Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law

SG Dietz; CW Scherer; GJ Looije; S Bennani

Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law

SG Dietz, CW Scherer, GJ Looije, S Bennani

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

Original language	Undefined/Unknown
Title of host publication	AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit
Editors	s.n.
Place of Publication	Reston
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages	1-14
Number of pages	14
ISBN (Print)	1-56347-638-X
Publication status	Published - 2003
Event	AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit - Austin Duration: 11 Aug 2003 → 14 Aug 2003

Publication series

Name
Publisher	AIAA

Conference

Conference	AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit
City	Austin
Period	11/08/03 → 14/08/03

Keywords

Conf.proc. > 3 pag

Cite this

Dietz, SG., Scherer, CW., Looije, GJ., & Bennani, S. (2003). Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law. In s.n. (Ed.), AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit (pp. 1-14). American Institute of Aeronautics and Astronautics Inc. (AIAA).

Dietz, SG ; Scherer, CW ; Looije, GJ et al. / Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law. AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit. editor / s.n. Reston : American Institute of Aeronautics and Astronautics Inc. (AIAA), 2003. pp. 1-14

@inproceedings{25728b5c827e4c2c9fd5fb39e3de71a2,

title = "Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law",

keywords = "Conf.proc. > 3 pag",

author = "SG Dietz and CW Scherer and GJ Looije and S Bennani",

year = "2003",

language = "Undefined/Unknown",

isbn = "1-56347-638-X",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

pages = "1--14",

editor = "s.n.",

booktitle = "AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit",

address = "United States",

note = "AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit ; Conference date: 11-08-2003 Through 14-08-2003",

}

Dietz, SG, Scherer, CW, Looije, GJ & Bennani, S 2003, Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law. in s.n. (ed.), AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit. American Institute of Aeronautics and Astronautics Inc. (AIAA), Reston, pp. 1-14, AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit, Austin, 11/08/03.

Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law. / Dietz, SG; Scherer, CW; Looije, GJ et al.
AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit. ed. / s.n. Reston: American Institute of Aeronautics and Astronautics Inc. (AIAA), 2003. p. 1-14.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

TY - GEN

T1 - Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law

AU - Dietz, SG

AU - Scherer, CW

AU - Looije, GJ

AU - Bennani, S

PY - 2003

Y1 - 2003

KW - Conf.proc. > 3 pag

M3 - Conference contribution

SN - 1-56347-638-X

SP - 1

EP - 14

BT - AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit

A2 - s.n., null

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

CY - Reston

T2 - AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit

Y2 - 11 August 2003 through 14 August 2003

ER -

Dietz SG, Scherer CW, Looije GJ, Bennani S. Comparison of different LMI synthesis techniques to design a flexible aircraft gust response control law. In s.n., editor, AIAA guidance, navigation and control conference and exhibit / AIAA atmospheric flight mechanics conference and exhibit / AIAA modeling and simulation technologies conference and exhibit. Reston: American Institute of Aeronautics and Astronautics Inc. (AIAA). 2003. p. 1-14