Static <mml:math altimg="si10.gif" display="inline" 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"><mml:msub><mml:mrow><mml:mi mathvariant="script">H</mml:mi></mml:mrow><mml:mrow><mml:mo>∞</mml:mo></mml:mrow></mml:msub></mml:math> loop shaping control of a fly-by-wire helicopter-Reference-Cited by-同舟云学术

Static H∞ loop shaping control of a fly-by-wire helicopter

Published:2005-09 Issue:9 Volume:41 Page:1517-1528
ISSN:0005-1098
Container-title:Automatica
language:en
Short-container-title:Automatica

Author:

Prempain E.,Postlethwaite I.

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Control and Systems Engineering

Reference36 articles.

1. Anonymous (1994). Handling qualities requirements for military rotorcraft, Aeronautical Design Standard ADS-33D. United States Army ATCOM St. Louis MO.

2. Fixed-order H∞ control design via a partially augmented Lagrangian method;Apkarian;International Journal of Robust and Nonlinear Control,2003

3. Self-scheduled H∞ control of a missile via linear matrix inequalities;Apkarian;AIAA Journal of Guidance Control and Dynamics,1995

4. Ouput feedback control of the angular velocity of a rigid body;Astolfi;Systems and Control Letters,1999

5. Static ouput feedback stabilization with prescribed degree of stability;Benton;IEEE Transactions on Automatic Control,1998

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