• DocumentCode
    183876
  • Title

    Almost global finite-time stable observer for rigid body attitude dynamics

  • Author

    Bohn, Jan ; Sanyal, Amit K.

  • Author_Institution
    Mech. & Aerosp. Eng., New Mexico State Univ., Las Cruces, NM, USA
  • fYear
    2014
  • fDate
    4-6 June 2014
  • Firstpage
    4949
  • Lastpage
    4954
  • Abstract
    A state observer is proposed for rigid body attitude motion with a given attitude dynamics model. This observer is designed on the state space of rigid body attitude motion, which is the tangent bundle of the Lie group of rigid body rotations in three dimensions, SO(3), and therefore avoids instability due to the unwinding phenomenon seen with unit quaternion-based attitude observers. In the absence of measurement noise and disturbance torques, the observer designed leads to almost global finite-time stable convergence of attitude motion state estimates to the actual states for a rigid body whose inertia is known. Almost global finite-time stability of this observer is shown using a Morse function as part of a Lyapunov analysis; this Morse function has been previously used for almost global asymptotic stabilization of rigid body attitude motion. Numerical simulation results confirm the analytically obtained stability properties of this attitude state observer. Numerical results also show that state estimate errors are bounded in the presence of bounded measurement noise and bounded disturbance torque.
  • Keywords
    Lie groups; Lyapunov methods; attitude control; convergence; motion control; numerical analysis; observers; stability; state-space methods; Lie group; Lyapunov analysis; Morse function; almost global finite-time stable observer; attitude motion state estimates; attitude state observer; bounded disturbance torque; bounded measurement noise; global asymptotic stabilization; global finite-time stable convergence; numerical simulation; rigid body attitude dynamics model; rigid body attitude motion; rigid body rotations; stability properties; state estimate errors; state observer design; state space; unit quaternion-based attitude observers; unwinding phenomenon; Angular velocity; Estimation error; Noise; Noise measurement; Observers; Torque; Torque measurement; Aerospace; Algebraic/geometric methods; Observers for nonlinear systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2014
  • Conference_Location
    Portland, OR
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4799-3272-6
  • Type

    conf

  • DOI
    10.1109/ACC.2014.6858823
  • Filename
    6858823