[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
导弹与制导技术

鸭舵式修正机构修正能力的分析与研究

  • 邵伟平 ,
  • 汪亚利 ,
  • 郝永平 ,
  • 郝启 ,
  • 许巍
展开
  • 沈阳理工大学机械工程学院,沈阳 110159

邵伟平(1968-),女,重庆合川人,教授,博士,研究方向:机械设计及理论。

收稿日期: 2016-03-31

  网络出版日期: 2025-05-28

The Analysis and Study of Correction Ability of Canard CorrectionMechanism

  • SHAO Weiping ,
  • WANG Yali ,
  • HAO Yongping ,
  • HAO Qi ,
  • XU Wei
Expand
  • Institute of Mechanical Engineering, Shenyang Ligong University, Shenyang 110159, China

Received date: 2016-03-31

  Online published: 2025-05-28

摘要

为了研究鸭舵式修正机构的修正能力,建立了不同舵高和不同舵偏角的二维弹道修正弹丸三维模型,采用了流体动力学和运动学的联合仿真,重点分析了弹丸的升阻比气动特性、舵片减旋和姿态控制,得出修正效果。得出结论:50mm高的舵片对射程的修正效果最好,55mm高的舵片对偏航的修正效果最好;舵偏角越大的舵片对射程和射高的修正效果越好,但对航偏的修正效果不佳,而偏角较小的舵片对航偏的修正效果较好。

本文引用格式

邵伟平 , 汪亚利 , 郝永平 , 郝启 , 许巍 . 鸭舵式修正机构修正能力的分析与研究[J]. 弹箭与制导学报, 2017 , 37(3) : 23 -25 . DOI: 10.15892/j.cnki.djzdxb.2017.03.007

Abstract

In order to study the correction ability of the canard correction mechanism, establishing 3D models of two-dimensional trajectory correction artillery with different heights and different rudder angles and conducting fluid dynamics and kinematics simulation. Using hydrodynamics and kinematics co-simulation, analyzing aerodynamic characteristics, anti-rotation and position-control of rudder specially. Drawing a conclusion: the rudder with 50 mm height makes the correction-result of range best, the rudder with 55 mm height makes the correction-result of deviation best; the bigger rudder angle, the better the correction-result of rang and cross, but the correction-result of deviation is not good and the smaller rudder angle makes the correction-result of deviation better.

[an error occurred while processing this directive]

参考文献

[1]
张通, 赵晓利. 弹道修正弹及其关键技术分析[J]. 飞航导弹, 2014(5):38-42.
[2]
郝永平, 郭煜洋, 张嘉易. 二维弹道修正弹修正机构气动布局研究[J]. 弹箭与制导学报, 2013 33(6):121-124.
[3]
杨慧娟, 霍鹏飞, 黄铮. 弹道修正弹修正执行机构综述[J]. 四川兵工学报, 2011, 32(1):7-9.
[4]
邵盼, 郭煜洋, 郝永平,等. 鸭舵修正机构舵偏角选择方法. 弹箭与制导学报, 2014, 34(6):33-36.
[5]
吴萍, 陈少松, 杨晋伟,等. 旋转控制固定鸭舵二维弹道修正弹气动特性[J]. 弹道学报, 2014,26(3): 7-9.
[6]
徐明友. 火箭外弹道学[M]. 哈尔滨: 哈尔滨工业大学出版社, 2004:10-15.
[7]
ROPERT J G, SIEWART J. 2-D projectile trajectory corrector:6502786 B2P[P]. 2003-01-07.
[8]
HAMEL Nicolas, GAGNON Eric. CFD and parametric study on a 155 mm artillery shell equipped with a roll-de-coupled course correction fuze:DRDC-VALCARTIER-SL-2011-297 [R].[S.1.:s.n.], 2011.
[9]
GLEISSL R, DESLANDES R M, BAETEN A. Assessment of missile plume impact characteristics:AIAA 2007-675[R].[S.l.:s.n.], 2007.
[10]
SMITH Douglas L. Fractional roll control apparatus for a spinning projectile:7412930[P]. 2008-08-19.
文章导航

/

[an error occurred while processing this directive]