DocumentCode
2972306
Title
Dynamic feedback linearization with application to aircraft control
Author
Charlet, B. ; Levine, J. ; Marino, R.
Author_Institution
Ecole Nat. Superieure des Mines de Paris, Fontainebleau, France
fYear
1988
fDate
7-9 Dec 1988
Firstpage
701
Abstract
The authors study the problem of the linearization of a nonlinear system by dynamic state feedback. A necessary condition and a sufficient condition are presented and are shown to apply to a general aircraft model
Keywords
aircraft control; feedback; linearisation techniques; aircraft control; dynamic state feedback; linearization; nonlinear system; Aerospace control; Aircraft; Control systems; Erbium; Nonlinear dynamical systems; Nonlinear systems; Output feedback; Stability; State feedback; Sufficient conditions;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1988., Proceedings of the 27th IEEE Conference on
Conference_Location
Austin, TX
Type
conf
DOI
10.1109/CDC.1988.194400
Filename
194400
Link To Document