导弹与制导技术

机载导弹传递对准匹配方案研究

  • 阮娟 ,
  • 杨栓虎 ,
  • 谭磊 ,
  • 赵军伟
展开
  • 中国兵器工业第203 研究所,西安 710065

阮娟(1981-),‚女,‚重庆人‚,硕士研究生‚,研究方向:惯性导航系统算法。

收稿日期: 2009-07-15

  网络出版日期: 2025-05-19

Study on Matching Schemes of Transfer Alignment for Airborne Missile

  • RUAN Juan ,
  • YANG Shuanhu ,
  • TAN Lei ,
  • ZHAO Junwei
Expand
  • No.203 Research Institute of China Ordnance Industries, Xi'an 710065, China

Received date: 2009-07-15

  Online published: 2025-05-19

摘要

传递对准是解决机载战术导弹在空中动基座条件下初始对准问题的有效方法。为有效估计机载战术导弹系统的姿态误差角,文中在基本匹配方案的基础上,详细研究了“角速率+比力”匹配和“速度+全姿态矩阵”匹配这两种传递对准的匹配方案,分别推导了其数学模型,并进行了数字仿真,最后对仿真的结果进行了比较、分析,结果表明该方法能够有效的估计姿态误差角,并能够在较短时间内以一定精度完成初始对准。

本文引用格式

阮娟 , 杨栓虎 , 谭磊 , 赵军伟 . 机载导弹传递对准匹配方案研究[J]. 弹箭与制导学报, 2010 , 30(1) : 43 -46 . DOI: 10.15892/j.cnki.djzdxb.2010.01.016

Abstract

Transfer alignment is the effective method of solving the problem of initial alignment for airborne tactical missile on moving base. Aiming at the airborne tactical missile system, on the basis of basic matching schemes, the “velocity+attitude matrix" matching and the “angular rate+specific force”matching schemes are entirely researched in this thesis, and their mathematic models are derived respectively. Then the simulations of them are made and the analysis of the simulation results is made. The result shows that the algorithm can effectively estimate the misalignment, and realize the transfer alignment with certain accuracy in short time.

参考文献

[1]
秦永元, 张洪钺, 汪叔华. 卡尔曼滤波与组合导航原理[M]. 西安: 西北工业大学出版社, 1998.
[2]
秦永元. 惯性导航[M]. 北京: 科学出版社, 2005.
[3]
朱绍箕. 姿态角传递对准原理研究[J]. 航天控制, 2000 (1): 9- 14.
[4]
陈璞, 冯培德. 一种快速传递对准改进方案的设计仿真[J]. 中国惯性技术学报, 2001, 9 (1): 16- 19.
[5]
方群, 丁滢颖, 袁建平. 机载导弹捷联惯导系统快速传递对准方法研究[J]. 飞行力学, 2001, 19 (4): 49- 53.
文章导航

/