• DocumentCode
    1612598
  • Title

    Self-tuning PID control design for quadrotor UAV based on adaptive pole placement control

  • Author

    Jinpeng Yang ; Zhihao Cai ; Qing Lin ; Yingxun Wang

  • Author_Institution
    Nat. Key Lab. of Sci. & Technol. on Aircraft Control, Beihang Univ. Beijing, Beijing, China
  • fYear
    2013
  • Firstpage
    233
  • Lastpage
    237
  • Abstract
    Quadrotor helicopters are an increasingly popular rotorcraft for unmanned aerial vehicle (UAV) platforms. Many groups have worked on quadrotors and realized various controllers and scenarios for it. And PID controller, because of simple structure, good stability and less dependence on the model, plays an important role in quadrotor control. This paper presents an application of Self-tuning PID controller based on adaptive pole placement to a quadrotor. This controller can tune the PID parameters online according to the system change. And the simulation results show that the designed flight controller can achieve accurate control for quadrotor with enough adaptability and robustness.
  • Keywords
    adaptive control; autonomous aerial vehicles; control system synthesis; helicopters; mobile robots; three-term control; UAV platforms; adaptive pole placement control; flight controller design; proportional-integral-derivative control; quadrotor UAV; quadrotor control; quadrotor helicopters; rotorcraft; self-tuning PID control design; Adaptation models; Aerospace control; Equations; Helicopters; Mathematical model; Robustness; Simulation; adaptive control; flight control; quadrotor helicopters; self-tuning PID; simulation verification;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Chinese Automation Congress (CAC), 2013
  • Conference_Location
    Changsha
  • Print_ISBN
    978-1-4799-0332-0
  • Type

    conf

  • DOI
    10.1109/CAC.2013.6775734
  • Filename
    6775734