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兵工学报 ›› 2006, Vol. 27 ›› Issue (2): 210-214.

• 论文 • 上一篇    下一篇

滑翔增程弹弹道特性分析

史金光1,王中原1,易文俊1,王枫2   

  1. 1.南京理工大学动カ工程学院,江苏南京210094; 2.中国船舶信息中心,北京100085
  • 收稿日期:2005-07-10 上线日期:2014-12-25
  • 通讯作者: 史金光

Analysis on the Ballistic Characteristics of Gliding Extended Range Projectile

SHI Jin-guang1, WANG Zhong-yuan1,YI Wen-jun1,WANG Feng2   

  1. 1. Power Engineering College, Nanjing University of Science and Technology, Nanjing 210094,Jiangsu, China; 2. China Ship Information Center, Beijing 100085, China
  • Received:2005-07-10 Online:2014-12-25
  • Contact: SHI Jin-guang

摘要: 滑翔增程是目前采用的较为有效的ー种弹箭增程技术。阐述了滑翔增程弹的飞行过 程,按其飞行过程将整个飞行弹道分为三段,并分别建立了各段的弹道模型;研究了整个飞行弹道 的特性,得到滑翔弹弹道与常规弹道在升弧段是一致的,在降弧段上则出现了较大的差別;在滚控 段采用“小步走”的控制策略,在滑控段采用开环控制。仿真计算表明:控制方法可行,计算结果与 设计思想一致,对滑翔增程弹的研制有一定的参考意义。滑翔增程是目前采用的较为有效的ー种弹箭增程技术。阐述了滑翔增程弹的飞行过 程,按其飞行过程将整个飞行弹道分为三段,并分别建立了各段的弹道模型;研究了整个飞行弹道 的特性,得到滑翔弹弹道与常规弹道在升弧段是一致的,在降弧段上则出现了较大的差別;在滚控 段采用“小步走”的控制策略,在滑控段采用开环控制。仿真计算表明:控制方法可行,计算结果与 设计思想一致,对滑翔增程弹的研制有一定的参考意义。

关键词: 流体力学 , 滑翔增程弾 , 飞行弹道 , 弾道特性

Abstract: The gliding flight of projectile is an efficient extended range technique. The flight process of gliding extended range projectile was explained. The whole flight trajectory was divided into three seg?ments and the ballistic model of every segment was established. The characteristics of the whole flight trajectory were studied. The result shows that the characteristics of climbing trajectory are same, while the characteristics of falling trajectory have obvious difference between gliding trajectory and or?dinary trajectory. The control strategy oi little step walk is adopted in rolling control segment and the open loop control is used in gliding control segment. The simulative results show that the control method is feasible and the conclusion is the same as the designed ideas. It can be used for the design of gliding extended range projectile in the future.

Key words: fluid mechanics , gliding extended range projectile , flight trajectory , characteristic of tra?jectory

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