• DocumentCode
    3028802
  • Title

    Compound control systems design for KKV based on the theory of adaptive approximate variable structure

  • Author

    Hao, Liu ; Yi, Shen

  • Author_Institution
    Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    1500
  • Lastpage
    1505
  • Abstract
    A robust controller design method for high-maneuverable kinetic kill vehicle (KKV) whose attitude is controlled by combining aerodynamic tail fins and direct force is presented in this paper, which is a new algorithm based on adaptive approximation variable structure control (AAVSC) theory. Using this approach chatting problem which is due to the presence of infinite frequency switching function can be solved basically. In addition, the boundaries of uncertainties and disturbances, whose deterministic structures are known exactly, can be obtained easily by using the technology of the on-line identification, which will make the compound control systems remain stable. Theoretical analysis and numerical simulation results show that adaptive approximation variable structure control law is robust against parameter perturbations and disturbances. Due to the effect of direct force, the response time can be dramatically shortened; therefore, the rapid response requirements for KKV can be met.
  • Keywords
    adaptive control; aerodynamics; attitude control; control system synthesis; missile control; motion control; robust control; variable structure systems; AAVSC theory; adaptive approximation variable structure control; aerodynamic tail fin; attitude control; chatting problem; compound control systems design; deterministic structure; high-maneuverable kinetic kill vehicle; infinite frequency switching function; missile; online identification; parameter disturbance; parameter perturbation; robust controller design; uncertainty boundary; Aerodynamics; Approximation methods; Force; Missiles; Switches; Uncertainty; KKV; adaptive variable structure; autopilot; compound control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5632358
  • Filename
    5632358