• DocumentCode
    3601434
  • Title

    Global Exponential Attitude Tracking Controls on {mathsf {SO}}({mathsf 3})

  • Author

    Taeyoung Lee

  • Author_Institution
    Dept. of Mech. & Aerosp. Eng., George Washington Univ., Washington, DC, USA
  • Volume
    60
  • Issue
    10
  • fYear
    2015
  • Firstpage
    2837
  • Lastpage
    2842
  • Abstract
    This technical note presents four types of tracking control systems for the attitude dynamics of a rigid body. First, a smooth control system is constructed to follow a given desired attitude trajectory, while guaranteeing almost semi-global exponential stability. It is generalized to achieve global exponential stability by using a hybrid control scheme based on multiple configuration error functions. They are further extended to obtain robustness with respect to a fixed disturbance using an integral term. The resulting robust, global exponential stability for attitude tracking is the unique contribution of this technical note.
  • Keywords
    aircraft control; asymptotic stability; attitude control; trajectory control; attitude dynamics; attitude tracking; attitude trajectory; fixed disturbance; global exponential attitude tracking controls; hybrid control scheme; integral term; multiple configuration error functions; rigid body; semiglobal exponential stability; smooth control system; tracking control systems; Asymptotic stability; Attitude control; Control theory; Robustness; Stability; Switches; Attitude control; geometric control; hybrid systems; special orthogonal group;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/TAC.2015.2407452
  • Filename
    7050256