Smooth robust adaptive sliding mode control of 2-DOF helicopter system

Authors

  • Dao Van Ba Institute of Weapons, Vietnam Defense Industry
  • Nguyen Viet Phuong (Corresponding Author) Institute of Missile, Academy of Military Science and Technology

DOI:

https://doi.org/10.54939/1859-1043.j.mst.107.2025.24-31

Keywords:

2-DOF helicopter; Nonlinear system; Robust adaptive sliding mode control; Smooth function; Parameter uncertainty; Time-varying disturbances.

Abstract

This paper investigates the development of a tracking control system for a 2-degree-of-freedom (2-DOF) helicopter under parameter uncertainties and time-varying external disturbances. A nonlinear mathematical model of the 2-DOF helicopter system is first established. Subsequently, a conventional sliding mode controller (SMC) is designed, and its limitations in handling parameter uncertainties and external disturbances are analyzed. To address these limitations, the paper proposes a smooth, robust adaptive sliding mode controller for the 2-DOF helicopter system, ensuring convergence of closed-loop signals. The robust stability of the proposed controller is rigorously proven using Lyapunov stability theory. The system is simulated in MATLAB/Simulink with both the conventional and proposed controllers. Comparative simulation results demonstrate that the proposed adaptive robust controller outperforms the conventional sliding mode controller and fully meets the control requirements.

References

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Published

28-11-2025

How to Cite

[1]
Dao Van Ba and D. P. Nguyen Viet, “Smooth robust adaptive sliding mode control of 2-DOF helicopter system”, JMST, vol. 107, no. 107, pp. 24–31, Nov. 2025.

Issue

Section

Electronics & Automation