• DocumentCode
    434003
  • Title

    Angle constraint biased PNG

  • Author

    Jeong, S.K. ; Cho, S.J. ; Kim, E.G.

  • Author_Institution
    Guidance & Control Technol. Div., Agency for Defense Dev., Daejeon, South Korea
  • Volume
    3
  • fYear
    2004
  • fDate
    20-23 July 2004
  • Firstpage
    1849
  • Abstract
    In this paper, we propose a new biased proportional navigation guidance (BPNG) to get an arbitrary impact angle against stationary target. The closed form solution of this angle constraint BPNG (named ACBPNG) is derived. And with the solution, we can determine the exact bias for a required impact angle analytically. The solution is shown to be very useful to determine a proper homing guidance condition including initial engaging geometry and missile maneuverability. Because of its handy form to implement and easy solution to analyze, ACBPNG can be the most simple and effective scheme for homing guidance with impact angle constraint. ACBPNG could be applicable to either the system that uses seeker (both active and passive) or the system that does not use seeker.
  • Keywords
    missile guidance; proportional control; angle constraint biased proportional navigation guidance; homing guidance; initial engaging geometry; missile maneuverability; Acceleration; Closed-form solution; Computer vision; Cost function; Differential equations; Geometry; Leg; Missiles; Navigation; Underwater vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference, 2004. 5th Asian
  • Conference_Location
    Melbourne, Victoria, Australia
  • Print_ISBN
    0-7803-8873-9
  • Type

    conf

  • Filename
    1426914