• DocumentCode
    1032
  • Title

    Development of 3-D Modified Proportional Navigation Guidance Law against High-Speed Targets

  • Author

    Yu-Ping Lin ; Chun-Liang Lin ; Yun-Hao Li

  • Author_Institution
    Dept. of Electr. Eng., Nat. Chung Hsing Univ., Taichung, Taiwan
  • Volume
    49
  • Issue
    1
  • fYear
    2013
  • fDate
    Jan. 2013
  • Firstpage
    677
  • Lastpage
    687
  • Abstract
    The work presented here proposes a terminal guidance law against very high-speed targets. Proportional navigation guidance (PNG) is mostly effective for interceptors and targets with ideal dynamics and constant speeds during the collision course, however, it is nonrobust for the objects with nonconstant speeds, such as the interceptor equipped with thrust-vector-control (TVC). To resolve the problem the interceptor considered here is guided by a 3-dimensional (3-D) modified proportional navigation guidance (MPNG) law, which is developed to account for the interceptor´s axial acceleration. The guidance law is potentially applicable to interceptors with TVC to provide lateral accelerations.
  • Keywords
    missile control; missile guidance; 3D modified proportional navigation guidance law; MPNG; TVC; collision course; high-speed targets; interceptor axial acceleration; lateral accelerations; thrust vector control; Acceleration; Estimation; Missiles; Navigation; Neural networks; Trajectory; Vectors;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2013.6404133
  • Filename
    6404133