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
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