• DocumentCode
    3612957
  • Title

    Analysis of 3D PPN guidance laws for nonmaneuvering target

  • Author

    Feng Tyan

  • Author_Institution
    Dept. of Aerosp. Eng., TamKang Univ., Taipei, Taiwan
  • Volume
    51
  • Issue
    4
  • fYear
    2015
  • Firstpage
    2932
  • Lastpage
    2943
  • Abstract
    Unlike the traditional ways adopted by most of the researchers, the rotating angle of relative velocity is adopted in this work as the independent variable to analyze the analytical solution of impact angle, capture region (with or without finite line of sight (LOS) turn rate constraint), range to go, time to go, and a defined fuel cost of a traditional pure proportional navigation (PPN) guidance law for both nonmaneuvering moving, and stationary targets.
  • Keywords
    marine navigation; missile guidance; 3D PPN guidance law analysis; LOS turn rate constraint; line of sight turn rate constraint; nonmaneuvering target; pure proportional navigation; Acceleration; Aerodynamics; Angular velocity; Cities and towns; Missiles; Navigation; Three-dimensional displays;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2015.140676
  • Filename
    7376228
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3612957