• DocumentCode
    2097359
  • Title

    ADRC based integrated guidance and control scheme for the interception of maneuvering targets with desired LOS angle

  • Author

    Zhao Chunzhe ; Huang Yi

  • Author_Institution
    Key Lab. of Syst. & Control, Acad. of Math. & Syst. Sci., Beijing, China
  • fYear
    2010
  • fDate
    29-31 July 2010
  • Firstpage
    6192
  • Lastpage
    6196
  • Abstract
    Based on the idea of the active disturbance rejection control (ADRC), an integrated guidance and control scheme is developed for the interception of maneuvering targets with the requested line-of-sight (LOS) angle. The ADRC based guidance law takes into account the nonlinearities and uncertainties involved both in the target kinematics and interceptor dynamics such that it can produce the acceleration which can realize the desired LOS angle even when the target is maneuvering. The ADRC based control law takes into account the nonlinearities and uncertainties existing in the motion dynamics such that the acceleration needed can be achieved. Furthermore, the capability of the proposed scheme is analyzed and the feasibility is tested by some simulations.
  • Keywords
    aerospace control; control nonlinearities; kinematics; ADRC based control law; ADRC based integrated guidance; LOS angle; active disturbance rejection control; interceptor dynamics; line-of-sight angle; maneuvering target; motion dynamics; nonlinearity; target kinematics; Acceleration; Aerodynamics; Control systems; Missiles; Navigation; Uncertainty; Control Design for Nonlinear Uncertain Systems; Guidance Law for Maneuvering Targets; Integrated Guidance and Control; LOS Angle Constraints; the Active Disturbance Rejection Control (ADRC);
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2010 29th Chinese
  • Conference_Location
    Beijing
  • Print_ISBN
    978-1-4244-6263-6
  • Type

    conf

  • Filename
    5573050