DocumentCode :
1435752
Title :
Quaternion-Based Hybrid Control for Robust Global Attitude Tracking
Author :
Mayhew, Christopher G. ; Sanfelice, Ricardo G. ; Teel, Andrew R.
Author_Institution :
Robert Bosch Res. & Technol. Center, Palo Alto, CA, USA
Volume :
56
Issue :
11
fYear :
2011
Firstpage :
2555
Lastpage :
2566
Abstract :
It is well known that controlling the attitude of a rigid body is subject to topological constraints. We illustrate, with examples, the problems that arise when using continuous and (memoryless) discontinuous quaternion-based state-feedback control laws for global attitude stabilization. We propose a quaternion-based hybrid feedback scheme that solves the global attitude tracking problem in three scenarios: full state measurements, only measurements of attitude, and measurements of attitude with angular velocity measurements corrupted by a constant bias. In each case, the hybrid feedback is dynamic and incorporates hysteresis-based switching using a single binary logic variable for each quaternion error state. When only attitude measurements are available or the angular rate is corrupted by a constant bias, the proposed controller is observer-based and incorporates an additional quaternion filter and bias observer. The hysteresis mechanism enables the proposed scheme to simultaneously avoid the “unwinding phenomenon” and sensitivity to arbitrarily small measurement noise that is present in discontinuous feedbacks. These properties are shown using a general framework for hybrid systems, and the results are demonstrated by simulation.
Keywords :
angular velocity measurement; attitude control; attitude measurement; robust control; stability; state feedback; angular velocity measurements; attitude control; attitude measurements; binary logic; discontinuous quaternion-based state-feedback control laws; global attitude stabilization; hysteresis-based switching; measurement noise; quaternion-based hybrid control; quaternion-based hybrid feedback scheme; robust global attitude tracking; state measurements; unwinding phenomenon; Asymptotic stability; Attitude control; Noise; Noise measurement; Quaternions; Robustness; Trajectory; Attitude control; hybrid control; output feedback; robustness; spacecraft;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/TAC.2011.2108490
Filename :
5701762
Link To Document :
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