• DocumentCode
    2848922
  • Title

    Finite-time attitude control for bank-to-turn missiles

  • Author

    Wang, Zhao ; Li, Shihua ; Fei, Shumin

  • Author_Institution
    Coll. of Inf. & Control Eng., China Univ. of Pet., Dongying, China
  • fYear
    2010
  • fDate
    26-28 May 2010
  • Firstpage
    2019
  • Lastpage
    2024
  • Abstract
    The design of a continuous finite-time controller for bank-to-turn(BTT) missiles is considered in this work. The proposed controller allows that roll rate and angle of attack can track the desired commands in finite-time with sideslip angle maintained in a small degree range. Based on input/output(I/O) feedback linearizaiton technique and finite-time stability results for homogenous system, a continuous finite-time controller is proposed. Compared with asymptotically stable systems, finite-time stable systems offer better robustness and disturbance rejection properties. Computer simulation results are presented to validate the effectiveness of our method.
  • Keywords
    asymptotic stability; attitude control; continuous time systems; linearisation techniques; missile control; state feedback; asymptotically stable system; bank-to-turn missiles; continuous finite time controller; disturbance rejection property; feedback linearizaiton technique; finite time attitude control; finite time stability; homogenous system; Automatic control; Control engineering; Control systems; Design automation; Educational institutions; Linear feedback control systems; Missiles; Output feedback; Petroleum; Stability; Attitude Control; BTT Missiles; Finite-time Control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Decision Conference (CCDC), 2010 Chinese
  • Conference_Location
    Xuzhou
  • Print_ISBN
    978-1-4244-5181-4
  • Electronic_ISBN
    978-1-4244-5182-1
  • Type

    conf

  • DOI
    10.1109/CCDC.2010.5498889
  • Filename
    5498889