Mixed sensitivity design: An aerospace case study

H. Kwakernaak

Mixed sensitivity design: An aerospace case study

H. Kwakernaak

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Professional

3 Citations (Scopus)

2 Downloads (Pure)

Abstract

The mixed sensitivity design method for multivariable linear control systems proposed in the companion paper (Kwakernaak, 2001) is applied to the design of a stability augmentation system for the longitudinal motion of a fighter airplane previously studied by Safonov and Chiang (1988). Both $H_\infty$ and $H_2$ mixed sensitivity design are considered. They lead to quite similar results

Original language	Undefined
Title of host publication	Proceedings of the 15th IFAC World Congress
Editors	E.F. Camacho, L. Basanez, J.A. de la Puente
Place of Publication	Amsterdam
Publisher	Elsevier
Pages	49-53
Number of pages	6
ISBN (Print)	978-0-08-044295-2
Publication status	Published - 2002
Event	15th IFAC World Congress 2002 - Barcelona, Spain Duration: 21 Jul 2002 → 26 Jul 2002 Conference number: 15 http://folk.ntnu.no/skoge/prost/proceedings/ifac2002/home.htm

Publication series

Name
Publisher	Elsevier

Conference

Conference	15th IFAC World Congress 2002
Country/Territory	Spain
City	Barcelona
Period	21/07/02 → 26/07/02
Internet address	http://folk.ntnu.no/skoge/prost/proceedings/ifac2002/home.htm

Keywords

METIS-211772
IR-69135
EWI-16733

Access to Document

Cite this

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title = "Mixed sensitivity design: An aerospace case study",

abstract = "The mixed sensitivity design method for multivariable linear control systems proposed in the companion paper (Kwakernaak, 2001) is applied to the design of a stability augmentation system for the longitudinal motion of a fighter airplane previously studied by Safonov and Chiang (1988). Both $H_\infty$ and $H_2$ mixed sensitivity design are considered. They lead to quite similar results",

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AU - Kwakernaak, H.

N1 - Conference code: 15

PY - 2002

Y1 - 2002

N2 - The mixed sensitivity design method for multivariable linear control systems proposed in the companion paper (Kwakernaak, 2001) is applied to the design of a stability augmentation system for the longitudinal motion of a fighter airplane previously studied by Safonov and Chiang (1988). Both $H_\infty$ and $H_2$ mixed sensitivity design are considered. They lead to quite similar results

AB - The mixed sensitivity design method for multivariable linear control systems proposed in the companion paper (Kwakernaak, 2001) is applied to the design of a stability augmentation system for the longitudinal motion of a fighter airplane previously studied by Safonov and Chiang (1988). Both $H_\infty$ and $H_2$ mixed sensitivity design are considered. They lead to quite similar results

KW - METIS-211772

KW - IR-69135

KW - EWI-16733

M3 - Conference contribution

SN - 978-0-08-044295-2

SP - 49

EP - 53

BT - Proceedings of the 15th IFAC World Congress

A2 - Camacho, E.F.

A2 - Basanez, L.

A2 - de la Puente, J.A.

PB - Elsevier

CY - Amsterdam

T2 - 15th IFAC World Congress 2002

Y2 - 21 July 2002 through 26 July 2002

ER -