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Gas turbine performance monitoring based on extended information fusion filter

机译:基于扩展信息融合滤波器的燃气轮机性能监测

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Performance monitoring is a critical issue for gas turbine engine for improving the operation safety and reducing the maintenance cost. With regard to this, variants of Kalman-filters-based state estimation have been employed to detect gas turbine performance, but the classical centralized Kalman filters are subject to heavy computational effort and poor fault tolerance. A novel nonlinear fusion filter algorithm using information description with distributed architecture is proposed and applied to gas turbine performance monitoring. This methodology is developed from federated Kalman filter, and a bank of local extended information filters and one information mixer are combined with extended information fusion filter. The local state estimates and covariance calculated in parallel by the local extended information filters are integrated in the information mixer to yield a global state estimate. The global state estimate of nonlinear system is fed back to the local filters with weighted factor for next iteration. The aim of the proposed methodology is to reduce the computational efforts of state estimation and improve robustness to sensor faults in cases of gas turbine performance monitoring. The simulation results on a turbofan engine confirm the extended information fusion filter's effective capabilities in comparison to the general central ones.
机译:对于燃气涡轮发动机而言,性能监测是关键问题,以提高运行安全性并降低维护成本。关于这一点,已经采用基于卡尔曼滤波器的状态估计的变体来检测燃气轮机性能,但是传统的集中式卡尔曼滤波器需要大量的计算工作和较差的容错能力。提出了一种基于信息描述的分布式架构非线性融合滤波算法,并将其应用于燃气轮机性能监测。该方法是从联邦卡尔曼滤波器发展而来的,并将一组本地扩展信息滤波器和一个信息混合器与扩展信息融合滤波器结合在一起。由局部扩展信息滤波器并行计算的局部状态估计和协方差被集成在信息混合器中以产生全局状态估计。非线性系统的全局状态估计被反馈给具有加权因子的局部滤波器,以进行下一次迭代。所提出的方法的目的是减少状态估计的计算量,并在燃气轮机性能监测的情况下提高对传感器故障的鲁棒性。涡轮风扇发动机的仿真结果证实了扩展信息融合滤波器与通用中央融合滤波器相比的有效功能。

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