DocumentCode :
630641
Title :
Self-scheduled and structured H synthesis : A launch vehicle application
Author :
Saussie, David ; Barbes, Quentin ; Berard, Caroline
Author_Institution :
Electr. Eng. Dept., Polytech. Montreal, Montréal, QC, Canada
fYear :
2013
fDate :
17-19 June 2013
Firstpage :
1590
Lastpage :
1595
Abstract :
This paper presents a new application of structured H synthesis to tune self-scheduled controllers. Newly available MATLAB-based tools allow to tune fixed-structure linear controllers while satisfying H constraints. Moreover multi-model synthesis capabilities can extend their application to self-scheduled controllers. This technique is successfully applied to the attitude control of a launch vehicle in atmospheric ascent phase.
Keywords :
H control; aircraft; attitude control; control system synthesis; linear systems; tuning; H constraints; MATLAB-based tools; atmospheric ascent phase; fixed-structure linear controllers; launch vehicle application; launch vehicle attitude control; multimodel synthesis; self-scheduled controllers; self-scheduled synthesis; structured H synthesis; Hafnium; MATLAB; Mathematical model; Scheduling; Standards; Transfer functions; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2013
Conference_Location :
Washington, DC
ISSN :
0743-1619
Print_ISBN :
978-1-4799-0177-7
Type :
conf
DOI :
10.1109/ACC.2013.6580062
Filename :
6580062
Link To Document :
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