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 :
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