航空液压泵用大功率永磁同步电机系统控制器的设计

Design of High-Power Permanent Magnet Synchronous Motor System Controller for Aeronautic Hydraulic Pumps

  • 摘要: 为满足大功率航空液压电动泵对驱动系统在功能、性能与可靠性方面的严苛要求,该文基于DSP+FPGA架构,设计了一款大功率液压电动泵系统控制器。该控制器主控电路采用DSP+FPGA架构,可实现多路控制信号的高速采集与高速运算;控制策略采用基于最大转矩电流比(MTPA)的磁场定向控制(FOC),满足内置式永磁同步电机(IPMSM)高性能、高效率的运动控制需求。实验结果表明,该系统控制器能够可靠驱动 540 V 电压等级下 100 kW 永磁同步电机,整机效率可达 95% 以上。

     

    Abstract: To meet the stringent requirements of high-power aeronautic hydraulic electric pumps for the driving system in terms of function, performance and reliability, this paper designs a high-power hydraulic electric pump system controller based on the DSP+FPGA architecture. The main-control circuit of the controller adopts the DSP+FPGA architecture to realize high-speed acquisition and computation of multi-channel control signals. A field-oriented control (FOC) strategy based on maximum torque per ampere (MTPA) is adopted to satisfy the high-performance and high-efficiency motion-control demands of the interior permanent-magnet synchronous motor (IPMSM). The experimental results show that the proposed system controller can reliably drive a 100 kW permanent-magnet synchronous motor under the voltage level of 540 V, with the overall efficiency reaching more than 95%.

     

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