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Purpose

This work focuses on modelling, robust controller design and real time control of 3-DOF Helicopter.

Design/methodology/approach

This study presents an improved H∞ controller for this aerial vehicle

Findings

Simulation and experiment results are addressed to demonstrate the capability of this proposed control strategy to counteract the effect of this disturbance

Originality/value

In order to reduce the complexity of the standard H∞ structure, a fixed order control design is proposed as original approach

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