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Composite Continuous High-Order Nonsingular Terminal Sliding Mode Control for Flying Wing UAVs with Disturbances and Actuator Faults

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  • Hao Wang

    (School of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China)

  • Zhenhua Zhao

    (School of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China)

Abstract

Flying wing UAVs are widely used in both civil and military areas and they are vulnerable to being affected by multi-source disturbances and actuator faults due to their unique aerodynamic configuration. This paper proposes composite continuous high-order nonsingular terminal sliding mode control controllers for the longitudinal command tracking control of flying wing UAVs. The proposed method guarantees not only the finite-time convergence of command tracking errors, but also the continuity of control actions. Simulation results validate the effectiveness of the proposed method.

Suggested Citation

  • Hao Wang & Zhenhua Zhao, 2025. "Composite Continuous High-Order Nonsingular Terminal Sliding Mode Control for Flying Wing UAVs with Disturbances and Actuator Faults," Mathematics, MDPI, vol. 13(15), pages 1-14, July.
    • Handle: RePEc:gam:jmathe:v:13:y:2025:i:15:p:2375-:d:1709132
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