• DocumentCode
    553042
  • Title

    Disturbances analysis for a hypersonic vehicle based on adaptive fuzzy control

  • Author

    Zhao-Hua Yang ; Yun-shan Feng

  • Author_Institution
    Sch. of Instrum. Sci. & Opto-Electron. Eng., Beihang Univ., Beijing, China
  • Volume
    1
  • fYear
    2011
  • fDate
    26-28 July 2011
  • Firstpage
    123
  • Lastpage
    128
  • Abstract
    There are many different disturbances for hypersonic air vehicles due to complex flight environment and flight conditions of the high altitudes and Mach numbers. This paper analyses many kinds of disturbances such as aerodynamic interference, measurement noise, elevator disturbance and parametric uncertainty based on the fuzzy adaptive controller. Simulation results show that these disturbances obviously impact the flight tracking of height and velocity. However, the fuzzy adaptive controller is also able to effectively overcome these problems, and it has fine tracking performance and robustness.
  • Keywords
    Mach number; adaptive control; aerodynamics; aircraft control; fuzzy control; missiles; noise measurement; uncertain systems; Mach numbers; aerodynamic interference; elevator disturbance analysis; flight conditions; flight environment; flight tracking; fuzzy adaptive controller; hypersonic air vehicles; measurement noise; parametric uncertainty; Adaptation models; Aerodynamics; Atmospheric modeling; Elevators; Simulation; Uncertainty; Vehicles; adaptive; disturbance; fuzzy; hypersonic vehicle;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Fuzzy Systems and Knowledge Discovery (FSKD), 2011 Eighth International Conference on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-1-61284-180-9
  • Type

    conf

  • DOI
    10.1109/FSKD.2011.6019542
  • Filename
    6019542