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弹箭与制导学报 >

2013 , Vol. 33 >Issue 2: 19 - 22

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2013.02.037

导弹与制导技术

一种基于速度加姿态匹配传递对准的稳瞄稳向方法

  • 高伟伟 ,
  • 王广龙 ,
  • 高凤岐 ,
  • 高爽 ,
  • 乔中涛
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  • 1 解放军军械工程学院纳米技术与微系统实验室,石家庄 050003
    2 北京航空航天大学仪器科学与光电工程学院,北京 100191

高伟伟(1986-),男,山西临汾人,博士研究生,研究方向:微型测控系统。

收稿日期: 2012-06-22

  网络出版日期: 2025-05-26

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A Stable Targeting Method Based on Transfer Alignment of Speed and Attitude Matching

  • GAO Weiwei ,
  • WANG Guanglong ,
  • GAO Fengqi ,
  • GAO Shuang ,
  • QIAO Zhongtao
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  • 1 Laboratory of Nanotechnology and Microsystems, Ordnance Engineering College, Shijiazhuang 050003, China
    2 School of Instrumentation Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

Received date: 2012-06-22

  Online published: 2025-05-26

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摘要

针对战车稳瞄稳向系统中单一惯性测量组合(IMU)组建的姿态测量系统初始对准时间较长,测量精度随惯性器件漂移影响较大的问题,提出了基于速度加姿态匹配传递对准的稳瞄稳向方法。仿真结果表明,提出的新方法可在10s内实现光电设备IMU的初始对准,并且能准确估计出光电设备IMU计算平台失准角。将结果用于解算姿态角的补偿,可大大提高稳瞄稳向精度。

关键词： 稳瞄稳向; 传递对准; 速度加姿态匹配; 卡尔曼滤波

本文引用格式

高伟伟 , 王广龙 , 高凤岐 , 高爽 , 乔中涛 . 一种基于速度加姿态匹配传递对准的稳瞄稳向方法[J]. 弹箭与制导学报, 2013 , 33(2) : 19 -22 . DOI: 10.15892/j.cnki.djzdxb.2013.02.037

Abstract

A stable targeting method based on transfer alignment of speed and attitude matching was proposed to solve the problem of longer time alignment and a greater impact by the device drift for single inertial measurement unit (IMU) system. Simulation results show that the initial alignment can be implemented within 10 seconds for optoelectronic device's IMU, and platform misalignment angle can be estimated accurately. The results for the attitude angle compensation can greatly improve the accuracy of stable targeting.

Key words： stable targeting; transfer alignment; speed and attitude matching; Kalman filter

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参考文献

[1]
吴树平. 车载三轴稳定平台控制系统的研制[D]. 南京: 南京理工大学, 2007.
[2]
秦永元. 惯性导航[M]. 北京: 科学出版社, 2006.
[3]
宫晓琳, 房建成, 郭雷. SINS 快速传递对准建模与仿真[J]. 北京航空航天大学学报, 2008,34 (8): 865- 868.
[4]
Zhou Naixin, Wang Si, Deng Zhenglong. Comparison of threetransefrailgnment methods in marine missile SINS[C]// Proceed of the 25th Chinese Control Conference, 2006: 27 31.
[5]
LYOU J, LIM Y C. Transfer alignment error compensatordesign based on robust state estimation J. Transactions of-the Japan Society for Aeronautical and Space Sciences, 2009, 48(161): 143-151.
[6]
Lu Hao, Li Qunsheng, Wang Jnian. Research on transferail-gnment for helicopter-borne air-to-air missile[C]//IEEEInternational Conference on Intelligent Computing and Intel-ligent Systems, 2009: 113-116.
[7]
韩英宏, 陈万春. 新型快速传递对准方法研究[J]. 北京航空航天大学学报, 2012, 38(2): 149–152.
[8]
刘昇, 卢广山, 张晓鸿,等. 一种用于光电平台的传递对准方案设计.弹箭与制导学报,2011, 31(5): 47 – 50.
[9]
江云, 鲁浩, 位晓峰. 弹载捷联惯导系统空中传递对准精度评估.弹箭与制导学报,2012, 32(1): 21-26.
[10]
吴赛成. 应用 Kalman 滤波器提高机抖激光陀螺姿态测量系统瞬时精度的方法[J]. 仪器仪表学报,2011, 32(1):201-205.
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