Observer-Driven LQR and FOLQR Control for Enhanced Stability of Underactuated 2-DOF Helicopter.
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Keywords

LQR;
Euler-langrangian
Trajectory tracking
MIMO Systems
Observer design

How to Cite

Abro, G. E. M., & Abdallah, A. M. (2025). Observer-Driven LQR and FOLQR Control for Enhanced Stability of Underactuated 2-DOF Helicopter. Instrumentation, 12(1). https://doi.org/10.15878/j.instr.202500263

Abstract

This study offers an empirical comparison of the Linear Quadratic Regulator (LQR) and Fractional Order LQR (FOLQR) controllers that were implemented on a two-degrees-of-freedom (2-DOF) Quanser Aero 2 helicopter platform. It employs both full and reduced-order observer designs to facilitate trajectory monitoring and stabilisation. The Aero 2 platform is dynamically modelled using Euler-Lagrange equations to develop a multi-input multi-output (MIMO) system. This system comprises two inputs and four state equations. The LQR and FOLQR controllers, in collaboration with observers, approximate states that are not directly measurable by utilising the system model and available data. This procedure effectively overcomes the practical limitations of sensors. The enhanced performance of FOLQR in regard to tracking precision and stability has been depicted from the experimental results, showing real-time execution on the Aero 2 platform. This paper provides rigorous insights into control engineering and advanced observer-based control design for underactuated systems

https://doi.org/10.15878/j.instr.202500263
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Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

Copyright (c) 2025 Ghulam E Mustafa Abro, Ayman M Abdallah

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