Volume 8 Issue 6
Dec.  2015
Turn off MathJax
Article Contents
ZHANG Yuan, WANG Zhi-qian, QIAO Yan-feng, LUO Jun, YIN Yan-he. Attitude measurement method research for missile launch[J]. Chinese Optics, 2015, 8(6): 997-1003. doi: 10.3788/CO.20150806.0997
Citation: ZHANG Yuan, WANG Zhi-qian, QIAO Yan-feng, LUO Jun, YIN Yan-he. Attitude measurement method research for missile launch[J]. Chinese Optics, 2015, 8(6): 997-1003. doi: 10.3788/CO.20150806.0997

Attitude measurement method research for missile launch

  • Received Date: 11 Jun 2015
  • Accepted Date: 16 Jul 2015
  • Publish Date: 25 Jan 2015
  • In order to solve the problem of attitude measurement in missile launch, tilted and plane collimation attitude measurement methods were presented by using high speed videos to calculate pitch and yaw angle for missile middle axes. The missile flight attitude measurement accuracy and applicability of these methods were analyzed by simulating representative near distance missile attitude measurement in flying-off process. The simulating result proves that it may acquire the measuring accuracy of less than 0.2° by these methods. Plane collimation method is more accuracy. Data processing method and mechanism configuration are relatively simple, and it is more advantage in proper application environment. Tilted collimation method is more universality and suitable for application. Analyzing result and method not only provide a new way to choose attitude measurement method, but also give a reference for measuring poses of other moving objects.

     

  • loading
  • [1]

    [2]

    [3]

    [4]

    [5]

    [6]

    [7]
    [8]

    [9]

    [10]
    [11]
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(4)  / Tables(5)

    Article views(4738) PDF downloads(653) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return