TY - EJOUR
AU - Zaeri, Amir
AU - Noor, Samsul Bahari Mohd
AU - Isa, Maryam Mohd
AU - Taip, Farah Saleena
PY - 2024
DA - February
TI - Design of Integral Augmented Sliding Mode Control for Pitch Angle of a 3-DOF Bench-top Helicopter
T2 - Majlesi Journal of Electrical Engineering
VL - 4
L1 - https://oiccpress.com/Majlesi-Journal-of-Electrical-Engineering/article/design-of-integral-augmented-sliding-mode-control-for-pitch-angle-of-a-3-dof-bench-top-helicopter/
DO - 10.1234/mjee.v4i3.338
N2 - Sliding mode control (SMC) is a nonlinear controller that is used to achieve desired performance in the presence of unstructured uncertainty as a result of carelessness of parameter specification of the system. The main aim for sliding control, or also called Variable Structure Control, is to control the nonlinear plant by introducing a sliding surface. The sliding surface should be reached by making the state of system approach this level. In this paper, an integral augmented sliding mode control (SMC+I) is proposed to improve the control performance of a plant with uncertainty giving the example of bench-top helicopter and the results are compared with the results obtained from conventional sliding mode control with and without a boundary layer.   
IS - 3
PB - OICC Press
KW - sliding mode control, chattering phenomenon, Boundary layer, Pitch Angel of a 3-DOF Helicopter. 
EN -