Autores
Aguilar Ibáñez Carlos Fernando
Mendoza Mendoza Julio Alberto
Título Output-Feedback Stabilization of the PVTOL Aircraft System Based on an Exact Differentiator
Tipo Revista
Sub-tipo JCR
Descripción Journal of Intelligent & Robotic Systems
Resumen An output-feedback control strategy for the regulation of a planar vertical take-off and landing aircraft is presented here. The strategy consists of two controllers that work simultaneously. The first controller stabilizes the vertical variable, and is based on a simple feedback linearization procedure, in combination with a nonlinear controller (which behaves as a terminal slide mode). The other controller stabilizes the horizontal and angular variables to the desired rest position, and was designed using an energy-control method. The velocities were exactly estimated with a second-order sliding-mode observer. Because this observer computes the velocities in finite time, the control strategy can be designed independently. The effectiveness of the closed-loop system was tested through numerical simulations and compared with other control strategies.
Observaciones doi: 10.1007/s10846-017-0660-0
Lugar Dordrecht
País Paises Bajos
No. de páginas 443-454
Vol. / Cap. v. 90 no. 3-4
Inicio 2018-06-01
Fin
ISBN/ISSN