氢燃料电池空气泵用PMSM预定义时空ST-SMO设计

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

  • 摘要: 氢燃料电池空气泵用高速永磁同步电机无位置传感器,难以在极短时间内获取电机转子位置和速度的准确信息,为此,本文提出一种基于障碍函数的预定义时空超螺旋滑模观测器设计方案。利用空间分割策略,将系统状态空间划分为障碍函数区与快速趋近区。在快速趋近区,设计预定义时空趋近律加速误差收敛;在障碍函数区,提出一种新型障碍函数以抑制抖振。基于所提出的预定义时空趋近律与超螺旋滑模算法,构建电流观测器,并?通过 Lyapunov 稳定性理论,证明电流观测误差在预定义时间内到达原点的预定义邻域内。仿真结果表明,在目标转速为时,所提观测器可将转子位置观测误差在预定义时间内实现观测精度,与传统滑模观测器和传统超螺旋滑模观测器相比,本文提出的观测器的误差精度分别提升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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