• DocumentCode
    261623
  • Title

    Full linear control of a quadrotor UAV, LQ vs H

  • Author

    Araar, Oualid ; Aouf, Nabil

  • Author_Institution
    Centre for Electron. Warfare, Cranfield Univ., Shrivenham, UK
  • fYear
    2014
  • fDate
    9-11 July 2014
  • Firstpage
    133
  • Lastpage
    138
  • Abstract
    Quadrotors low level control has attracted the attention of many research works over the last decade. In most of previous works, position stabilisation was achieved using nonlinear control techniques. In this paper, two full linear techniques based on optimal control theory are presented. The first, based on the L2 norm, is a Linear Quadratique Servo (LQ-Servo) controller. The second one, optimizes the L norm and is designed using H control approach. Emphasis is placed on the robustness to external disturbances and particularly wind gusts. Simulation results based on the full nonlinear model of the quadrotor are presented as a basis of comparison between the two controllers.
  • Keywords
    H control; autonomous aerial vehicles; control system synthesis; helicopters; linear quadratic control; mobile robots; optimisation; position control; robust control; servomechanisms; H control; L norm optimization; L2 norm; LQ-servo controller; UAV; control system design; linear quadratique servo; optimal control theory; position stabilisation; quadrotor linear control; robustness; Equations; Mathematical model; Robustness; Trajectory; Vectors; Vehicle dynamics; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control (CONTROL), 2014 UKACC International Conference on
  • Conference_Location
    Loughborough
  • Type

    conf

  • DOI
    10.1109/CONTROL.2014.6915128
  • Filename
    6915128