A structured <mml:math altimg="si1.gif" overflow="scroll" xmlns:xocs="http://www.elsevier.com/xml/xocs/dtd" xmlns:xs="http://www.w3.org/2001/XMLSchema" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns="http://www.elsevier.com/xml/ja/dtd" xmlns:ja="http://www.elsevier.com/xml/ja/dtd" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:tb="http://www.elsevier.com/xml/common/table/dtd" xmlns:sb="http://www.elsevier.com/xml/common/struct-bib/dtd" xmlns:ce="http://www.elsevier.com/xml/common/dtd" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:cals="http://www.elsevier.com/xml/common/cals/dtd" xmlns:sa="http://www.elsevier.com/xml/common/struct-aff/dtd"><mml:msub><mml:mrow><mml:mi>H</mml:mi></mml:mrow><mml:mrow><mml:mo>∞</mml:mo></mml:mrow></mml:msub></mml:math>-based optimization approach for integrated plant and self-scheduled flight control system design-Reference-Cited by-同舟云学术

A structured H∞-based optimization approach for integrated plant and self-scheduled flight control system design

Author:

Lhachemi H.,Saussié D.,Zhu G.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

2. Aircraft Control and Simulation;Stevens,2003

3. On the coupling between the plant and controller optimization problems;Fathy,2001

5. An optimization approach to integrated aircraft-controller design;Yang,2003

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