Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
718853 | IFAC Proceedings Volumes | 2009 | 5 Pages |
Abstract
A non-smooth optimization approach for designing a constant output feedback controller for a linear time-invariant system is considered. The design requirements combine both H∞ performance requirements together with regional pole constraints. The pole constraints are embedded in the design criterion using a transformation on the system model which modifies the H∞ -norm of the closed-loop system via a barrier function that is related to the closed-loop poles damping. The method is applied to a flight control example.
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