| dc.contributor | Taylor & Francis | |
| dc.creator | López Araujo, Daniela Juanita | |
| dc.creator | Zavala Río, Arturo | |
| dc.creator | Fantoni, Isabelle | |
| dc.creator | Salazar, Sergio | |
| dc.creator | Lozano, Rogelio | |
| dc.date | 2018-08-24T23:52:29Z | |
| dc.date | 2018-08-24T23:52:29Z | |
| dc.date | 2010-06 | |
| dc.date.accessioned | 2023-07-17T22:03:16Z | |
| dc.date.available | 2023-07-17T22:03:16Z | |
| dc.identifier | D.J. López-Araujo, A. Zavala-Río, I. Fantoni, S. Salazar & R. Lozano (2010) Global stabilisation of the PVTOL aircraft with lateral force coupling and bounded inputs, International Journal of Control, 83:7, 1427-1441, DOI: 10.1080/00207171003758778 | |
| dc.identifier | http://hdl.handle.net/11627/4087 | |
| dc.identifier | https://doi.org/10.1080/00207171003758778 | |
| dc.identifier.uri | https://repositorioslatinoamericanos.uchile.cl/handle/2250/7543417 | |
| dc.description | "This work is devoted to prove that the nonlinear control scheme previously proposed by Zavala-Río, Fantoni and Lozano for the global stabilisation of the planar vertical take-off and landing (PVTOL) aircraft with bounded inputs neglecting the lateral force coupling is robust with respect to the parameter characterising such a lateral force coupling, ϵ, as long as such a parameter takes small enough values. In other words, global stabilisation is achieved even if ϵ > 0, provided that such a parameter be sufficiently small. As far as the authors are aware, such a property has not been proved in other existing control schemes when the value of ϵ is not known. The presented methodology is based on the use of embedded saturation functions. Furthermore, experimental results of the control algorithm implemented on a real prototype are presented." | |
| dc.format | application/pdf | |
| dc.language | eng | |
| dc.publisher | Taylor & Francis LTD | |
| dc.rights | Attribution-NonCommercial-NoDerivatives 4.0 Internacional | |
| dc.rights | http://creativecommons.org/licenses/by-nc-nd/4.0/ | |
| dc.subject | PVTOL aircraft | |
| dc.subject | Global stabilisation | |
| dc.subject | Bounded inputs | |
| dc.subject | Saturations | |
| dc.subject | Nonlinear control | |
| dc.subject | Robustness | |
| dc.subject | Area::CIENCIAS FÍSICO MATEMÁTICAS Y CIENCIAS DE LA TIERRA::MATEMÁTICAS | |
| dc.title | Global stabilisation of the PVTOL aircraft with lateral force coupling and bounded inputs | |
| dc.type | article | |
