DocumentCode :
838286
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
Volume :
53
Issue :
6
fYear :
2008
fDate :
7/1/2008 12:00:00 AM
Firstpage :
1516
Lastpage :
1520
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;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/TAC.2008.927789
Filename :
4601498
Link To Document :
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