H-Infinity Output Feedback Control (Paperback)

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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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Product Description

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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Product Details

General

Imprint

Lap Lambert Academic Publishing

Country of origin

Germany

Release date

December 2010

Availability

Expected to ship within 10 - 15 working days

First published

December 2010

Authors

,

Dimensions

229 x 152 x 7mm (L x W x T)

Format

Paperback - Trade

Pages

124

ISBN-13

978-3-8433-8606-7

Barcode

9783843386067

Categories

LSN

3-8433-8606-4



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