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Adaptive Barrier Fast Terminal Sliding Mode Actuator Fault Tolerant Control Approach for Quadrotor UAVs

Author

Listed:
  • Amin Najafi

    (Department of Electrical Engineering, University of Zanjan, Zanjan 45195-313, Iran
    Amin Najafi and Mai The Vu are the first authors; These authors contributed equally to this work.)

  • Mai The Vu

    (School of Intelligent Mechatronics Engineering, Sejong University, Seoul 05006, Korea
    Amin Najafi and Mai The Vu are the first authors; These authors contributed equally to this work.)

  • Saleh Mobayen

    (Future Technology Research Center, National Yunlin University of Science and Technology, Douliu 64002, Taiwan)

  • Jihad H. Asad

    (Department of Physics, Faculty of Applied sciences, Palestine Technical University, Tulkarm P.O. Box 7, Palestine)

  • Afef Fekih

    (Department of Electrical and Computer Engineering, University of Louisiana at Lafayette, Lafayette, LA 70504, USA)

Abstract

This paper proposes an adaptive barrier fast terminal sliding mode control (ABFTSMC) approach for quadrotor unmanned aerial vehicles (UAV). Its main objectives are to mitigate the external disturbances, parametric uncertainties, and actuator faults. An adaptive barrier function is considered in the design to ensure the finite-time convergence of the output variables to a predefined locality of zero, independent of the disturbance bounds. A fast terminal sliding mode control (FTSMC) approach is designed to speed up the convergence rate in both reaching and sliding phases. The design considers hyperbolic tangent functions in the adaptive control law to drastically reduce the chattering effect, typically associated with the standard SMC. The performance of the proposed approach was assessed using a quadrotor UAV subject to external disturbances and sudden actuator faults. The obtained results show that the trajectory and the sliding surface converge to the origin in a finite time, without being affected by the high disturbance and actuator faults. In this method, due to the substitution of the discontinuous function by the hyperbolic tangent function, the chattering effect has also been highly reduced.

Suggested Citation

  • Amin Najafi & Mai The Vu & Saleh Mobayen & Jihad H. Asad & Afef Fekih, 2022. "Adaptive Barrier Fast Terminal Sliding Mode Actuator Fault Tolerant Control Approach for Quadrotor UAVs," Mathematics, MDPI, vol. 10(16), pages 1-22, August.
  • Handle: RePEc:gam:jmathe:v:10:y:2022:i:16:p:3009-:d:893364
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    References listed on IDEAS

    as
    1. Kamran Naseri & Mai The Vu & Saleh Mobayen & Amin Najafi & Afef Fekih, 2022. "Design of Linear Matrix Inequality-Based Adaptive Barrier Global Sliding Mode Fault Tolerant Control for Uncertain Systems with Faulty Actuators," Mathematics, MDPI, vol. 10(13), pages 1-14, June.
    2. Khalid A. Alattas & Mai The Vu & Omid Mofid & Fayez F. M. El-Sousy & Afef Fekih & Saleh Mobayen, 2022. "Barrier Function-Based Nonsingular Finite-Time Tracker for Quadrotor UAVs Subject to Uncertainties and Input Constraints," Mathematics, MDPI, vol. 10(10), pages 1-16, May.
    3. Afef Fekih & Saleh Mobayen & Chih-Chiang Chen, 2021. "Adaptive Robust Fault-Tolerant Control Design for Wind Turbines Subject to Pitch Actuator Faults," Energies, MDPI, vol. 14(6), pages 1-13, March.
    4. Luis Arturo Soriano & José de Jesús Rubio & Eduardo Orozco & Daniel Andres Cordova & Genaro Ochoa & Ricardo Balcazar & David Ricardo Cruz & Jesus Alberto Meda-Campaña & Alejandro Zacarias & Guadalupe , 2021. "Optimization of Sliding Mode Control to Save Energy in a SCARA Robot," Mathematics, MDPI, vol. 9(24), pages 1-16, December.
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    Cited by:

    1. Liyin Zhang & Yinlong Hou & Hui Liu & Dafeng Tang & Long Li, 2023. "Prescribed Performance Fault-Tolerant Tracking Control of Uncertain Robot Manipulators with Integral Sliding Mode," Mathematics, MDPI, vol. 11(11), pages 1-20, May.
    2. Anh Tuan Vo & Thanh Nguyen Truong & Hee-Jun Kang, 2023. "Fixed-Time RBFNN-Based Prescribed Performance Control for Robot Manipulators: Achieving Global Convergence and Control Performance Improvement," Mathematics, MDPI, vol. 11(10), pages 1-25, May.
    3. Nguyen Xuan-Mung & Mehdi Golestani & Sung Kyung Hong, 2023. "Constrained Nonsingular Terminal Sliding Mode Attitude Control for Spacecraft: A Funnel Control Approach," Mathematics, MDPI, vol. 11(1), pages 1-23, January.

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