Synthesis of nonlinear robust control for aerial vehicles under parameter uncertainties

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Authors

  • Nguyen Viet Phuong (Corresponding Author) Institute of Missile, Academy of Military Science and Technology
  • Nguyen Duy Khanh Faculty of Industrial Automation and Electrical Engineering, Saint Petersburg Electrotechnical University

DOI:

https://doi.org/10.54939/1859-1043.j.mst.105.2025.28-35

Keywords:

Aerial vehicle; Robust nonlinear control; Sliding mode control; Longitudinal motion; Parameter uncertainty.

Abstract

This paper proposes a nonlinear robust control strategy for the longitudinal motion channel of an aerial vehicle (AV) to enhance flight control quality under parameter uncertainties. A mathematical model of the control object is developed, and a robust nonlinear controller is synthesized using sliding mode control (SMC) combined with a reference model. The controller parameters are designed based on Lyapunov stability theory, ensuring the robust stability of the closed-loop system. A linear modal controller is developed to compare with the proposed nonlinear controller. Comparative simulations conducted in MATLAB/Simulink highlight the superior performance of the proposed controller in terms of tracking accuracy and robustness.

References

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Published

25-08-2025

How to Cite

[1]
D. P. Nguyen Viet and Nguyen Duy Khanh, “Synthesis of nonlinear robust control for aerial vehicles under parameter uncertainties”, J. Mil. Sci. Technol., vol. 105, no. 105, pp. 28–35, Aug. 2025.

Issue

Section

Electronics & Automation