TY - GEN
T1 - Output feedback sliding mode control of a PVTOL including actuators dynamics
AU - Cárdenas, Ricardo
AU - Aguilar, Luis T.
PY - 2011
Y1 - 2011
N2 - This paper focuses on the regulation problem of a planar vertical take-off and landing (PVTOL) aircraft using output feedback sliding mode controller where a sliding mode observer is used to estimate the velocity. The observer design is independent of the feedback control design (separation principle). Considering as important the actuators response in the performance of the closed-loop systems, the dynamics of the PVTOL is augmented with the dynamics of the actuators. The performance of the closed-loop system is illustrated through simulation results.
AB - This paper focuses on the regulation problem of a planar vertical take-off and landing (PVTOL) aircraft using output feedback sliding mode controller where a sliding mode observer is used to estimate the velocity. The observer design is independent of the feedback control design (separation principle). Considering as important the actuators response in the performance of the closed-loop systems, the dynamics of the PVTOL is augmented with the dynamics of the actuators. The performance of the closed-loop system is illustrated through simulation results.
KW - Planar Vertical Take Off and Landing
KW - observer
KW - separation principle
KW - variable structure systems
UR - http://www.scopus.com/inward/record.url?scp=80155210237&partnerID=8YFLogxK
U2 - 10.1109/CCA.2011.6044516
DO - 10.1109/CCA.2011.6044516
M3 - Contribución a la conferencia
AN - SCOPUS:80155210237
SN - 9781457710629
T3 - Proceedings of the IEEE International Conference on Control Applications
SP - 1482
EP - 1486
BT - 2011 IEEE International Conference on Control Applications, CCA 2011
T2 - 2011 20th IEEE International Conference on Control Applications, CCA 2011
Y2 - 28 September 2011 through 30 September 2011
ER -