TY - GEN
T1 - Almost global finite-time stable observer for rigid body attitude dynamics
AU - Bohn, Jan
AU - Sanyal, Amit K.
PY - 2014
Y1 - 2014
N2 - 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.
AB - 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.
KW - Aerospace
KW - Algebraic/geometric methods
KW - Observers for nonlinear systems
UR - http://www.scopus.com/inward/record.url?scp=84905694151&partnerID=8YFLogxK
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U2 - 10.1109/ACC.2014.6858823
DO - 10.1109/ACC.2014.6858823
M3 - Conference contribution
AN - SCOPUS:84905694151
SN - 9781479932726
T3 - Proceedings of the American Control Conference
SP - 4949
EP - 4954
BT - 2014 American Control Conference, ACC 2014
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2014 American Control Conference, ACC 2014
Y2 - 4 June 2014 through 6 June 2014
ER -