• DocumentCode
    1253
  • Title

    Robust L_{bm \\infty } -Gain Fuzzy Disturbance Observer-Based Control Design With Adaptive Bounding for a Hypersonic Vehicle

  • Author

    Huai-Ning Wu ; Zhi-Yong Liu ; Lei Guo

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
  • Volume
    22
  • Issue
    6
  • fYear
    2014
  • fDate
    Dec. 2014
  • Firstpage
    1401
  • Lastpage
    1412
  • Abstract
    A novel robust fuzzy disturbance observer-based control (DOBC) design methodology with adaptive bounding is proposed for the longitudinal dynamics of a generic hypersonic vehicle (HV) with modeled and unmodeled disturbances. A Takagi-Sugeno (T-S) fuzzy model is first employed to approximate the nonlinear dynamics of an HV. Subsequently, a new fuzzy disturbance observer is constructed to estimate the modeled disturbance. An augmented system with multiple disturbances is thus obtained by combining the dynamics of HV and the state estimation error of the modeled-disturbance generator. Then, a robust L∞ -gain fuzzy DOBC design with adaptive bounding is developed to guarantee that the closed-loop augmented system is semiglobally input-to-state practically stable (ISpS) with an L∞-gain performance. In the proposed control scheme, the compound disturbance, including the unmodeled disturbance and the approximation error in fuzzy modeling procedure, is divided into the matched part and the mismatched one, which are attenuated by adaptive bounding control and L∞ -gain control, respectively. The outcome of the robust L∞-gain fuzzy DOBC problem is formulated as a linear matrix inequality (LMI) problem. Moreover, by means of the existing LMI optimization technique, a suboptimal controller is obtained in the sense of minimizing an upper bound of L∞-gain, meanwhile a control constraint is respected. Finally, simulation results demonstrate the effectiveness of the proposed controller.
  • Keywords
    adaptive control; aircraft control; approximation theory; closed loop systems; control system synthesis; fuzzy control; linear matrix inequalities; minimisation; nonlinear dynamical systems; observers; stability; suboptimal control; DOBC design methodology; ISpS; L∞ -gain control; L∞-gain performance; LMI optimization technique; T-S fuzzy model; Takagi-Sugeno fuzzy model; adaptive bounding control; approximation error; closed-loop augmented system; compound disturbance; control design; fuzzy modeling procedure; hypersonic vehicle; input-to-state practically stable; linear matrix inequality problem; longitudinal dynamics; modeled-disturbance generator; nonlinear dynamics; robust L ∞-gain fuzzy disturbance observer; robust L∞-gain fuzzy DOBC problem; robust fuzzy disturbance observer-based control; state estimation error; suboptimal controller; upper bound minimization; Adaptation models; Aerodynamics; Fuzzy control; Mathematical model; Nonlinear dynamical systems; Robustness; $L_infty$-gain; Adaptive bounding technique; disturbance observer; fuzzy control; hypersonic vehicle (HV); input-to-state practically stable (ISpS); linear matrix inequality;
  • fLanguage
    English
  • Journal_Title
    Fuzzy Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    1063-6706
  • Type

    jour

  • DOI
    10.1109/TFUZZ.2013.2292976
  • Filename
    6675804