Title :
On quaternion-based attitude control and the unwinding phenomenon
Author :
Mayhew, C.G. ; Sanfelice, R.G. ; Teel, A.R.
Author_Institution :
Robert Bosch Res. & Technol. Center, Palo Alto, CA, USA
fDate :
June 29 2011-July 1 2011
Abstract :
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and analysis of feedback control laws. Often, quaternion-based feedbacks require an additional mechanism that lifts a continuous attitude path to the unit quaternion space. When this mechanism is memoryless, it has a limited domain where it remains injective and leads to discontinuities when used globally. To remedy this limitation, we propose a hybrid-dynamic algorithm for lifting a continuous attitude path to the unit quaternion space. We show that this hybrid-dynamic mechanism allows us to directly translate quaternion-based controllers and their asymptotic stability properties (obtained in the unit-quaternion space) to the actual rigid-body-attitude space. We also show that when quaternion-based controllers are not designed to account for the double covering of the rigid-body-attitude space by a unit-quaternion parameterization, they can give rise to the unwinding phenomenon, which we characterize in terms of the projection of asymptotically stable sets.
Keywords :
asymptotic stability; attitude control; feedback; asymptotic stability properties; asymptotically stability; feedback control laws; hybrid dynamic algorithm; hybrid dynamic mechanism; pervasive representation; quaternion based attitude control; quaternion based controllers; quaternion based feedbacks; unit quaternion; unwinding phenomenon; Aerospace electronics; Asymptotic stability; Attitude control; Heuristic algorithms; Quaternions; Stability analysis; Trajectory;
Conference_Titel :
American Control Conference (ACC), 2011
Conference_Location :
San Francisco, CA
Print_ISBN :
978-1-4577-0080-4
DOI :
10.1109/ACC.2011.5991127