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.
https://hal.archives-ouvertes.fr/hal-00858102
Contributor : Vincent Léchappé <>
Submitted on : Monday, January 25, 2016 - 11:08:56 AM Last modification on : Wednesday, December 2, 2020 - 10:14:03 PM Long-term archiving on: : Tuesday, April 26, 2016 - 10:51:14 AM
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⟩