• DocumentCode
    3523455
  • Title

    Effect of unmodelled actuator dynamics on feedback linearised systems and a two stage feedback linearisation method

  • Author

    Kara Mohamed, Mohamed ; Lanzon, A.

  • Author_Institution
    Control Syst. Centre, Univ. of Manchester, Manchester, UK
  • fYear
    2013
  • fDate
    10-13 Dec. 2013
  • Firstpage
    841
  • Lastpage
    846
  • Abstract
    This paper is concerned with the control design of nonlinear systems using feedback linearisation. The paper highlights the destabilisation effect of unmodelled actuator dynamics when applying feedback linearisation. To overcome this difficulty, a two stage feedback linearisation technique is proposed to compensate for actuator dynamics and subse- quently linearise nonlinear systems. A case study of a tri-rotor UAV is used to showcase the benefits of the proposed method in comparison with classical feedback linearisation. The paper is written from a UAV application´s point of view, however, the proposed procedure is still valid for any input-affine invertible nonlinear system.
  • Keywords
    actuators; compensation; control system synthesis; feedback; linearisation techniques; nonlinear control systems; stability; UAV application; actuator dynamics; compensation; control design; destabilisation effect; feedback linearised systems; input-affine invertible nonlinear system; tri-rotor UAV; two-stage feedback linearisation method; unmanned aerial vehicles; unmodelled actuator dynamics; Actuators; Nonlinear systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control (CDC), 2013 IEEE 52nd Annual Conference on
  • Conference_Location
    Firenze
  • ISSN
    0743-1546
  • Print_ISBN
    978-1-4673-5714-2
  • Type

    conf

  • DOI
    10.1109/CDC.2013.6759987
  • Filename
    6759987