• DocumentCode
    3211714
  • Title

    Nonlinear observer for real-time attitude estimation

  • Author

    Guerrero-Sánchez, W.F. ; Guerrero-Castellanos, J.F. ; Juárez-Salazar, R. ; Salmerón-Quiroz, B.B.

  • Author_Institution
    Fac. de Cienc. Fisico-Mat., Benemerita Univ. Autonoma de Puebla (BUAP), Puebla, Mexico
  • fYear
    2009
  • fDate
    10-13 Jan. 2009
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    This paper deals with the attitude estimation of a rigid body equipped with a module of GAM sensors (rate gyros, accelerometers and magnetometers). A quaternion-based nonlinear observer is proposed in order to fuse all information sources and to obtain an accurate estimation of the attitude. It is shown that the error dynamics can break up into two passive subsystems connected in ¿feedback¿. This property is a first and crucial result that could be used to show that the error dynamics is input-to-state stable (ISS) when the measurement disturbance is seen as an input and the error state as the state. The effectiveness of the observer is confirmed in a real-time application.
  • Keywords
    accelerometers; aircraft; attitude measurement; magnetometers; observers; real-time systems; GAM sensors; accelerometers; error dynamics; input-to-state stable; magnetometers; quaternion-based nonlinear observer; rate gyros; realtime attitude estimation; Accelerometers; Fuses; Gravity; Magnetic sensors; Magnetometers; Micromechanical devices; Observers; Quaternions; Robot kinematics; Robot sensing systems; Aerial Robotics; Attitude; MEMS sensors; Nonlinear Observer; SVD;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical Engineering, Computing Science and Automatic Control,CCE,2009 6th International Conference on
  • Conference_Location
    Toluca
  • Print_ISBN
    978-1-4244-4688-9
  • Electronic_ISBN
    978-1-4244-4689-6
  • Type

    conf

  • DOI
    10.1109/ICEEE.2009.5393399
  • Filename
    5393399