Autores
Cruz Cortés Nareli
Aguilar Ibáñez Carlos Fernando
Suárez Castañón Miguel Santiago
Título Output Feedback Stabilization for a PVTOL Aircraft Based on a Sliding Mode Combined with an Energy Control Strategy (CCE 2015)
Tipo Congreso
Sub-tipo Memoria
Descripción 12th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)
Resumen A control strategy for the regulation of a PVTOL, based on output-feedback, is introduced. To this end, a couple of controllers or actuators that operate concurrently are proposed. One of them stabilizes the vertical variable, in finite time by means of a novel sliding mode controller. The other actuator uses the energy control approach to balance, simultaneously, the horizontal and angular variables. The needed velocity is computed in finite time by a second-order sliding-mode observer, which works independently of the controllers. To verify the performance of the stabilizing strategy, a numerical experiment and a numerical comparison among two well-known control strategies, were carried out.
Observaciones
Lugar México City
País Mexico
No. de páginas 6
Vol. / Cap.
Inicio 2015-10-28
Fin 2015-10-30
ISBN/ISSN