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  • 氫燃料電池空氣泵用PMSM預定義時空ST-SMO設計

    Predefined time-space super-twisting sliding mode observer design for permanent magnet synchronous motor in hydrogen fuel cell air pump

    • 摘要: 氫燃料電池空氣泵用高速永磁同步電機無位置傳感器,難以在極短時間內獲取電機轉子位置和速度的準確信息,為此,本文提出一種基于障礙函數的預定義時空超螺旋滑模觀測器設計方案。利用空間分割策略,將系統狀態空間劃分為障礙函數區與快速趨近區。在快速趨近區,設計預定義時空趨近律加速誤差收斂;在障礙函數區,提出一種新型障礙函數以抑制抖振。基于所提出的預定義時空趨近律與超螺旋滑模算法,構建電流觀測器,并?通過 Lyapunov 穩定性理論,證明電流觀測誤差在預定義時間內到達原點的預定義鄰域內。仿真結果表明,在目標轉速為時,所提觀測器可將轉子位置觀測誤差在預定義時間內實現觀測精度,與傳統滑模觀測器和傳統超螺旋滑模觀測器相比,本文提出的觀測器的誤差精度分別提升5.5%和4.875%。

       

      Abstract: For the high-speed permanent magnet synchronous motor (PMSM) with sensorless rotor position used in hydrogen fuel cell air pumps, it is challenging to obtain accurate information about the motor rotor position and speed within an extremely short time. To address this issue, this paper proposes a design scheme of a predefined time-space super-twisting sliding mode observer (PdT-ST-SMO) based on a barrier function. By adopting a space division strategy, the system states are divided into two regions, the barrier function region and the rapid reaching region. In the rapid reaching region, a predefined-time-space reaching law is employed to accelerate the convergence of errors. In the barrier function region, an improved barrier function is utilized to suppress chattering—a common issue in sliding mode control systems that can degrade control performance and cause mechanical wear. Ultimately, the super-twisting sliding mode algorithm is leveraged to achieve accurate observation of the back electromotive force (bEMF), which is crucial for deriving the rotor position and speed of the PMSM. Design an observer based on the designed predefined time-space reaching law and super-twisting sliding mode algorithm. To verify the stability of the proposed observer, the Lyapunov stability theory is applied. The theoretical analysis demonstrates that the current observation error of the designed observer can converge to the predefined neighborhood of the origin within the predefined time, ensuring the reliability and effectiveness of the observer in practical applications. Simulation results are presented to validate the performance of the proposed approach. When the target speed is , the proposed observer achieves the rotor position observation accuracy ofwithin the different predefined times . Comparative studies are conducted against the traditional sliding mode observer (SMO) and the conventional super-twisting sliding mode observer. The results show that the error accuracy of the observer proposed in this paper is improved by 5.5% and 4.875%, respectively, compared with these two traditional observers. This significant improvement in observation accuracy highlights the superiority of the proposed design in addressing the sensorless control challenge of high-speed PMSMs for hydrogen fuel cell air pumps, laying a solid foundation for enhancing the overall efficiency and stability of hydrogen fuel cell systems.

       

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