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