• DocumentCode
    2900809
  • Title

    Analysis of PPN guidance law - A new approach

  • Author

    Feng Tyan

  • Author_Institution
    Dept. of Aerosp. Eng., TamKang Univ., Taipei, Taiwan
  • fYear
    2013
  • fDate
    17-19 June 2013
  • Firstpage
    1030
  • Lastpage
    1035
  • Abstract
    In this paper, we analyze the capture region, time to go, cost and impact angle of a classical pure proportional navigation guidance law. Unlike the traditional ways adopted by most of the researchers, the angle of relative velocity is used in this work as the independent variable instead. Through this approach an analytical solution of cost and impact angle can be obtained. Furthermore, the time to go for a stationary target is also derived.
  • Keywords
    missile guidance; PPN guidance law; capture region; missile guidance; pure proportional navigation guidance law; stationary target; Aerodynamics; Equations; Missiles; Navigation; Trajectory; Upper bound; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2013
  • Conference_Location
    Washington, DC
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4799-0177-7
  • Type

    conf

  • DOI
    10.1109/ACC.2013.6579972
  • Filename
    6579972
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2900809