共形整流罩技术研究
DOI:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:


Research on conformal fairing technology
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    由于共形光学技术对红外制导导弹的空气动力学性能提高明显,近年来对该领域研究的投入不断加大,文章通过对比安装有共形整流罩导弹与传统导弹的作战性能,说明了共形光学技术在提高导弹机动性和隐身性方面的优势,论述了共形光学研究领域的难点问题,详细介绍了固定校正器、反向旋转位相板、可变形性反射镜等几种设计方案,用于消除共形整流罩随扫描视场变化的像差,并对各方案的优点与不足进行了讨论,简单介绍了共形光学零件加工与检测技术,最后对共形光学的未来进行了展望。

    Abstract:

    Because the conformal optical technology can obviously improve the aerodynamic performance of the infrared guidance missile,it has been studied deeply in recent years.By comparing the performance of the missiles with conformal fairing and conventional missiles,the advantages of the conformal optical technology are demonstrated in the maneuverability and stealth of the missile.The difficult problems of conformal optical field are discussed.For removing the aberration of conformal fairing with the change of scanning field,several design schemes are introduced in detail,including fixed corrector,counter-rotating phase plate,deformable mirror and so on.The advantages and the disadvantages of each scheme are discussed,and the processing and test of the conformal optical parts are introduced briefly.Finally,it is outlooked for the future of the conformal optical technology.

    参考文献
    相似文献
    引证文献
引用本文

李庆波,张健.共形整流罩技术研究[J].激光与红外,2014,44(8):837~840
LI Qing-bo, ZHANG Jian. Research on conformal fairing technology[J]. LASER & INFRARED,2014,44(8):837~840

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2014-08-27
  • 出版日期: