TY - GEN
T1 - Sliding mode control synthesis of a 3-DOF helicopter prototype using position feedback
AU - Starkov, Konstantin K.
AU - Aguilar, Luis T.
AU - Orlov, Yury
PY - 2008
Y1 - 2008
N2 - Sliding mode control synthesis is developed for an underactuated mechanical system. A laboratory helicopter prototype is used as a test bed. Both state feedback design and dynamic output feedback design with a nonlinear velocity observer, running in parallel, are proposed. Performance and robustness issues of the closed-loop system are illustrated in numerical simulations.
AB - Sliding mode control synthesis is developed for an underactuated mechanical system. A laboratory helicopter prototype is used as a test bed. Both state feedback design and dynamic output feedback design with a nonlinear velocity observer, running in parallel, are proposed. Performance and robustness issues of the closed-loop system are illustrated in numerical simulations.
UR - http://www.scopus.com/inward/record.url?scp=52049111897&partnerID=8YFLogxK
U2 - 10.1109/VSS.2008.4570713
DO - 10.1109/VSS.2008.4570713
M3 - Contribución a la conferencia
AN - SCOPUS:52049111897
SN - 9781424422005
T3 - IEEE 10th International Workshop on Variable Structure Systems, VSS'08
SP - 233
EP - 237
BT - IEEE 10th International Workshop on Variable Structure Systems, VSS'08
T2 - IEEE 10th International Workshop on Variable Structure Systems, VSS'08
Y2 - 8 June 2008 through 10 June 2008
ER -