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
Link To Document :
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