DocumentCode
574595
Title
Structured H∞ control for a launch vehicle
Author
Knoblauch, M. ; Saussie, David ; Berard, Caroline
Author_Institution
SUPAERO, ISAE, Toulouse, France
fYear
2012
fDate
27-29 June 2012
Firstpage
967
Lastpage
972
Abstract
This work presents an application of structured H∞ synthesis, a novel robust controller synthesis technique that takes the benefits of the classic H∞ synthesis imposing additional restrictions to the controller structure. These restrictions allows the designer to synthesize controllers with a more understandable structure and help in the optimization process. This technique is applied to the atmospheric ascent phase of a launch vehicle.
Keywords
H∞ control; control system synthesis; optimisation; robust control; space vehicles; atmospheric ascent phase; controller structure; launch vehicle; optimization process; robust controller synthesis technique; structured H∞ control synthesis; understandable structure; Aerodynamics; Atmospheric modeling; Complexity theory; Hafnium; Mathematical model; Stability analysis; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2012
Conference_Location
Montreal, QC
ISSN
0743-1619
Print_ISBN
978-1-4577-1095-7
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2012.6315181
Filename
6315181
Link To Document