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Tan-Type BLF-Based Attitude Tracking Control Design for Rigid Spacecraft with Arbitrary Disturbances

Author

Listed:
  • Nguyen Xuan-Mung

    (Faculty of Mechanical and Aerospace Engineering, Sejong University, Seoul 05006, Republic of Korea)

  • Mehdi Golestani

    (Department of Electrical Engineering, Iran University of Science and Technology, Tehran 16844, Iran)

  • Sung-Kyung Hong

    (Faculty of Mechanical and Aerospace Engineering, Sejong University, Seoul 05006, Republic of Korea
    Department of Convergence Engineering for Intelligent Drone, Sejong University, Seoul 05006, Republic of Korea)

Abstract

This study deals with the problem of disturbances in observer-based attitude tracking control for spacecraft in the presence of inertia-matrix uncertainty and arbitrary disturbance. Following the backstepping control, a tan-type barrier Lyapunov function (BLF)-based attitude tracking control method with prescribed settling time and performance is systematically developed. The proposed control framework possesses three advantages over the existing attitude controllers. Firstly, the singularity problem associated with the use of fractional power in fixed-time control is effectively resolved without employing any command filter or piece-wise continuous function. Secondly, inspired by the concept of the tan-type BLF approach, any desired performance for the attitude tracking error is satisfied. Lastly, the total disturbance, including the system’s uncertainty, external disturbances, and time-derivative of the virtual control, is precisely reconstructed during a predefined time, even if the initial estimation error tends to infinity. Moreover, this time is determined as a tunable gain in the observer. The numerical simulations confirm the superior performance of the proposed control strategy in comparison with the existing pertinent works.

Suggested Citation

  • Nguyen Xuan-Mung & Mehdi Golestani & Sung-Kyung Hong, 2022. "Tan-Type BLF-Based Attitude Tracking Control Design for Rigid Spacecraft with Arbitrary Disturbances," Mathematics, MDPI, vol. 10(23), pages 1-21, December.
    • Handle: RePEc:gam:jmathe:v:10:y:2022:i:23:p:4548-:d:990304
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    References listed on IDEAS

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    1. Runze Chen & Zhenling Wang & Weiwei Che, 2022. "Adaptive Sliding Mode Attitude-Tracking Control of Spacecraft with Prescribed Time Performance," Mathematics, MDPI, vol. 10(3), pages 1-18, January.
    2. Qijia Yao & Hadi Jahanshahi & Irene Moroz & Naif D. Alotaibi & Stelios Bekiros, 2022. "Neural Adaptive Fixed-Time Attitude Stabilization and Vibration Suppression of Flexible Spacecraft," Mathematics, MDPI, vol. 10(10), pages 1-17, May.
    3. Dapeng Wang & Shaogang Liu & Youguo He & Jie Shen, 2021. "Barrier Lyapunov Function-Based Adaptive Back-Stepping Control for Electronic Throttle Control System," Mathematics, MDPI, vol. 9(4), pages 1-14, February.
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    Cited by:

    1. Nguyen Xuan-Mung & Mehdi Golestani & Huu Tiep Nguyen & Ngoc Anh Nguyen & Afef Fekih, 2023. "Output Feedback Control for Spacecraft Attitude System with Practical Predefined-Time Stability Based on Anti-Windup Compensator," Mathematics, MDPI, vol. 11(9), pages 1-17, May.

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