• DocumentCode
    696148
  • Title

    Capturability of a simple guidance law with angular acceleration input

  • Author

    Urakubo, Takateru ; Kanade, Takeo

  • Author_Institution
    Dept. of Comput. Sci. & Syst. Eng., Kobe Univ., Kobe, Japan
  • fYear
    2009
  • fDate
    23-26 Aug. 2009
  • Firstpage
    2390
  • Lastpage
    2395
  • Abstract
    This paper examines the capturability of a guidance law that provides a desired angular acceleration of the heading angle to a pursuer. The guidance law has originally been proposed by Fajen and Warren[13], in order to explain the behavior of walking humans. It is shown that the relative rotational motion between a pursuer and an evader can be represented by an equation similar to the equation of motion for a pendulum with a disturbance. A set of sufficient conditions for successful pursuit are derived, and it is proved that the gain parameters of the guidance law can be chosen so that the conditions are satisfied. For sufficiently large gains, a pursuer controlled by the guidance law catches a maneuvering evader while achieving motion camouflage.
  • Keywords
    missile guidance; motion control; pendulums; angular acceleration input; capturability; evader; guidance law; heading angle; motion camouflage; pendulum; pursuer; relative rotational motion; walking humans; Acceleration; Angular velocity; Equations; Lyapunov methods; Missiles; Trajectory; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (ECC), 2009 European
  • Conference_Location
    Budapest
  • Print_ISBN
    978-3-9524173-9-3
  • Type

    conf

  • Filename
    7074763