[Legacy Report] Nonlinear Control of Helicopter Model using Sliding Mode Control

#Nonlinear #control #Helicopter #model #2DOF #Sliding #mode #Control #Design #Regulation.

IEEE Control Society Islamabad has organized an event on "Nonlinear Control of Helicopter Model using Sliding Mode Control" on 20th April, 2016 at Capital University of Science and Technology (CUST).

Helicopter is a mechanical system used for flying purpose having many flying features. It offer a challenging task to design a controller for helicopters stability control. This helicopter model will be used to implement a simulation environment that can give a valid alternative to real flight testing. When the simulation environment is in place, the task is to develop a controller that will stabilize the helicopter.

The CE 150 is a helicopter model intended to study dynamics of this system and apply control systems techniques. In the First part, helicopter model is described, followed by mathematical modeling.  In next part, model simulation results without controller are explained. First order and higher order Sliding Mode controller are applied and their results have been compared to show the removal of chattering by higher order sliding mode controller. Only elevation dynamics of model helicopter are used in this document to consider a system free of cross coupling.

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• Islamabad, Islamabad Capital Territory
• Pakistan

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• Co-sponsored by Capital University of Science and Technology, Islamabad