Skip to Main content Skip to Navigation
Conference papers

Partial linearization of the PVTOL aircraft with internal stability

Vincent Léchappé 1 Yannick Aoustin 1 L. Marquez Martinez 2 Claude Moog 1
1 IRCCyN - Institut de Recherche en Communications et en Cybernétique de Nantes
2 CICESE - Centro de Investigacion Cientifica y de Education Superior de Ensenada [Mexico]
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 : MIMO underactuated non-minimum phase zero-dynamics internal dynamics algebraic method partial linearization nonlinear stabilization PVTOL
Complete list of metadatas

Cited literature [17 references]  Display  Hide  Download
https://hal.archives-ouvertes.fr/hal-00858102
Contributor : Vincent Léchappé <>
Submitted on : Monday, January 25, 2016 - 11:08:56 AM
Last modification on : Tuesday, February 12, 2019 - 4:34:10 PM
Document(s) archivé(s) le : Tuesday, April 26, 2016 - 10:51:14 AM

File

Vignette du document
cdc_2013_hal.pdf
Files produced by the author(s)

Identifiers

Collections

CNRS | EC-NANTES | IRCCYN | UNAM | UNIV-NANTES | IRCCYN-ADTSI | TDS-MACS

Citation

Vincent Léchappé, Yannick Aoustin, L. Marquez Martinez, Claude Moog. Partial linearization of the PVTOL aircraft with internal stability. 52nd Conference on Decision and Control, Dec 2013, Florence, Italy. ⟨10.1109/CDC.2013.6760268⟩. ⟨hal-00858102⟩

Export

BibTeX TEI DC DCterms EndNote

Share

Metrics

Record views

544

Files downloads

438

Contact

Informations

CCSD