Title :
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
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;
Conference_Titel :
Decision and Control (CDC), 2013 IEEE 52nd Annual Conference on
Conference_Location :
Firenze
Print_ISBN :
978-1-4673-5714-2
DOI :
10.1109/CDC.2013.6760268
