• DocumentCode
    1721366
  • Title

    Time-varying sliding mode guidance with impact angle constraints against nonmaneuvering targets

  • Author

    Yao Zhao ; Yongzhi Sheng ; Xiangdong Liu

  • Author_Institution
    Sch. of Autom., Beijing Inst. of Technol., Beijing, China
  • fYear
    2013
  • Firstpage
    4898
  • Lastpage
    4903
  • Abstract
    In this paper, a time-varying sliding model control (TVSMC) based guidance law against nonmaneuvering targets is proposed with impact angle constraints. The algorithm is first designed for constant-speed interceptors to attack stationary and constant-velocity targets, and the global robustness of the system is ensured. Then, an adaptation strategy, adaptive time-varying sliding model control (ATVSMC), is adopted to deal with unknown but bounded disturbances by adjusting the switching gain online. Stability analysis of the closed loop system is obtained through Lyapunov theory. Finally, numerical simulation results are presented to verify the effectiveness and robustness of the proposed guidance law.
  • Keywords
    Lyapunov methods; adaptive control; asymptotic stability; closed loop systems; missile guidance; time-varying systems; variable structure systems; ATVSMC based guidance law; Lyapunov theory; adaptation strategy; adaptive time-varying sliding model control based guidance law; attack stationary; bounded disturbances; closed loop system stability analysis; constant-speed interceptors; constant-velocity targets; impact angle constraints; nonmaneuvering targets; switching gain; system global robustness; Acceleration; Adaptation models; Adaptive systems; Navigation; Robustness; Switches; Adaptive; Guidance; Impact angle; Robustness; Time-varying sliding model control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2013 32nd Chinese
  • Conference_Location
    Xi´an
  • Type

    conf

  • Filename
    6640289