DocumentCode :
294497
Title :
LMI-based model reduction for a vectored-thrust ducted fan
Author :
Beck, Carolyn ; Bodenheimer, Bobby ; Bendotti, Pascale
Author_Institution :
Dept. of Electr. Eng., California Inst. of Technol., Pasadena, CA, USA
Volume :
1
fYear :
1995
fDate :
13-15 Dec 1995
Firstpage :
871
Abstract :
This paper contains the first experimental application of model reduction methods developed for systems represented by a linear fractional transformation (LFT) on a repeated scalar uncertainty structure. These methods provide for reduction of both the state order, and the uncertainty descriptions. LFT models of a vectored-thrust flight control experiment are reduced in order to make controller synthesis feasible. Recent linear parameter varying design techniques are used to synthesize the controllers
Keywords :
aircraft control; matrix algebra; reduced order systems; state-space methods; transforms; uncertain systems; aircraft control; ducted fan engine; flight control; linear fractional transformation; linear matrix inequality; linear parameter varying design; model reduction; repeated scalar uncertainty structure; state order; state space model; uncertain systems; uncertainty descriptions; vectored-thrust ducted fan; Aerospace control; Aircraft propulsion; Control system synthesis; Ear; Nonlinear equations; Process control; Reduced order systems; State-space methods; Uncertain systems; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
Conference_Location :
New Orleans, LA
ISSN :
0191-2216
Print_ISBN :
0-7803-2685-7
Type :
conf
DOI :
10.1109/CDC.1995.479092
Filename :
479092
Link To Document :
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