激光驾束制导仪制导过程中信息场参数测量方法研究

于洵, 宇文乾, 姜旭, 李博, 刘宝元

于洵, 宇文乾, 姜旭, 李博, 刘宝元. 激光驾束制导仪制导过程中信息场参数测量方法研究[J]. 应用光学, 2011, 32(1): 75-79.
引用本文: 于洵, 宇文乾, 姜旭, 李博, 刘宝元. 激光驾束制导仪制导过程中信息场参数测量方法研究[J]. 应用光学, 2011, 32(1): 75-79.
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YU Xun, YUWEN -Qian, JIANG Xu, LI Bo, LIU Bao-yuan. AInformation filed parameters measurement inlaser beam riding guidance[J]. Journal of Applied Optics, 2011, 32(1): 75-79.
Citation: YU Xun, YUWEN -Qian, JIANG Xu, LI Bo, LIU Bao-yuan. AInformation filed parameters measurement inlaser beam riding guidance[J]. Journal of Applied Optics, 2011, 32(1): 75-79.
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激光驾束制导仪制导过程中信息场参数测量方法研究

  • 1.

    西安工业大学光电工程学院,陕西西安710032;

  • 2.

    西安应用光学研究所,陕西西安710065

详细信息
    通讯作者:

    于洵(1964-)，男，陕西西安人，硕士，高级工程师，硕士生导师，主要从事光电测试技术和光电信息系统与技术的研究与教学工作。

  • 中图分类号: TN249;TJ765.4

AInformation filed parameters measurement inlaser beam riding guidance

  • 1.

    School of Optoelectronic Engineering,Xi’an Technological University,Xi’an 710032,China;

  • 2.

    Xi’an Institute of Applied Optics,Xi’an 710065,China

摘要

    摘要
  • 摘要: 传统信息场参数测量方式只能测量制导始端和末端的信息场参数，无法测量制导过程中信息场参数,不能全面对制导过程中制导仪性能进行准确评估。为解决传统测量方式存在的问题，采用大口径变焦平行光管与精密光栅尺测控技术实现信息场的制导距离测量，通过专用光纤靶标与PIN阵列探测器接收信息场，根据已建立的数学模型对信号处理，从而得到制导过程中信息场参数。实践验证测量系统的指令测试精度达到0.01单位指令，照度测量精度为5%，光轴一致性精度为4.89。
    Abstract: Since traditional measurement can only measure the parameters of information field at the beginning stage and terminal stage，complete information field parameters during whole guiding process is not available and the missile guidance performance can not be accurately evaluated. To solve this problem, the guiding distance measurement of the information field was realized by using large aperture zooming collimator and precision grating ruler. The information field was detected by optical fiber target and PIN detector array. The signal was processed according to the existing mathematical model and the information field parameters during guiding process were obtained. Results indicate that the test accuracy of command test reaches 0.01 unit command, the accuracy of irradiance measurement reaches 5% and the bore-sight accuracy reaches to 4.89.
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  • ［1］李云霞.激光驾束制导仪性能测试系统研究［J］.红外与激光工程,2001,30(6):474-477.LI Yun-xia.Research on performance testing solutionof laser beam riding guider［J］.Infrared and Laser Engineering, 2001,30(6):474-477. (in Chinese with an English abstract)［2］王狂飙.激光制导武器的现状、关键技术与发展［J］.红外与激光工程,2007,36(5):651-654.WANG Kuang-biao.key technology and develo-pment of laser guided weapon［J］. Infrared and Laser Engineering,2007,36(5):651-654. (in Chinese with an English abstract)［3］WENG Yan,WANG Zhen-gjie, ZHANG Tian-qiao. Optimum design of the control system for a laser beam riding guidance anti-tank missle［J］. Journal of BeiJing Institute of Technology,2000,9(2):160-165.［4］徐飞飞.激光驾束制导的辐射接收技术［D］.长春:长春理工大学,2008.XU Fei-fei.Developent of radiant receiving technology on laser beam-riding guidance［D］.Changchun:Changchun University of Science and Technology,2008. (in Chinese)［5］李明松,黄柯彦,徐容甫.激光驾束制导仪空间光场性能测量系统［J］.兵工学报,2001,22(4):508-511.LI Ming-song,HUANG Ke-yan,XU Rong-fu. A mesuring system for the spatial lsaer wave field of a laser beam missil guidance system［J］. Acta  ArmamentarII,2001,22(4):508-511. (in Chinese with an English abstract)［6］周木春,陈延如,赵琦.激光驾束制导偏振编码器设计参数［J］.红外与激光工程,2008,37(6):1025-1028.ZHOU Mu-chun, CHEN Yan-ru; ZHAO Qi. Design parameters of polarization encoder in laser beam riding guidance［J］.Infrared and Laser Engineering,2008,37(6):1025-1028. (in Chinese with an English abstract)［7］彭利军,杨坤涛,章秀华.红外制导激光光束性能测试方法的研究［J］.激光技术,2007,31(4):423-426.PENG Li-jun,YANG Kun-tao,ZHANG Xiu-hua. Performance measurement of the infrared guided laser beam［J］.Laser Technology,2007,31(4):423-426. (in Chinese with an English abstract)［8］江月松,李小路，陈海亭.一种驾束式激光制导仪的基本组成和制导过程［J］.光学技术,2005,31(3):354-356.JIANG Yue-song,LI Xiao-lu,CHENG Hai-ting. Studies of basic component part and guided process for a certain modal of surmounted laser-beam guided instrument［J］. Optical Technique, 2005,31(3):354-356.(in Chinese with an English abstract)
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  • 刊出日期:  2011-01-14

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