Partial linearization of the PVTOL aircraft with internal stability

Author

Lechappe, V. ; Aoustin, Y. ; Marquez-Martinez, L.A. ; Moog, C.H.

Author_Institution

Ecole Centrale de Nantes, Univ. de Nantes, Nantes, France

fYear

2013

fDate

10-13 Dec. 2013

Firstpage

2564

Lastpage

2569

Abstract

The planar vertical take-off and landing (PVTOL) aircraft is worked out by inspecting the various feedback linearization solutions. Partial linearizations of the state space are performed, which ensure the stability of the associated internal dynamics. The results are obtained through the search of dummy outputs with a 0-dimensional, 1-dimensional or 2-dimensional zero-dynamics that are stable.

Keywords

aircraft landing guidance; feedback; linearisation techniques; stability; state-space methods; vehicle dynamics; 0-dimensional zero-dynamics; 1-dimensional zero-dynamics; 2-dimensional zero-dynamics; PVTOL aircraft; dummy outputs; feedback linearization solutions; internal dynamics; internal stability; partial linearization; planar vertical take-off and landing aircraft; state space; Aerodynamics; Aircraft; Biological system modeling; Couplings; Equations; Mathematical model; Stability analysis; MIMO; PVTOL; algebraic method; internal dynamics; non-minimum phase; nonlinear; partial linearization; stabilization; underactuated; zero-dynamics;

fLanguage

English

Publisher

ieee

Conference_Titel

Decision and Control (CDC), 2013 IEEE 52nd Annual Conference on

Conference_Location

Firenze

ISSN

0743-1546

Print_ISBN

978-1-4673-5714-2

Type

conf

DOI

10.1109/CDC.2013.6760268

Filename

6760268