This book presents new necessary and sufficient conditions for
static output-feedback control of linear time-invariant systems
using the H-Infinity approach. This work presents a simplified
parameterization of all H-Infinity static state-feedback
controllers in terms of a single algebraic Riccati equation and a
free parameter matrix. This work also proposes three numerically
efficient solution algorithms for the coupled design equations to
determine the static output-feedback gain. These algorithms also
give flexibility to relatively weight control input and system
performance. Application to Unmanned Aerial Vehicles exemplifies
the power of the theory developed. This work gives a procedure for
designing compensators of specified structure for shaping the
closed loop response that uses H-infinity output-feedback design
techniques. The method developed takes advantage of the wealth of
experience in aerospace control design. F-16 design examples drawn
from the popular literature, Unmanned Aerial Vehicle Control,
Electromechanical Systems, and Wireless Control Design problems are
included to show the power of the approach.
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