DocumentCode
986561
Title
Quadratically constrained attitude control via semidefinite programming
Author
Kim, Yoonsoo ; Mesbahi, Mehran
Author_Institution
Dept. of Aeronaut. & Astronaut., Univ. of Washington, Seattle, WA, USA
Volume
49
Issue
5
fYear
2004
fDate
5/1/2004 12:00:00 AM
Firstpage
731
Lastpage
735
Abstract
We consider the attitude control problem augmented with an arbitrary number of nonconvex quadratic constraints. By utilizing the implicit magnitude constraint of the state vector (i.e., quaternion), we are able to reduce this problem to a convex quadratically constrained quadratic program or a semidefinite program. This result leads to an efficient solution strategy for general quadratically constrained attitude control problems. An example demonstrates the proposed methodology.
Keywords
attitude control; constraint theory; convex programming; space vehicles; implicit magnitude constraints; nonconvex quadratic constraints; quadratically constrained attitude control; semidefinite programming; state vector; Constraint optimization; Linear matrix inequalities; Optical control; Optimal control; Quadratic programming; Quaternions; Space missions; Space vehicles; Symmetric matrices; Torque control; Attitude control; convex optimization; semidefinite programming; state constrained control;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.2004.825959
Filename
1298998
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