DocumentCode :
404000
Title :
Quadratically constrained attitude control via semidefinite programming
Author :
Kim, Yoonsoo ; Mesbahi, Mehran
Author_Institution :
Dept. of Aeronaut. & Astronaut., Washington Univ., Seattle, WA, USA
Volume :
4
fYear :
2003
fDate :
9-12 Dec. 2003
Firstpage :
3408
Abstract :
We consider the attitude control problem as 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 semi-definite 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; convex programming; quadratic programming; convex programming; nonconvex quadratic constraints; quadratically constrained attitude control; quadratically constrained quadratic program; quaternion; semidefinite programming; state vector; Nonlinear optics; Optical control; Optical sensors; Optimal control; Quadratic programming; Quaternions; Space missions; Space vehicles; Symmetric matrices; Torque control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2003. Proceedings. 42nd IEEE Conference on
ISSN :
0191-2216
Print_ISBN :
0-7803-7924-1
Type :
conf
DOI :
10.1109/CDC.2003.1271671
Filename :
1271671
Link To Document :
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