Title :
Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem
Author :
Tayebi, Abdelhamid
Author_Institution :
Dept. of Electr. Eng., Lakehead Univ., Thunder Bay, ON
fDate :
7/1/2008 12:00:00 AM
Abstract :
In this note, we propose a quaternion-based dynamic output feedback for the attitude tracking problem of a rigid body without velocity measurement. Our approach consists of introducing an auxiliary dynamical system whose output (which is also a unit quaternion) is used in the control law together with the unit quaternion representing the attitude tracking error. Roughly speaking, the necessary damping that would have been achieved by the direct use of the angular velocity can be achieved, in our approach, by the vector part mathtilde q of the error signal between the output of the auxiliary system and the unit quaternion tracking error. The resulting velocity-free control scheme guarantees almost global asymptotic stability which is as strong as the topology of the motion space can permit. In the regulation case, our control law is a pure quaternion feedback (i.e., consisting of two terms that are vector parts of unit-quaternion), and hence, the control torques are naturally bounded by the control gains. Simulation results are provided to show the effectiveness of the proposed control scheme.
Keywords :
asymptotic stability; attitude control; feedback; tracking; vehicle dynamics; auxiliary dynamical system; control gain; control law; control torque; dynamical spacecraft model; global asymptotic stability; rigid body attitude tracking problem; unit quaternion-based dynamic output feedback; velocity-free control scheme; Angular velocity; Attitude control; Control systems; Damping; Error correction; Output feedback; Quaternions; Torque control; Velocity control; Velocity measurement; Attitude tracking; output feedback; rigid body;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.2008.927789