DocumentCode
1506502
Title
A Lie-Backlund approach to equivalence and flatness of nonlinear systems
Author
Fliess, Michel ; Lévine, Jean ; Martin, Philippe ; Rouchon, Pierre
Author_Institution
Centre de Math. de Leurs Applications, Ecole Normalle Superieure de Cachan, France
Volume
44
Issue
5
fYear
1999
fDate
5/1/1999 12:00:00 AM
Firstpage
922
Lastpage
937
Abstract
A new system equivalence relation, using the framework of differential geometry of jets and prolongations of infinite order, is studied. In this setting, two systems are said to be equivalent if any variable of one system may be expressed as a function of the variables of the other system and of a finite number of their time derivatives. This is a Lie-Backlund isomorphism. The authors prove that, although the state dimension is not preserved, the number of input channels is kept fixed. They also prove that a Lie-Backlund isomorphism can be realized by an endogenous feedback. The differentially flat nonlinear systems introduced by the authors (1992) via differential algebraic techniques, are generalized and the new notion of orbitally flat systems is defined. They correspond to systems which are equivalent to a trivial one, with time preservation or not. The endogenous linearizing feedback is explicitly computed in the case of the VTOL aircraft to track given reference trajectories with stability
Keywords
aircraft control; differential geometry; feedback; nonlinear systems; Lie-Backlund isomorphism; VTOL aircraft; aircraft control; differential algebra; differential geometry; dynamic feedback; flat nonlinear systems; infinite order prolongation; system equivalence; tracking; Aircraft; Computational modeling; Control systems; Geometry; Helium; Linear feedback control systems; Nonlinear dynamical systems; Nonlinear systems; Stability; Trajectory;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/9.763209
Filename
763209
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