@article{Zaeri_Noor_Isa_Taip_2024, title={Design of Integral Augmented Sliding Mode Control for Pitch Angle of a 3-DOF Bench-top Helicopter}, volume={4}, url={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/}, DOI={10.1234/mjee.v4i3.338}, abstractNote={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.   }, number={3}, journal={Majlesi Journal of Electrical Engineering}, publisher={OICC Press}, author={Zaeri, Amir and Noor, Samsul Bahari Mohd and Isa, Maryam Mohd and Taip, Farah Saleena}, year={2024}, month={Feb.}, keywords={Boundary layer, Pitch Angel of a 3-DOF Helicopter., sliding mode control, chattering phenomenon} }