sliding phase, the exterior trajectory model was established, then give out a trajectory optimization arithmetic about gliding phase. The arithmetic need not go multifarious grads calculation, the calculation time much lesser to sequence quadratic programming algorithm. The simulation result indicate that the scheme of trajectory not only improve the projectile range, but also advance the projectile hit probability.

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