• DocumentCode
    231322
  • Title

    A real-time assessment approach to quadrotor flight control capability

  • Author

    Liu Bin ; Zhao Zhiyao ; Yang Binxian ; Quan Quan ; Cai Kai-Yuan

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
  • fYear
    2014
  • fDate
    28-30 July 2014
  • Firstpage
    3112
  • Lastpage
    3117
  • Abstract
    To solve the problem for the online assessment of the quadrotor flight control capability, this paper proposes a novel definition of control capability, and an approach to assess the control capability online. A quadrotor fault model is presented firstly, and the real-time fault detection is implemented using an Extended Kalman filter. Then, the function fitting method is used to achieve real-time controlability calculation by obtaining the relation between the controllability and the estimated fault vector. Finally, the online assessment of control capability is achieved by the integration of the controllability and the performance factor of the control law. A simulation based on a quadrotor shows that the proposed approach can achieve an accurate online assessment of quadrotor flight control capability.
  • Keywords
    Kalman filters; autonomous aerial vehicles; controllability; fault tolerant control; helicopters; control law performance factor; controllability calculation; extended Kalman filter; fault vector estimation; function fitting method; quadrotor fault model; quadrotor flight control capability; realtime assessment approach; realtime fault detection; Aerospace control; Educational institutions; Electronic mail; Hafnium; Kalman filters; Monte Carlo methods; Real-time systems; Control Capability; Controllability; Extended Kalman Filter; Quadrotor;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2014 33rd Chinese
  • Conference_Location
    Nanjing
  • Type

    conf

  • DOI
    10.1109/ChiCC.2014.6895449
  • Filename
    6895449