Fuzzy Logic Enhanced Second-Order Sliding Mode Controller Design for an Experimental Twin Rotor System Under External Disturbances


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Özer H. Ö., Hacıoğlu Y., Yağız N.

JOURNAL OF VIBRATION ENGINEERING & TECHNOLOGIES, cilt.12, ss.1-15, 2024 (SCI-Expanded, Scopus) identifier identifier

Özet

Abstract

Background

The twin rotor model is frequently studied by researchers because although it has a basic structure the coupled

pitch and yaw motions are adequately represented. However, it is quite difficult to obtain an efficient controller due to external

disturbances. Classical sliding mode controller (SMC), which is of first order, is recognized to be robust in case of parameter

changes and external disturbances especially when the sliding motion takes place, but it possesses chattering in the control

input which may damage the mechanical parts of the system.

Purpose

In this study it was aimed to design a robust controller without chattering effect which will be used for the control

of the twin rotor system in real time experiments.

Methods

To remedy the chattering issue, a novel fuzzy logic enhanced second-order sliding mode controller (FSOSMC)

based on super twisting algorithm is proposed. This controller suppresses chattering while enhancing the robustness of the

controller where the sliding surface slope parameter is updated online via a fuzzy logic unit. Then the proposed controller

is implemented on an experimental twin-rotor system which has highly nonlinear and coupled dynamics.

Results

Real time experiments were performed on the twin rotor system using the proposed FSOSMC. For comparison

purpose the SMC and second-order sliding mode controller (SOSMC) were also applied to the same system. The results

have shown that the proposed controller increased the tracking performance without increasing the control effort while

reducing the chattering.

Conclusions

The experimental results verified the success of the designed FSOSMC, therefore it may be recommended for

the robust and precise control of aerial vehicles.