Abstract
A non-smooth optimization approach for designing constant output-feedback controllers for linear time-invariant systems is considered. The design requirements combine H ∞ performance requirements 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 various flight control examples.
Original language | English |
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Article number | 5944996 |
Pages (from-to) | 1066-1072 |
Number of pages | 7 |
Journal | IEEE Transactions on Control Systems Technology |
Volume | 20 |
Issue number | 4 |
DOIs | |
State | Published - 2012 |
Keywords
- Flight control
- H optimization
- hifoo
- non-smooth optimization
- pole placement