采用自适应扰动控制的三叶涡轮独立桨距控制器设计

Na Wang, A. Wright, K. Johnson
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引用次数: 16

摘要

设计了基于自适应扰动控制(DAC)算法的独立桨距控制器(IPCs),用于调节转子转速和减轻额定风速下叶片根部的襟翼弯曲载荷。其中一个基于dac的IPCs是基于转换的对称-不对称(TSA)涡轮模型设计的,其中风扰动被建模为一个集体水平分量和一个不对称线性剪切分量。另一种基于dac的IPC基于多叶片坐标(MBC)转换涡轮模型,将水平分量和垂直剪切分量建模为阶跃波形扰动。通过Kronecker积求解的调节方程,得到了两种基于dac的IPCs。在设计过程中考虑了作动器的动力学特性,以补偿作动器的相位延迟。仿真研究表明,与比例积分(PI)集体螺距控制器(CPC)相比,所提出的基于dac的ipc是有效的。改进的转子转速调节和每转一次和每转两次的负载减少已经在提议的IPC设计中观察到。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Independent blade pitch controller design for a three-bladed turbine using disturbance accommodating control
Two independent pitch controllers (IPCs) based on the disturbance accommodating control (DAC) algorithm are designed for the three-bladed Controls Advanced Research Turbine to regulate rotor speed and to mitigate blade root flapwise bending loads in above-rated wind speed. One of the DAC-based IPCs is designed based on a transformed symmetrical-asymmetrical (TSA) turbine model, with wind disturbances being modeled as a collective horizontal component and an asymmetrical linear shear component. Another DAC-based IPC is designed based on a multiblade coordinate (MBC) transformed turbine model, with a horizontal component and a vertical shear component being modeled as step waveform disturbance. Both of the DAC-based IPCs are found via a regulation equation solved by Kronecker product. Actuator dynamics are considered in the design processes to compensate for actuator phase delay. The simulation study shows the effectiveness of the proposed DAC-based IPCs compared to a proportional-integral (PI) collective pitch controller (CPC). Improvement on rotor speed regulation and once-per-revolution and twice-per-revolution load reductions has been observed in the proposed IPC designs.
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