DocumentCode :
1743717
Title :
LMI based multi-objective H control of flexible microsatellites
Author :
Pittet, C. ; Mignot, J. ; Fallet, C.
Author_Institution :
CNES, Toulouse, France
Volume :
4
fYear :
2000
fDate :
2000
Firstpage :
4000
Abstract :
An example of an application of multi-objective control based on linear matrix inequalities (LMIs) is presented. H optimization is used to synthesize a dynamic output feedback controller for a microsatellite subject to disturbances, important sensor time delay, actuator saturation and flexible modes. The reduced controller is compared with a classical phase lead controller and finally validated with the complete nonlinear satellite model
Keywords :
H control; H optimisation; artificial satellites; attitude control; closed loop systems; control system synthesis; feedback; flexible structures; matrix algebra; nonlinear control systems; poles and zeros; reduced order systems; DEMETER; LMI based multi-objective H control; actuator saturation; classical phase lead controller; complete nonlinear satellite model; dynamic output feedback controller; flexible microsatellites; flexible modes; linear matrix inequalities; reduced controller; sensor time delay; Actuators; Delay effects; Linear matrix inequalities; Output feedback; Robust control; Satellites; Space technology; Symmetric matrices; Torque control; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2000. Proceedings of the 39th IEEE Conference on
Conference_Location :
Sydney, NSW
ISSN :
0191-2216
Print_ISBN :
0-7803-6638-7
Type :
conf
DOI :
10.1109/CDC.2000.912340
Filename :
912340
Link To Document :
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