%0 Journal Article
%T Design of Integral Augmented Sliding Mode Control for Pitch Angle of a 3-DOF Bench-top Helicopter
%A Amir Hossein Zaeri
%A Samsul Bahari Mohd Noor
%A Maryam Mohd Isa
%A Farah Saleena Taip
%J Majlesi Journal of Electrical Engineering
%D 2010
%I Islamic Azad University- Majlesi
%R 10.1234/mjee.v4i3.338
%X 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.
%K Sliding Mode Control
%K Chattering Phenomenon
%K Boundary Layer
%K Pitch Angel of a 3-DOF Helicopter.
%U http://ee.majlesi.info/index/index.php/ee/article/view/338