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基于Bladed和HiGale的风力发电系统半实物联合仿真

Hardware-in-loop Simulation of a Wind Turbine Based on Bladed and HiGale

  • 摘要:
      目的  风力发电系统结构复杂,为实现风力发电系统的高效测试和控制算法验证,需要对风力发电系统进行实时仿真。目前市场上缺乏国产的针对风力发电系统的实时仿真验证平台。
      方法  提出了一种基于Bladed和HiGale的半实物联合仿真系统架构,通过BHTM实现了Bladed和HiGale的实时联合仿真,用于风力发电系统控制器的硬件在环测试。
      结果  文章以典型半直驱永磁同步电机风力发电单元为例,搭建主要由风场模型、机械传动和电气模型构成的硬件在环模型,利用联合仿真平台针对并网控制、变桨控制和低电压穿越3种工况下硬件的性能进行测试。
      结论  实验结果一方面验证了并网控制和变桨控制算法的有效性;另一方面也证明了该平台可以在风力发电系统的开发测试阶段提供可靠的技术支持,对于提高系统研发效率、节省研发成本具有重要的工程意义。

     

    Abstract:
      Objective  The structure of the wind power generation system is complex, and in order to achieve efficient testing and control algorithm verification of the wind power generation system, it is necessary to simulate the wind power generation system in real time. At present, there is a lack of domestic real-time simulation and verification platform for wind power generation systems in the market.
      Method  A hardware-in-the-loop co-simulation system architecture based on Bladed and HiGale was proposed, and the real-time co-simulation of Bladed and HiGale through BHTM was realized for hardware-in-the-loop testing of wind power system controllers.
      Result  In this paper, a typical semi-direct drive permanent magnet synchronous motor wind power generation unit is taken as an example, and a hardware-in-the-loop accompanying test model is built, which is mainly composed of wind field model, mechanical transmission and electrical model, and the co-simulation platform was used to test the performance of the hardware under three working conditions: grid-connected control, pitch control and low-voltage ride-through.
      Conclusion  On the one hand, the experimental results verify the effectiveness of grid-connected control and pitch control algorithms. On the other hand, it is also proved that the platform can provide reliable technical support in the development and testing stage of wind power generation systems, which is of great engineering significance for improving system R&D efficiency and saving R&D costs.

     

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